US2845079A - Fuel flow divider - Google Patents

Fuel flow divider Download PDF

Info

Publication number
US2845079A
US2845079A US564101A US56410156A US2845079A US 2845079 A US2845079 A US 2845079A US 564101 A US564101 A US 564101A US 56410156 A US56410156 A US 56410156A US 2845079 A US2845079 A US 2845079A
Authority
US
United States
Prior art keywords
valve
flow
fuel
pressure
sector
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US564101A
Inventor
Forest F Hutton
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
PIERCE GOVERNOR CO Inc
Original Assignee
PIERCE GOVERNOR CO Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by PIERCE GOVERNOR CO Inc filed Critical PIERCE GOVERNOR CO Inc
Priority to US564101A priority Critical patent/US2845079A/en
Application granted granted Critical
Publication of US2845079A publication Critical patent/US2845079A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22Fuel supply systems
    • F02C7/228Dividing fuel between various burners
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/2496Self-proportioning or correlating systems
    • Y10T137/2559Self-controlled branched flow systems
    • Y10T137/265Plural outflows
    • Y10T137/2657Flow rate responsive

Definitions

  • This invention relates generally to fuel-flow control systems for jet engines and it relates more particularly to a flow dividing and selecting valve for dividing and scheduling flow of fuelinto the after-burner manifold of a jet engine.
  • Conventional control devices for dividing and scheduling flow of fuel into an after burner include electrically operated valves and in order to prevent damage to such valves from theheat generated in the engine, it is necessary that they be located a substantial distance from the afterburner manifold.
  • the fuel lines between the valves and the burners are of substantial length and contain a substantial amount of fuel.
  • there is uncontrolled burning of fuel in these lines and coking of fuel therein which causes stoppage within the lines and faulty operation of the jet engine.
  • the principal object of this invention is to provide, in the fuel-supply system of a jet engine, a means of controlling division and scheduling of fuel flow which requires no control connections other than the usual fuel lines.
  • Another object of this invention is to provide, in a fuelcontrol system for a jet engine, a means of controlling division and scheduling of fuel flow which is not affected by high-fuel temperatures or high or low ambient temperatures.
  • Still another object of this invention is to provide a fuel-flow dividing and scheduling apparatus adapted to respond to pressure signals in the fuel-supply lines for controlling division of fuel flow in accordance with said pressure signals.
  • a further object of this invention is-to provide a fuelflow dividing and scheduling valve for jet engines which utilizes the fuel as a control medium for providing hydraulic forces to which the valve mechanism may respond.
  • a still further object of this invention is to provide fuel-flow dividing and scheduling apparatus for jet engines which operates by means of pressure signals to schedule division of flow of fuel to an after burner and to provide a predetermined fuel-to-air ratio throughout the complete range of engine power requirements at all altitudes of operation.
  • a still further object of this invention is to provide in a fuel-supply system for a multiple section burner in a jet engine, a means of scheduling flow of fuel to each section of said burner and of maintaining a predetermined ratio of fuel to certain sections of said burner throughout the complete range of engine power requirements at all altitudes of operation.
  • a still further object of this invention is to provide, in a fuel-flow system for a jet engine, a combined selector valve and flow-divider valve in a single unit or enclosure to afford maximum protection from heat, thereby to. shorten fuel lines to the burners and eliminate uncontrolled burn-j ing of fuel in said lines and coking of fuel therein.
  • a fuel-flow dividing and scheduling apparatus adapted to cooperate with a pilot operated control mechanism and a multiple sector burner for jet engines which comprises a plurality of pressure-responsive valves, each of which is connected to one of the sectors of said burner, one of said valves being responsive to a predetermined minimum inlet pressure for initiating fuel flow to a first section of said burner, a flow-divider valve responsive to a higher inlet pressure and coupled to a second one of said valves for initiating flow to a second sector of said burner, and I a selector valve coupled between the flow-divider valve and the others of said valves and responsive toa still higher inlet pressure for initiating flow of fuel to the remaining sectors of said burner.
  • Fig. 1 is a schematic diagram of a fuel-control system in which the flow divider and scheduling valve of this in vention is utilized.
  • Fig. 2 is a perspective view showing the top side of the flow divider and scheduling valve as provided in accordance with this invention.
  • Fig. 3 is a perspective view showing the bottom side of the valve shown in Fig. 2;
  • Fig. 4 is a longitudinal cross-section taken on a line through the axes of the primary sector valve, primary uniform valve, secondary uniform valve, inlet chamber and flow divider valve shown in Fig. 2.
  • Fig. 4A is a longitudinal cross-section of the secondary sector valve.
  • Fig. 4B is a longitudinal cross section of the squirtflow valve
  • Fig. 5 is a schematic diagram illustrating a longitudinal cross section similar to that shown in Fig. 4 and illustrating the valve mechanism in one phase of operation; and Fig. 6 is a schematic diagram similar to that of Fig. 5 but illustrating the valve mechanism in another phase of operation. 7
  • this invention is utilized in a fuelflow control system comprising a source of fuel (not shown) having connected thereto a first fuel supply pump 10, a main control throttle 11 connected to pump 10 and a fuel supply line 12 connected to the burners of a jet a engine (not shown). Flow of fuel through supply line 12 is controlled by the first of movement of the throttle lever 14.
  • a second supply pump 15 supplies fuel to the manifold 16 of the after burner of a jet engine through an afterburner control valve 17 and a flow divider and selector valve 18.
  • the valve 18 constitutes the principal feature of this invention and includes a fuel inlet 19, together with pressure-operated valves adapted to schedule and divide the flow of fuel coming from inlet 19 through the lines 20, 21, 22, and 23 connecting with the primary.
  • the flow divider and scheduling valve 18 consists of a body member 30 which may be in the form of a single casting having 'an inlet chamber 31 adapted to be coupled .to the inlet line 19 by means of a suitable coupling 32.
  • the primary sector line 20 may be coupled to the primary sector valve chamber'34 by means of a' conventional coupling member 35 while the secondary sector valve chamber 36 may be coupled to a secondary sector fuel line 21 by means of a conventional "coupling member 37.
  • the primary uniform fuel line 22 may be coupled with the p imary uniform valve chamber 38 by means of a coupling 39 bolted to the body by means of bolts 40.
  • the secondary uniform fuel line .23 may be coupled with the secondary uniform valve chamber 42 bymeans of a coupling member 43 bolted tothe body 30 by means of bolts 44.
  • a chamber 46 is formed in the body 30 for housing a flow-divider valve 47.
  • This valve consists of a cylindrical valve member 48 normally closing the port 49.
  • a cylindrical sleeve 50 fits over the stem portion of valve 48 and normally compresses a relatively light spring 51 and a relatively heavy spring 52 into engagement with the head portion of the valve 48.
  • the heavy spring 52 may be compressed to exert a predetermined amount of pressure on valve 48 by means of a plurality of washers 53 mounted over a locating stem 54, whereby the spring 52 is centered by means of stem 54 and the spring 51 is centered over the exterior of the spring 52.
  • the cylindrical sleeve member 50 is normally held downwardly (Fig. 6) by means of fluid pressure within chamber 56, thereby to hold valve 48 closed.
  • Chamber 31 is provided with the passage 58 opening into a passage 59 connecting with the valve chamber 34 of the primary sector valve 60.
  • the primary sector valve 60 normally closes passage 59 and a cap member 61 is suitably fixed to body 30 to confine a valveclosing spring 62 which normally holds the valve 60 in closed position.
  • the inlet 31 is connected to a selector valve chamber 64 by a passage 65 and the flow-divider valve chamber 46 is also connected to the selector valve chamber by means of a passage 66.
  • a selector valve 68 biased by spring 67 and having a land 69 normally closing passage 66 and a second land 70 positioned normally to close the passage 71 opening from chamber 64 into a chamber 38 containing a primary uniform valve 72.
  • the valve 72 is held in closed position by means of a spring 73 seated within a counter bore in coupling member 39 and normally exerting pressure on valve 72 holding it in closed position.
  • it is provided with longitudinal grooves, such as 75, whereby fuel may flow outwardly through coupling 39.
  • the selector valve 68 also closes, by means of land 69, a passage 76 opening from chamber .64 into the secondary uniform valve chamber 42.
  • the secondary uniform valve 77 is normally held in closed position with respect to passage 76 by means of the spring 78 nested at one end within a counterbore in coupling member 43, as shown in Fig. 4.
  • Spring 78 bears on the head portion of valve 77, as shown in Fig. 4, for holding this valve normally closed.
  • valve 77 is provided with longitudinal grooyes 79 which permit flow of fuel to coupling member .43 when the valve is opened.
  • the selector valve 68 includes another land 80 which normally is positioned as shown in Fig. 4 leaving a small chamber 81 which is connected to the passage 82 in coupling member 82 by means of the passage 83 having a restricted portion .84.
  • the coupling member 82 is fixed to a cover 86 secured to body portion 30 by means of bolts 87.
  • Land 80 includes a by-pass 85.
  • a plurality of washers 88 serve to hold a plate member 89, having passage 84 therein, in position over the land 80 of selector valve 68.
  • the flow-divider valve chamber 46 is also connected to the secondary sector valve chamber 36 by means of the passage 91 shown in dotted lines in Fig. 4.
  • a secondary sector valve 93 is also shown in dotted lines in Fig. and in cross-section in Fig. 4A, and it normally closes .
  • the secondary sector valve includes a spring 95 bearing on the inner surface 3' ment may be substantially instantaneous.
  • valve 93in closed position of a.cap.96 and .serving normally to hold valve 93in closed position.
  • a squirt-flow valve (Figs. 4 and 4B), biased by spring 99 operable within a chamber 101 and connected by passage 102 through coupling member 103 to an auxiliary fuel pump supply (not shown) which applies pressure within chamber 101 as will be described.
  • Chamber 101 is connected through a passage 104 with passage 83.
  • Chamber 101 is connected with chamber 56 over the flow-divider valve by means of a passage 105 and this passage is normally open with respect to land 106 of squirt valve 100.
  • Chamber 56 is connected by a bleeder passage .97 with chamber 64 and land 80 normally closes this passage.
  • the chamber 101 is also connected with chamber 64 of the selector valve by means of a passage 108 (Fig. 4B) opening into chamber 64 at a point normally below (Fig. 6) the land 80 of valve 68.
  • Another passage 109 opens into chamber 64 below (Fig. 6) the land 69. Passages 108 and 109 are .normally closed by lower land 112 of valve 100. This is shown schematically in Figs.
  • passage 107 is shown for convenience as coupling passages 10,8 and 109 to chamber 101.
  • Chamber 101 is connected by still another passage 110 to the lowermost (Fig. 6) end of chamber 64 and also to the coupling member 111 which connects with the low-pressure side .of the control apparatus 17.
  • the pilot causes the control lever 14 to swing through an arc of approximately 90 in which portion of the arc the control feeds the proper amountof fuel to the turbine section of a jet engine.
  • the normal fluid pressure within inlet 31 is less than sixty pounds per square inchand is not sufficient to open the Howdivider valve 47 or the primary sector valve 60.
  • the springs of these valves are designed to hold them closed until the control lever 14 is operated into the last 20 of its arc of operation.
  • valves 60, 72, 77, and 93 are designed to operate or to crack at a minimum pressure of sixty pounds per square inch. Therefore, the pressure within inlet 31 will become sufiicient to open the primary sector valve 60 when the arc of operation of lever 14 exceeds 90, and fuel will flow through line 20 to the primary sector 24 of the after burner 16, thereby to start its operation.
  • lever 14 is gradually moved from its 90 position to its 110 position or this'move- In either case, the pressure within the inlet 31 will build up while fuel flow continues through the primary sector valve 60.
  • the inlet pressure reaches pounds, for example. it overcomes the spring force on flow-divider 47, causing it to open slightly, at which time fuel can flow from inlet 31 through the port 49, chamber 46, passage 91, and port 94, thereby to open the secondary sector valve 93. This causes fuel to flow through line 21 to the secondary sector 25 of after burner 16.
  • control lever 14 and the after burner control valve 17 cause pressure signals to be generated, the first of which causes the primary sector valve 60 to open and the second of which causes the flow-divider valve 47 and the secondary sector valve 93 to open.
  • pressure signals By means of these pressure signals, flow of fuel is divided and scheduled with'respect to the primary sector and secondary sector of the after burner.
  • the squirt-flow valve 100 immediately moves downwardly .(Fig. to its lowermost position closing the passage 105. Meanwhile, land 80 of valve 68 opens passage 97 and the pressure in chamber 56 will decrease by reason of flow from this chamber through passages 97 and 85 into the chamber 64 between lands 69 and 80 of the selector valve (Fig. 5).
  • selector valve 68 will have connected port 65 and port 71, thereby applying pressure to the primary uniform valve 72 and opening it to permit flow of fuel through line 22 to the primary uniform burner 26.
  • the port 66 will have been connected with port 76, applying fluid pressure to the secondary uniform valve 77.
  • the fluid pressure will overcome the force of spring 78, opening valve 77 to permit flow of fuel through line 23 to the secondary uniform burner 27.
  • the light spring 51 will close the flow-divider valve 47, thereby cutting off flow of fuel to the secondary sector valve 93 and the secondary uniform valve 77.
  • the tWo primary valves 60 and -72 still receive flow of oil through the passages 58, 59, and 65, respectively, because passage 58 is always open to inlet 31 and the selector valve 68 is still in its open position.
  • valve 47 can open at this lower pressure because the head 50 is up and heavy spring 52 is ineffective.
  • the operating spring of the squirt-flow valve 100 quickly returns this valve to closed position, shown in Fig. 6.
  • the lower land 112 of the squirt-flow valve 100 immediately closes passage 107 to the selector valve 68.
  • passage 105 to the chamber 56 of the flowdivider valve 47 is opened.
  • the main selector valve 68 under the influence of spring 67,'moves slowly upwardly (Fig. 5) because of the restricted flow through passage 84, thereby closing the passage 97 to the flowdivider chamber 56.
  • valve squirt-flow pressure is connected to chamber 56, causing the piston 50 to move downwardly (Fig. 6) engaging the heavy .spring 52 with the valve head 48. If the pressure in inlet 31 has decreased, then the port 49 will be closed by valve '47. Also, the upward movement of the selector valve 68 will close the ports 71 and 76 of the primary and secondary uniform valves 72 and 77, respectively. Thus, flow'of fuel to burners 26 and 27 will be cut off. From the foregoing description, it will be apparent that the valve provided in accordance with this invention responds to changes of pressure in order to divide and schedule flow of fuel to different burners. The division and scheduling of fuel flow may be determined by designing the valve-operating springs and the valve orifices so that the valves will open and close when predetermined pressures occur.
  • the flowdivider and scheduling device as provided in accordance with this invention can be located in close proximity to the burners where the ambient temperatures are intense and would prohibit the use of hydraulic and electrical devices.
  • the resultant shortening of fuel lines prevents uncontrolled burning of fuel therein and the coking of fuel which would cause faulty operation of the burners.
  • I Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising an inlet, means for increasing or decreasing the pressure within said inlet, a first valve having spring means responsive to relatively low inlet'pressure permitting said valve to open and supply fuel to a first sector of said burner, second, third,
  • valves each including spring means for normally holdingsaid valves in closed position, means for coupling said second, third, and fourth valves to second, third, and fourth sectors of said burner, a flow-divider valve coupled to said inlet and including spring means responsive. to a predetermined higher pressure for per-f mitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve, whereby said second valve opens in response to said higher pressure to permit fuel flow to a second sector of said burner, a selector valve coupled between said flow-divider valve and said third and fourth valves and normally operative totisolate said third and fourth valves to maintain them in closed position, and a squirt-flow valve coupled to said control means and said selector valve and responsive to a predetermined third value of pressure for opening said selector valve and admitting pressure from said flow-divider valve to said third and fourth valves, thereby to supply fuel to the third and fourth sectors of said burner.
  • Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising an inlet, means for increasing or decreasing the pressure within said inlet, a first sector valve having spring means responsive to relatively low inlet pressure permitting said valve to open and supply fuel to a first sector-of said burner, other sector valves each including spring means for normally holding said valves in closed position, means for coupling said other sector valves to other sectors of said burner, a flow-divider valve coupled to said inlet and including spring means responsive to a predetermined higher pressure for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to one of said other valvesand n mal y per t ve-1o; cl esa roth s fsaid sector valves to maintain themjmelosed position, and a squirt-flow valve coupled to said'control means and said selector valve and responsive to a predetermined :third value of pressure for opening ,said selector valve and admitting pressure from said flow-divider valve :to said others
  • Apparatus for dividing andscheduling flow of fuel to a multiple sector burner comprising an inlet, means for increasing or decreasing the pressure within said inlet, a first sector valve having spring means responsive to relatively low inlet pressure permitting said valve to openand supply fuel to afirst sector of said burner, other sector valves eachincluding-spring means for normally holding'said valves in closedposition, means for coupling said other sector valves to other sectors of said burner, a flow-divider valve coupled to said inlet and including spring means responsive to a predetermined higher pressure for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to a second sector valve, whereby said second sector valve opens in response to said higher pressure to permit'fuel flow-to a second sector ofsaid burner, a selector means normally operative to maintain the remaining sector valves in closed position, and means responsive to a predetermined third value of pressure for operating said selector means to open said remaining sector valves, thereby to supply fuel to said other sectors of said burner.
  • Apparatus for dividing andschedulingfiowtof fuel to a multiple sector burner comprising aninlet, means for increasing or decreasing the, pressure within said inlet, a first sector valve having means responsive to relatively low inlet pressure permittingsaid .valveto open and supply fuel to a first sector of said burner, other sector valves normally in closed position, means for coupling said other sector valves to other sectorsiof ;said burner, a flow-divider valve coupled to said inlet, means responsive to a predetermined higher pressure for permitting said flowdivider valve to open, a passage coupling said flow-divider valve to a second sector valve, whereby said second sector valve opens in response to said higher pressure to permit fuel flow to a secondsector of said burner, and means responsive to a predetermined thirdvalue of pressure for first sector valve having'spring means responsive to relatively low inlet pressure permittingsaid valve to open and supply fuel to a firstsector of said burner, second, third, and fourth sector valves each including spring means for normally holding said valves in closed position, means responsive to
  • Apparatus for dividing and-scheduling flow of fuel to a multiple sector burner comprising an inlet, means for increasing or decreasing the pressure within said inlet, a first valve means responsive to relatively low inlet pressure to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low pressure, flow-divider valve means coupled to said inlot and responsive to a predeterminedhigher pressure for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens in response to said higher pressure to permit fuel flow to a second sector of ,6 said burner, and valve means (responsive to a predeterminedthird valueof pressure for admitting pressure from saidflow-divider valve .to said third and fourth valves, thereby to supply fuel to the third and fourth sectors of said burner.
  • Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a first valve means responsive to relatively low pressure thereon to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low pressure, flow-divider valve means including means responsive to a predetermined higher pressure thereon for permitting said fiow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens inresponseto said higher pressure thereon to permit fuel flow to a second sector of said burner, and valve means responsive to a predetermined third value of pressure thereon for admitting pressure from said flow-divider valve to said third and fourth valves, thereby to supply fuel to the third and fourth sectorsof said burner.
  • Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising an inlet, means for increasing or decreasing the pressure within said inlet, a first valve means responsive to relatively low inlet pressure to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low, pressure, flow-divider valve means coupled tosaid inlet and including spring means adjustable to respond to predetermined higher pressures for permitting said flow-divider valve to open, passages coupling :said flow-divider valve to said second, third, and fourth valve ean wher by sai sec d, th rd, and f r h valve means open in response to said higher pressures to permit fuel flow to other sectors of saidburner, and valve means responsive to a predetermined thirdvalue of pressure for adjusting said spring means to change the pressure to which said flow-divider valve responds.
  • Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising an inlet, means forincreasing or decreasing the pressure Within said inlet, a plurality of valves operable to open in response to a relatively low pressure in said inlet, flow-divider valve means coupled to said inlet and responsive to a predetermined higher pressure in said inletfor permitting said flow-divider valve to open, passageseoupling said fiowdivider valve to said valves, whereby said valves open in response to said higher pressure to permit fuel flow to the sectors of said burner, and valve means responsive to a predetermined third value of pressure for adjusting said flow-divider valve means to change the pressure at which said flow-divider valve responds.
  • Apparatus for dividing and scheduling flow of fuel to a multiple sector burner afirst valve means responsive to relatively low pressure to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low pressure, flow-divider valve means adjustable to respond to predetermined higher pressures for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens in response to said higher pressure to permit fuel flow to a second sector of said burner, and valve means rcsponsive to a predetermined third value of pressure for changing the pressure at which said flow-divider valve opens and admitting pressure to said third and fourth valves, thereby to supply fuel to the third and fourth sectors of said burner at different pressures.
  • Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a plurality of valve means responsive to a relatively low pressure, adjustable flow-divider valve means responsive to predetermined higher pressures for permitting said flow-divider valve to open, passages coupling said flow-divider valve to saicl plurality of valve means, whereby said plurality of valve means open in response to said higher pressure to permit fuel flow to said burner, and valve means responsive to a predetermined ":hird value of pressure for adjusting the pressure at which said flow-divider valve responds.
  • Apparatus for dividing and scheduling flow of fuel 'to a multiple sector burner comprising a first valve means responsive to relatively low pressure to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low pressure, flowdivider valve means adjustable to respond to predetermined higher pressures for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens in response to said higher pressure to permit fuel flow to a second sector of said burner, a selector valve coupling said flow-divider valve to said third and fourth valve means, and means responsive to a predetermined third value of pressure for changing the pressure at which said flow-divider valve opens and operating said selector valve to admit pressure to said third and fourth valves, thereby to supply fuel to the third and fourth sectors of said burner at different pressures.
  • Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a first valve means responsive to relatively low pressure to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low pressure, flow-divider valve means responsive to predetermined higher pressures for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens in response to said higher pressure to permit fuel flow to a second sector of said burner, and valve means coupling said flow-divider valve means to said third and fourth valve means and responsive to a predetermined third value of pressure for admitting pressure to said third and fourth valves, thereby to supply fuel to the third and fourth sectors of said burner at different pressures.
  • Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a plurality of valve means responsive to relatively low pressure, flow-divider valve means responsive to predetermined higher pressure for permitting said flow-divider valve to open, passages coupling said flow-divider valve to said plurality of valve means, and selector valve means in at least one of said passages and responsive to a predetermined third value of pressure for controlling admission of pressure to one of said valve means, thereby to supply fuel to said burner at different pressures.
  • Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a plurality of valves responsive to a relatively low pressure, flow-divider valve means adjustable to respond to predetermined higher pressures for permitting said flow-divider valve to open, passages coupling said flow-divider valve to said plurality of valves, a selector valve coupling said flow divider valve to at least one of said plurality of valves, and means responsive to a predetermined third value of pressure for changing the pressure at which said flowdivider valve opens and operating said selector valve to admit pressure to said one valve.
  • Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a first valve means responsive to relatively low pressure to supply fuel to a first sector of said burner, second, and other valve means responsive to an equally low pressure, flow-divider valve means adjustable to respond to predetermined higher pressures for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens in response to said higher pressure to permit fuel flow to a second sector of said burner, and scheduling means responsive to a predetermined third value of pressure for changing the pressure at which said flow-divider valve opens and admitting pressure to said other valve means, thereby to supply fuel to other sectors of said burner at different pressures.
  • Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a first valve means responsive to relatively low pressure to supply fuel to a first sector of said burner, other valve means responsive to an equally low pressure, flow-divider valve means responsive to predetermined higher pressure for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said other valve means, whereby said other valve means. opens in response to said higher pressure to permit fuel flow to a second sector of said burner, and scheduling means responsive to a predetermined value of pressure for admitting pressure to said other valve means, thereby to supply fuel to other sectors of said burner.

Description

July 29, 1958 F. F. HliTTON 2,845,079
FUEL FLOW DIVIDER 4- Sheets-Sheet 1 Filed Feb. 6, 1956 2 I INVENTQR. fbkz'sr 2? 02/770,
July 29, 1958 F. F. HUTTON 2,845,079
FUEL FLOW DIVIDER Filed Feb. 6, 1956 v 4 Sheets-Sheet 2 INVENTOR. fizz-5r)? flurra/v.
z wwd/w July 29, 1958 F. F. HUTTON FUEL FLOW DIVIDER 4 Sheets-Sheet 3 Filed Feb. 6, 1956 r IIIIIIIII llllllllllllll I w B a wmfl m; B r I a 5 M K m E I. 0 M M 2 \mm H 1 7 w y 1958 F. F. HUTTON 2,845,079
FUEL FLOW DIVIDER Filed Feb. 6, 195's 4 Sheets-Sheet 4 III him
w INVENTOR. faefsrf' flurra/v,
a/mins.
2,845,079 Patented July 29, 1958 FUEL FLOW DIVIDER Forest F. Hutton, Anderson, Ind., assignorto The Pierce Governor Company, Inc., Anderson, Ind, a corporation of Indiana Application February 6, 1956, Serial No. 564,101
17 Claims. Cl. 137-418) This invention relates generally to fuel-flow control systems for jet engines and it relates more particularly to a flow dividing and selecting valve for dividing and scheduling flow of fuelinto the after-burner manifold of a jet engine.
Conventional control devices for dividing and scheduling flow of fuel into an after burner include electrically operated valves and in order to prevent damage to such valves from theheat generated in the engine, it is necessary that they be located a substantial distance from the afterburner manifold. As a consequence, the fuel lines between the valves and the burners are of substantial length and contain a substantial amount of fuel. As a result, there is uncontrolled burning of fuel in these lines and coking of fuel therein which causes stoppage within the lines and faulty operation of the jet engine.
The use of electrical controls for such flow-divider valves naturally requires a rather complex electrical circuit and a substantial number of electrical conductors extending between the pilots control position and the valves of the engine. Accordingly, conventional control systems are subject to the usual troubles inherent in electrical circuits.
The principal object of this invention is to provide, in the fuel-supply system of a jet engine, a means of controlling division and scheduling of fuel flow which requires no control connections other than the usual fuel lines.
Another object of this invention is to provide, in a fuelcontrol system for a jet engine, a means of controlling division and scheduling of fuel flow which is not affected by high-fuel temperatures or high or low ambient temperatures.
Still another object of this invention is to provide a fuel-flow dividing and scheduling apparatus adapted to respond to pressure signals in the fuel-supply lines for controlling division of fuel flow in accordance with said pressure signals.
A further object of this invention is-to provide a fuelflow dividing and scheduling valve for jet engines which utilizes the fuel as a control medium for providing hydraulic forces to which the valve mechanism may respond.
A still further object of this invention is to provide fuel-flow dividing and scheduling apparatus for jet engines which operates by means of pressure signals to schedule division of flow of fuel to an after burner and to provide a predetermined fuel-to-air ratio throughout the complete range of engine power requirements at all altitudes of operation.
A still further object of this invention is to provide in a fuel-supply system for a multiple section burner in a jet engine, a means of scheduling flow of fuel to each section of said burner and of maintaining a predetermined ratio of fuel to certain sections of said burner throughout the complete range of engine power requirements at all altitudes of operation.
A still further object of this invention is to provide, in a fuel-flow system for a jet engine, a combined selector valve and flow-divider valve in a single unit or enclosure to afford maximum protection from heat, thereby to. shorten fuel lines to the burners and eliminate uncontrolled burn-j ing of fuel in said lines and coking of fuel therein.
In accordance with this invention there is provideda fuel-flow dividing and scheduling apparatus adapted to cooperate with a pilot operated control mechanism and a multiple sector burner for jet engines which comprises a plurality of pressure-responsive valves, each of which is connected to one of the sectors of said burner, one of said valves being responsive to a predetermined minimum inlet pressure for initiating fuel flow to a first section of said burner, a flow-divider valve responsive to a higher inlet pressure and coupled to a second one of said valves for initiating flow to a second sector of said burner, and I a selector valve coupled between the flow-divider valve and the others of said valves and responsive toa still higher inlet pressure for initiating flow of fuel to the remaining sectors of said burner.
The full nature of the invention will be understood from the accompanying drawings and the following description and claims:
Fig. 1 is a schematic diagram of a fuel-control system in which the flow divider and scheduling valve of this in vention is utilized.
Fig. 2 is a perspective view showing the top side of the flow divider and scheduling valve as provided in accordance with this invention; 1
Fig. 3 is a perspective view showing the bottom side of the valve shown in Fig. 2;
Fig. 4 is a longitudinal cross-section taken on a line through the axes of the primary sector valve, primary uniform valve, secondary uniform valve, inlet chamber and flow divider valve shown in Fig. 2.
Fig. 4A is a longitudinal cross-section of the secondary sector valve.
Fig. 4B is a longitudinal cross section of the squirtflow valve;
Fig. 5 is a schematic diagram illustrating a longitudinal cross section similar to that shown in Fig. 4 and illustrating the valve mechanism in one phase of operation; and Fig. 6 is a schematic diagram similar to that of Fig. 5 but illustrating the valve mechanism in another phase of operation. 7
Referring to Fig. 1, this invention is utilized in a fuelflow control system comprising a source of fuel (not shown) having connected thereto a first fuel supply pump 10, a main control throttle 11 connected to pump 10 and a fuel supply line 12 connected to the burners of a jet a engine (not shown). Flow of fuel through supply line 12 is controlled by the first of movement of the throttle lever 14. I
A second supply pump 15 supplies fuel to the manifold 16 of the after burner of a jet engine through an afterburner control valve 17 and a flow divider and selector valve 18. The valve 18 constitutes the principal feature of this invention and includes a fuel inlet 19, together with pressure-operated valves adapted to schedule and divide the flow of fuel coming from inlet 19 through the lines 20, 21, 22, and 23 connecting with the primary.
sector 24, secondary sector 25, primary uniform 26, and secondary uniform 27, respectively, of the after-burner manifold 16..
The flow divider and scheduling valve 18 consists of a body member 30 which may be in the form of a single casting having 'an inlet chamber 31 adapted to be coupled .to the inlet line 19 by means of a suitable coupling 32. The primary sector line 20 may be coupled to the primary sector valve chamber'34 by means ofa' conventional coupling member 35 While the secondary sector valve chamber 36 may be coupled to a secondary sector fuel line 21 by means of a conventional "coupling member 37.
The primary uniform fuel line 22 may be coupled with the p imary uniform valve chamber 38 by means of a coupling 39 bolted to the body by means of bolts 40. Similarly, the secondary uniform fuel line .23 may be coupled with the secondary uniform valve chamber 42 bymeans of a coupling member 43 bolted tothe body 30 by means of bolts 44.
A chamber 46 is formed in the body 30 for housing a flow-divider valve 47. This valve consists of a cylindrical valve member 48 normally closing the port 49. A cylindrical sleeve 50 fits over the stem portion of valve 48 and normally compresses a relatively light spring 51 and a relatively heavy spring 52 into engagement with the head portion of the valve 48. The heavy spring 52 may be compressed to exert a predetermined amount of pressure on valve 48 by means of a plurality of washers 53 mounted over a locating stem 54, whereby the spring 52 is centered by means of stem 54 and the spring 51 is centered over the exterior of the spring 52. The cylindrical sleeve member 50 is normally held downwardly (Fig. 6) by means of fluid pressure within chamber 56, thereby to hold valve 48 closed.
Chamber 31 is provided with the passage 58 opening into a passage 59 connecting with the valve chamber 34 of the primary sector valve 60. The primary sector valve 60 normally closes passage 59 and a cap member 61 is suitably fixed to body 30 to confine a valveclosing spring 62 which normally holds the valve 60 in closed position.
The inlet 31 is connected to a selector valve chamber 64 by a passage 65 and the flow-divider valve chamber 46 is also connected to the selector valve chamber by means of a passage 66. For controlling flow of fuel from inlet 31 and flow-divider chamber 46, there is provided a selector valve 68 biased by spring 67 and having a land 69 normally closing passage 66 and a second land 70 positioned normally to close the passage 71 opening from chamber 64 into a chamber 38 containing a primary uniform valve 72. The valve 72 is held in closed position by means of a spring 73 seated within a counter bore in coupling member 39 and normally exerting pressure on valve 72 holding it in closed position. In order to permit flow of fuel when valve 72 is opened, it is provided with longitudinal grooves, such as 75, whereby fuel may flow outwardly through coupling 39.
The selector valve 68 also closes, by means of land 69, a passage 76 opening from chamber .64 into the secondary uniform valve chamber 42. The secondary uniform valve 77 is normally held in closed position with respect to passage 76 by means of the spring 78 nested at one end within a counterbore in coupling member 43, as shown in Fig. 4. Spring 78 bears on the head portion of valve 77, as shown in Fig. 4, for holding this valve normally closed. As in the case of the primary uniform valve 72, valve 77 is provided with longitudinal grooyes 79 which permit flow of fuel to coupling member .43 when the valve is opened.
The selector valve 68 includes another land 80 which normally is positioned as shown in Fig. 4 leaving a small chamber 81 which is connected to the passage 82 in coupling member 82 by means of the passage 83 having a restricted portion .84. The coupling member 82 is fixed to a cover 86 secured to body portion 30 by means of bolts 87. Land 80 includes a by-pass 85. A plurality of washers 88 serve to hold a plate member 89, having passage 84 therein, in position over the land 80 of selector valve 68.
The flow-divider valve chamber 46 is also connected to the secondary sector valve chamber 36 by means of the passage 91 shown in dotted lines in Fig. 4. A secondary sector valve 93 is also shown in dotted lines in Fig. and in cross-section in Fig. 4A, and it normally closes .a passage 94 connecting the secondary sector chamber 36 with the passage 91. The secondary sector valve includes a spring 95 bearing on the inner surface 3' ment may be substantially instantaneous.
of a.cap.96 and .serving normally to hold valve 93in closed position.
For controlling timing and sequence of operation of the flow-divider valve 47 and the selector valve 68 and therewith the primary and secondary uniform valves 72, 77, together with the primary and secondary sector valves 60 and 93, there is provided a squirt-flow valve (Figs. 4 and 4B), biased by spring 99 operable within a chamber 101 and connected by passage 102 through coupling member 103 to an auxiliary fuel pump supply (not shown) which applies pressure within chamber 101 as will be described.
Chamber 101 is connected through a passage 104 with passage 83. Chamber 101 is connected with chamber 56 over the flow-divider valve by means of a passage 105 and this passage is normally open with respect to land 106 of squirt valve 100. Chamber 56 is connected by a bleeder passage .97 with chamber 64 and land 80 normally closes this passage. The chamber 101 is also connected with chamber 64 of the selector valve by means of a passage 108 (Fig. 4B) opening into chamber 64 at a point normally below (Fig. 6) the land 80 of valve 68. Another passage 109 opens into chamber 64 below (Fig. 6) the land 69. Passages 108 and 109 are .normally closed by lower land 112 of valve 100. This is shown schematically in Figs. 5 and 6 wherein passage 107 is shown for convenience as coupling passages 10,8 and 109 to chamber 101. Chamber 101 is connected by still another passage 110 to the lowermost (Fig. 6) end of chamber 64 and also to the coupling member 111 which connects with the low-pressure side .of the control apparatus 17.
In operation of a jet engine at normal flight speeds, the pilot causes the control lever 14 to swing through an arc of approximately 90 in which portion of the arc the control feeds the proper amountof fuel to the turbine section of a jet engine. During such periods the normal fluid pressure within inlet 31 is less than sixty pounds per square inchand is not sufficient to open the Howdivider valve 47 or the primary sector valve 60. The springs of these valves are designed to hold them closed until the control lever 14 is operated into the last 20 of its arc of operation.
The springs of valves 60, 72, 77, and 93 are designed to operate or to crack at a minimum pressure of sixty pounds per square inch. Therefore, the pressure within inlet 31 will become sufiicient to open the primary sector valve 60 when the arc of operation of lever 14 exceeds 90, and fuel will flow through line 20 to the primary sector 24 of the after burner 16, thereby to start its operation.
It will be noted that no fuel can flow to any of the other burners because the springs 51 and 52 of the flowdivider 47 are compressed by the valve head 50. This head is held in a lower position by pressure from the squirt-flow supply coming through passage 102, chamber 101 of the squirt-flow valve, and passage 105. Bleeder passage 97 is closed by land 80 of valve 68 and, therefore, selector valve 68 must operate before head 50 can move upwardly (Fig. 6). Also, fuel How is cut off from the primary uniform valve 72 by the land 70 of the sector valve.
It may be assumed that lever 14 is gradually moved from its 90 position to its 110 position or this'move- In either case, the pressure within the inlet 31 will build up while fuel flow continues through the primary sector valve 60. When the inlet pressure reaches pounds, for example. it overcomes the spring force on flow-divider 47, causing it to open slightly, at which time fuel can flow from inlet 31 through the port 49, chamber 46, passage 91, and port 94, thereby to open the secondary sector valve 93. This causes fuel to flow through line 21 to the secondary sector 25 of after burner 16.
From the foregoing description, it will be apparent that control lever 14 and the after burner control valve 17 cause pressure signals to be generated, the first of which causes the primary sector valve 60 to open and the second of which causes the flow-divider valve 47 and the secondary sector valve 93 to open. By means of these pressure signals, flow of fuel is divided and scheduled with'respect to the primary sector and secondary sector of the after burner.
As the fluid pressure within inlet 31 continues to increase, a point is reached where there is a differential of 100 pounds per square inch between the pressure in the passage 82' of coupling member 82 and the return line coupled to the coupling 111. As a result of this differential in pressure, the force of spring 99 is overcome and the squirt-flow valve 100 begins to open by the flow of fluid through passage 104 which connects to the chamber over the land 106. Simultaneously, there is restricted flow through passage 84, thereby starting movement of the selector valve 68.
The squirt-flow valve 100 immediately moves downwardly .(Fig. to its lowermost position closing the passage 105. Meanwhile, land 80 of valve 68 opens passage 97 and the pressure in chamber 56 will decrease by reason of flow from this chamber through passages 97 and 85 into the chamber 64 between lands 69 and 80 of the selector valve (Fig. 5).
When the squirt-flow valve 100 moved downwardly to the position shown in Fig. 5, fluid pressure was transferred to the selector valve through passages 107, 108, and 109. This flow ceases when the lands 69 and 80 close off passages 109 and 108, respectively, as shown in Fig. 5.
At this point, the selector valve 68 will have connected port 65 and port 71, thereby applying pressure to the primary uniform valve 72 and opening it to permit flow of fuel through line 22 to the primary uniform burner 26.
The port 66 will have been connected with port 76, applying fluid pressure to the secondary uniform valve 77. The fluid pressure will overcome the force of spring 78, opening valve 77 to permit flow of fuel through line 23 to the secondary uniform burner 27.
It will be understood that the flow-divider valve 47 will have opened completely when passage 97 was opened allowing the operating head 53 to move to its uppermost position shown in Fig; 5. This action disengaged the heavy spring 52 from the valve head 48, leaving only the light spring 51 in control of this section. In this manner, the flow-divider valve moves to its fully open position and there is full flow of fuel through all of the valves 60, 72, 77, and 93.
If the pressure within inlet 31 drops to 80 pounds per square inch, for example, under the control of the pilot, the light spring 51 will close the flow-divider valve 47, thereby cutting off flow of fuel to the secondary sector valve 93 and the secondary uniform valve 77. The tWo primary valves 60 and -72 still receive flow of oil through the passages 58, 59, and 65, respectively, because passage 58 is always open to inlet 31 and the selector valve 68 is still in its open position.
Another control action by the pilot can then occur which may boost the inlet pressure above 90 pounds per square inch and the flow-divider valve 47 may re-open, thereby re-opening the secondary sector valve 93 and the secondary uniform valve 77 thereby restoring burning in sectors 25 and 27. Valve 47 can open at this lower pressure because the head 50 is up and heavy spring 52 is ineffective.
When the pilot creates a control condition which causes the differential pressure between couplings 82 and 111 to decay toa value less than 100 pounds per square inch, the operating spring of the squirt-flow valve 100 quickly returns this valve to closed position, shown in Fig. 6. The lower land 112 of the squirt-flow valve 100 immediately closes passage 107 to the selector valve 68. Simultaneously, passage 105 to the chamber 56 of the flowdivider valve 47 is opened. The main selector valve 68 under the influence of spring 67,'moves slowly upwardly (Fig. 5) because of the restricted flow through passage 84, thereby closing the passage 97 to the flowdivider chamber 56. In this manner, the squirt-flow pressure is connected to chamber 56, causing the piston 50 to move downwardly (Fig. 6) engaging the heavy .spring 52 with the valve head 48. If the pressure in inlet 31 has decreased, then the port 49 will be closed by valve '47. Also, the upward movement of the selector valve 68 will close the ports 71 and 76 of the primary and secondary uniform valves 72 and 77, respectively. Thus, flow'of fuel to burners 26 and 27 will be cut off. From the foregoing description, it will be apparent that the valve provided in accordance with this invention responds to changes of pressure in order to divide and schedule flow of fuel to different burners. The division and scheduling of fuel flow may be determined by designing the valve-operating springs and the valve orifices so that the valves will open and close when predetermined pressures occur.
By utilizing pressure changes as signals to cause valve operation, it is possible to eliminate auxiliary, electrical, or hydraulic systems for operating the valves. The flowdivider and scheduling device as provided in accordance with this invention can be located in close proximity to the burners where the ambient temperatures are intense and would prohibit the use of hydraulic and electrical devices. The resultant shortening of fuel lines prevents uncontrolled burning of fuel therein and the coking of fuel which would cause faulty operation of the burners.
The invention claimed is: I 1. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising an inlet, means for increasing or decreasing the pressure within said inlet, a first valve having spring means responsive to relatively low inlet'pressure permitting said valve to open and supply fuel to a first sector of said burner, second, third,
and fourth valves each including spring means for normally holdingsaid valves in closed position, means for coupling said second, third, and fourth valves to second, third, and fourth sectors of said burner, a flow-divider valve coupled to said inlet and including spring means responsive. to a predetermined higher pressure for per-f mitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve, whereby said second valve opens in response to said higher pressure to permit fuel flow to a second sector of said burner, a selector valve coupled between said flow-divider valve and said third and fourth valves and normally operative totisolate said third and fourth valves to maintain them in closed position, and a squirt-flow valve coupled to said control means and said selector valve and responsive to a predetermined third value of pressure for opening said selector valve and admitting pressure from said flow-divider valve to said third and fourth valves, thereby to supply fuel to the third and fourth sectors of said burner.
2. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising an inlet, means for increasing or decreasing the pressure within said inlet, a first sector valve having spring means responsive to relatively low inlet pressure permitting said valve to open and supply fuel to a first sector-of said burner, other sector valves each including spring means for normally holding said valves in closed position, means for coupling said other sector valves to other sectors of said burner, a flow-divider valve coupled to said inlet and including spring means responsive to a predetermined higher pressure for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to one of said other valvesand n mal y per t ve-1o; cl esa roth s fsaid sector valves to maintain themjmelosed position, and a squirt-flow valve coupled to said'control means and said selector valve and responsive to a predetermined :third value of pressure for opening ,said selector valve and admitting pressure from said flow-divider valve :to said others ofsaid sector valves, thereby .to supply fuel tostill other sectorsof said burner.
3. Apparatus for dividing andscheduling flow of fuel to a multiple sector burner comprising an inlet, means for increasing or decreasing the pressure within said inlet, a first sector valve having spring means responsive to relatively low inlet pressure permitting said valve to openand supply fuel to afirst sector of said burner, other sector valves eachincluding-spring means for normally holding'said valves in closedposition, means for coupling said other sector valves to other sectors of said burner, a flow-divider valve coupled to said inlet and including spring means responsive to a predetermined higher pressure for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to a second sector valve, whereby said second sector valve opens in response to said higher pressure to permit'fuel flow-to a second sector ofsaid burner, a selector means normally operative to maintain the remaining sector valves in closed position, and means responsive to a predetermined third value of pressure for operating said selector means to open said remaining sector valves, thereby to supply fuel to said other sectors of said burner.
4, Apparatus for dividing andschedulingfiowtof fuel to a multiple sector burner comprising aninlet, means for increasing or decreasing the, pressure within said inlet, a first sector valve having means responsive to relatively low inlet pressure permittingsaid .valveto open and supply fuel to a first sector of said burner, other sector valves normally in closed position, means for coupling said other sector valves to other sectorsiof ;said burner, a flow-divider valve coupled to said inlet, means responsive to a predetermined higher pressure for permitting said flowdivider valve to open, a passage coupling said flow-divider valve to a second sector valve, whereby said second sector valve opens in response to said higher pressure to permit fuel flow to a secondsector of said burner, and means responsive to a predetermined thirdvalue of pressure for first sector valve having'spring means responsive to relatively low inlet pressure permittingsaid valve to open and supply fuel to a firstsector of said burner, second, third, and fourth sector valves each including spring means for normally holding said valves in closed position, means responsive to a predetermined higher pressure for permitting said second valve to'open in response to said higher pressure to permit fuel flow to asecond sector of said burner, and selectorv means operative in response to a predetermined third value of pressure for opening said third and fourth valves, thereby to supply fuel to the third and fourth sectors of said burner.
6. Apparatus for dividing and-scheduling flow of fuel to a multiple sector burner comprising an inlet, means for increasing or decreasing the pressure within said inlet, a first valve means responsive to relatively low inlet pressure to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low pressure, flow-divider valve means coupled to said inlot and responsive to a predeterminedhigher pressure for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens in response to said higher pressure to permit fuel flow to a second sector of ,6 said burner, and valve means (responsive to a predeterminedthird valueof pressure for admitting pressure from saidflow-divider valve .to said third and fourth valves, thereby to supply fuel to the third and fourth sectors of said burner.
7. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a first valve means responsive to relatively low pressure thereon to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low pressure, flow-divider valve means including means responsive to a predetermined higher pressure thereon for permitting said fiow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens inresponseto said higher pressure thereon to permit fuel flow to a second sector of said burner, and valve means responsive to a predetermined third value of pressure thereon for admitting pressure from said flow-divider valve to said third and fourth valves, thereby to supply fuel to the third and fourth sectorsof said burner.
8. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising an inlet, means for increasing or decreasing the pressure within said inlet, a first valve means responsive to relatively low inlet pressure to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low, pressure, flow-divider valve means coupled tosaid inlet and including spring means adjustable to respond to predetermined higher pressures for permitting said flow-divider valve to open, passages coupling :said flow-divider valve to said second, third, and fourth valve ean wher by sai sec d, th rd, and f r h valve means open in response to said higher pressures to permit fuel flow to other sectors of saidburner, and valve means responsive to a predetermined thirdvalue of pressure for adjusting said spring means to change the pressure to which said flow-divider valve responds.
9. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising an inlet, means forincreasing or decreasing the pressure Within said inlet, a plurality of valves operable to open in response to a relatively low pressure in said inlet, flow-divider valve means coupled to said inlet and responsive to a predetermined higher pressure in said inletfor permitting said flow-divider valve to open, passageseoupling said fiowdivider valve to said valves, whereby said valves open in response to said higher pressure to permit fuel flow to the sectors of said burner, and valve means responsive to a predetermined third value of pressure for adjusting said flow-divider valve means to change the pressure at which said flow-divider valve responds.
10. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner, afirst valve means responsive to relatively low pressure to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low pressure, flow-divider valve means adjustable to respond to predetermined higher pressures for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens in response to said higher pressure to permit fuel flow to a second sector of said burner, and valve means rcsponsive to a predetermined third value of pressure for changing the pressure at which said flow-divider valve opens and admitting pressure to said third and fourth valves, thereby to supply fuel to the third and fourth sectors of said burner at different pressures.
11. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a plurality of valve means responsive to a relatively low pressure, adjustable flow-divider valve means responsive to predetermined higher pressures for permitting said flow-divider valve to open, passages coupling said flow-divider valve to saicl plurality of valve means, whereby said plurality of valve means open in response to said higher pressure to permit fuel flow to said burner, and valve means responsive to a predetermined ":hird value of pressure for adjusting the pressure at which said flow-divider valve responds.
12. Apparatus for dividing and scheduling flow of fuel 'to a multiple sector burner comprising a first valve means responsive to relatively low pressure to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low pressure, flowdivider valve means adjustable to respond to predetermined higher pressures for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens in response to said higher pressure to permit fuel flow to a second sector of said burner, a selector valve coupling said flow-divider valve to said third and fourth valve means, and means responsive to a predetermined third value of pressure for changing the pressure at which said flow-divider valve opens and operating said selector valve to admit pressure to said third and fourth valves, thereby to supply fuel to the third and fourth sectors of said burner at different pressures.
13. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a first valve means responsive to relatively low pressure to supply fuel to a first sector of said burner, second, third, and fourth valve means responsive to an equally low pressure, flow-divider valve means responsive to predetermined higher pressures for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens in response to said higher pressure to permit fuel flow to a second sector of said burner, and valve means coupling said flow-divider valve means to said third and fourth valve means and responsive to a predetermined third value of pressure for admitting pressure to said third and fourth valves, thereby to supply fuel to the third and fourth sectors of said burner at different pressures.
14. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a plurality of valve means responsive to relatively low pressure, flow-divider valve means responsive to predetermined higher pressure for permitting said flow-divider valve to open, passages coupling said flow-divider valve to said plurality of valve means, and selector valve means in at least one of said passages and responsive to a predetermined third value of pressure for controlling admission of pressure to one of said valve means, thereby to supply fuel to said burner at different pressures.
15. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a plurality of valves responsive to a relatively low pressure, flow-divider valve means adjustable to respond to predetermined higher pressures for permitting said flow-divider valve to open, passages coupling said flow-divider valve to said plurality of valves, a selector valve coupling said flow divider valve to at least one of said plurality of valves, and means responsive to a predetermined third value of pressure for changing the pressure at which said flowdivider valve opens and operating said selector valve to admit pressure to said one valve.
16. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a first valve means responsive to relatively low pressure to supply fuel to a first sector of said burner, second, and other valve means responsive to an equally low pressure, flow-divider valve means adjustable to respond to predetermined higher pressures for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said second valve means, whereby said second valve means opens in response to said higher pressure to permit fuel flow to a second sector of said burner, and scheduling means responsive to a predetermined third value of pressure for changing the pressure at which said flow-divider valve opens and admitting pressure to said other valve means, thereby to supply fuel to other sectors of said burner at different pressures.
17. Apparatus for dividing and scheduling flow of fuel to a multiple sector burner comprising a first valve means responsive to relatively low pressure to supply fuel to a first sector of said burner, other valve means responsive to an equally low pressure, flow-divider valve means responsive to predetermined higher pressure for permitting said flow-divider valve to open, a passage coupling said flow-divider valve to said other valve means, whereby said other valve means. opens in response to said higher pressure to permit fuel flow to a second sector of said burner, and scheduling means responsive to a predetermined value of pressure for admitting pressure to said other valve means, thereby to supply fuel to other sectors of said burner.
References Cited in the file of this patent UNITED STATES PATENTS 2,606,066 Thompson Aug. 5, 1952 2,724,239 Fox Nov. 22, 1955 2,750,953 Helsey et a1. June 19, 1956
US564101A 1956-02-06 1956-02-06 Fuel flow divider Expired - Lifetime US2845079A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US564101A US2845079A (en) 1956-02-06 1956-02-06 Fuel flow divider

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US564101A US2845079A (en) 1956-02-06 1956-02-06 Fuel flow divider

Publications (1)

Publication Number Publication Date
US2845079A true US2845079A (en) 1958-07-29

Family

ID=24253157

Family Applications (1)

Application Number Title Priority Date Filing Date
US564101A Expired - Lifetime US2845079A (en) 1956-02-06 1956-02-06 Fuel flow divider

Country Status (1)

Country Link
US (1) US2845079A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2980176A (en) * 1957-01-15 1961-04-18 United Aircraft Corp Fail-safe afterburner fuel control
US3197958A (en) * 1961-10-11 1965-08-03 Parker Hannifin Corp Fuel selector and flow divider valve and control means for jet engines
US3411291A (en) * 1966-05-03 1968-11-19 Dowty Fuel Syst Ltd Fuel supply system for gas turbine engines
US5694967A (en) * 1995-11-14 1997-12-09 Dana Corporation Multi-port proportional flow control valve
US5941074A (en) * 1995-11-14 1999-08-24 Dana Corporation Multi-port proportional fuel control valve for gas turbine engine

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2606066A (en) * 1947-04-03 1952-08-05 Bendix Aviat Corp Automatic flow regulator
US2724239A (en) * 1952-04-21 1955-11-22 Samuel S Fox Fuel flow distributing and manifold pressurizing valve for dual orifice fuel injection nozzles
US2750953A (en) * 1952-12-19 1956-06-19 Gen Motors Corp Fluid flow proportioner

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2606066A (en) * 1947-04-03 1952-08-05 Bendix Aviat Corp Automatic flow regulator
US2724239A (en) * 1952-04-21 1955-11-22 Samuel S Fox Fuel flow distributing and manifold pressurizing valve for dual orifice fuel injection nozzles
US2750953A (en) * 1952-12-19 1956-06-19 Gen Motors Corp Fluid flow proportioner

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2980176A (en) * 1957-01-15 1961-04-18 United Aircraft Corp Fail-safe afterburner fuel control
US3197958A (en) * 1961-10-11 1965-08-03 Parker Hannifin Corp Fuel selector and flow divider valve and control means for jet engines
US3411291A (en) * 1966-05-03 1968-11-19 Dowty Fuel Syst Ltd Fuel supply system for gas turbine engines
US5694967A (en) * 1995-11-14 1997-12-09 Dana Corporation Multi-port proportional flow control valve
US5941074A (en) * 1995-11-14 1999-08-24 Dana Corporation Multi-port proportional fuel control valve for gas turbine engine

Similar Documents

Publication Publication Date Title
US2520434A (en) Control system for turbojet engines with reheat fuel supply system
US4027474A (en) Fuel prefill and distributor valve construction
US2986881A (en) Fuel accumulator for aircraft jet engine starter
US2818703A (en) Jet engine fuel, pressure ratio, and nozzle area control
US2808702A (en) Gas turbine pneumatic governor fuel supply control
US2845079A (en) Fuel flow divider
US3293847A (en) Coordinated main and afterburner fuel controls for gas turbine engines
US3052095A (en) Liquid vapor fuel system
US3857241A (en) Fuel control apparatus for gas turbine engine reheat systems
US3060684A (en) Control for missile having a plurality of jet engines
US2737016A (en) Afterburner controls
US2863283A (en) Speed control system for gas turbine engines
US3771314A (en) Gas turbine engine emergency speed control system
US2979889A (en) Temperature-modified exhaust nozzle scheduling controller for a gas turbine engine
US3289411A (en) Coordinated afterburner fuel control and exhaust nozzle area control for gas turbine engine
US2774414A (en) Fuel flow equalizer valve
US2734490A (en) moulton
US3080709A (en) Afterburner fuel and nozzle area control
US2555818A (en) Dual fuel engine
US3037552A (en) Prefilling system for the fuel-feed circuit of a ram-jet unit
US3760590A (en) Device for metering ignition fuel to the ignition unit of an afterburner associated with a turbojet engine
US2594790A (en) Fuel system for internal-combustion engines
US2788063A (en) Fluid flow controls
GB2285304A (en) A flow rate regulator
GB932749A (en) Improvements in afterburner fuel control mechanism for turbojet engines