US998897A - Propeller. - Google Patents

Propeller. Download PDF

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Publication number
US998897A
US998897A US60872811A US1911608728A US998897A US 998897 A US998897 A US 998897A US 60872811 A US60872811 A US 60872811A US 1911608728 A US1911608728 A US 1911608728A US 998897 A US998897 A US 998897A
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propeller
wood
laminations
portions
extremities
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US60872811A
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Spencer Heath
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/20Constructional features
    • B64C11/22Solid blades
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Definitions

  • the invention relates to screw propellers
  • One object of the invention is to produce a propeller with great strength and durability, without excessive or unnecessary weight.
  • a further object is to produce a propeller fromniaterials of unlike wei ht and durability, and having the materia s so arranged that'the less durable is protected. by the more durable at its more exposed edges and surfaces.
  • a further object is to produce a propeller, of moderate weight from materials of unlike weight? in such manner that the reatest portion of the heavier material shall be incorporated in the portion of the "propeller lying farthest from its axis of revolution.
  • FIG. 1 is a plan view.
  • Fig. 2 is a side elevation.
  • Fig. 3 is a perspective view of one of the laminations.
  • Fig. 4 is a typical transverse section of the unfinished propeller.
  • Figs; 5 and 6 are alternate forms of Fig. 1.
  • the propeller consistsof a series of five com und laminations these laminations being t d rmed of either two i or four pieces of wood.
  • the lowermost lamination, 1, is formed of two-pieces of hard wood (usually quartered white oak) joined together atthe liub with a diagonal scarf.
  • the uppermost lamination, 5, is likewise formed of two similar pieces of hard wood joined together at the' diate, laminations, however, are made up of four ieces each; two of these pieces being of so t wood of low specific gravity (usually spruce).
  • These two light portions, 2, '3 and 4:, of each intermediate lamination are similar to each other and joined together by a ub.
  • the intermee' diagonal scarf at the hub in the same manner as the hard wood laminations, 1 and 5.
  • the outer" extremities, however, of these in terior I soft wood portions are formed of pieces 8, 9 and 10, of hard, heavy, and durable wood. ,These pieces 8, 9 and 10, are secured to the extremities by the inner soft portions, 2, 3, and 4, respectively, by long slanting scarfed joints; With this arrangement 0 the wood, the propeller is formed of a relatively light inner core or .filler, surrounded and protected at all edges and ex-. posed portions of the blade and hub by the harder, heavier, and more durable material.
  • a propeller of the kind I the corresponding pieces forming each lamination are selected from adjacent portions of the same board,, and after placing one above the other they are sawed out together to the precise profile form ,whioh they will have in the finished propeller.
  • the hard wood portions for the extremities of the inner laminations are sawed out, each pair together,'in a similar manner.
  • Fig. 3 shows one of the inner laminations with the hard Wood extremities ready to be glued on, and the joint ready to be made at thehub. After the two sides orhalf laminations have been prepared, a hole is bored in the center of the hub portion of each, andnumerous similar holes arebored at regular intervals throughout the length of each half lamination.
  • a suitable block or I washer, 22, is laid upon the hub portion and the nut, 23, screwed down firmly'to clam all the scarfs and laminations in the hu securely together.
  • a laminated propeller consisting of interior laminations of soft wood, exterior laminations of hard wood, and hard wood portions forming the extremities of the interior laminati ons.
  • a laminated propeller consisting of interior laminations of soft wood, exterior laminations of hard wood, and hard wood portions forming the extremities of the interior laminations, the hard wood extremities being joined to the interior laminations by long slanting scarfs.
  • a propeller lamlnation comprising a central portion of light material and a peripheral portion of heavy material.
  • a propeller lamination comprising a central portion of light material and a peripheral portion of heavy material, the two portions being joined together by a long, slanting scarf.
  • a propeller lamination for two blades comprising two similar interior portions of light wood scarfed together at the hub and two similar peripheral portions of heavy wood scarfed to the extremities of the interior portions.

Description

S. HEATH.
PRQPELLEB.
APPLICATION FILED 53.15, 1911.
998,897, Patented July 25, 1911.
qwbbmzooeo @i ZZZ SPENCER HEATH, OF WASHINGTON,-DISTBIGT OF COLUMBIA.
PBOPELLER.
Specification of Letters .Patent.
Application filed February 15, 1911. Serial No. 608,728.
To all whom it may concern:
Be it known that .I, SPENCER HEATH,'a citizen of the United States, residing at Washington, in the District of Columbia, have invented certain new and useful Improvements in Propellers, of which the following is a specification.
The invention relates to screw propellers,
and particularly to screw propellers in connection with apparatus for navigating the air, and has special reference to laminated propellers formed of wood or similar material.
One object of the invention is to produce a propeller with great strength and durability, without excessive or unnecessary weight.
A further object is to produce a propeller fromniaterials of unlike wei ht and durability, and having the materia s so arranged that'the less durable is protected. by the more durable at its more exposed edges and surfaces. I L
A further object is to produce a propeller, of moderate weight from materials of unlike weight? in such manner that the reatest portion of the heavier material shall be incorporated in the portion of the "propeller lying farthest from its axis of revolution.
With the above objects in view and further objects which will appear, I have invented the form and style of propeller, one example of which is shown by the accompanying drawin forming a part of this specification, an in which- Figure 1 is a plan view. Fig. 2 is a side elevation. Fig. 3 is a perspective view of one of the laminations. Fig. 4 is a typical transverse section of the unfinished propeller. Figs; 5 and 6 are alternate forms of Fig. 1.
Referring to Fig. 1, the propeller consistsof a series of five com und laminations these laminations being t d rmed of either two i or four pieces of wood. The lowermost lamination, 1, is formed of two-pieces of hard wood (usually quartered white oak) joined together atthe liub with a diagonal scarf. The uppermost lamination, 5, is likewise formed of two similar pieces of hard wood joined together at the' diate, laminations, however, are made up of four ieces each; two of these pieces being of so t wood of low specific gravity (usually spruce). These two light portions, 2, '3 and 4:, of each intermediate lamination are similar to each other and joined together by a ub. The intermee' diagonal scarf at the hub, in the same manner as the hard wood laminations, 1 and 5. The outer" extremities, however, of these in terior I soft wood portions are formed of pieces 8, 9 and 10, of hard, heavy, and durable wood. ,These pieces 8, 9 and 10, are secured to the extremities by the inner soft portions, 2, 3, and 4, respectively, by long slanting scarfed joints; With this arrangement 0 the wood, the propeller is formed of a relatively light inner core or .filler, surrounded and protected at all edges and ex-. posed portions of the blade and hub by the harder, heavier, and more durable material. in constructing a propeller of the kind I have described, the corresponding pieces forming each lamination are selected from adjacent portions of the same board,, and after placing one above the other they are sawed out together to the precise profile form ,whioh they will have in the finished propeller. The hard wood portions for the extremities of the inner laminations are sawed out, each pair together,'in a similar manner. Fig. 3 shows one of the inner laminations with the hard Wood extremities ready to be glued on, and the joint ready to be made at thehub. After the two sides orhalf laminations have been prepared, a hole is bored in the center of the hub portion of each, andnumerous similar holes arebored at regular intervals throughout the length of each half lamination. These holes are so arranged that when the pieces are assembled in the propeller in their correct relation, the holes in the adjoin-in laminations willregi'ster correctly for t e insertion of screws to bind them together,.as in Fig. 4, after an adequate coating of glue or cement has been applied to the overlappin portions. A bench or slab, 20, is provi ed with a perpendicular bolt, 21. The prepared half lam- Patented only 25, 1911 inations are laced, one at a time, upon the slab with the olt rejecting upward through the holes in the ub portions, the laminations for eachblade being alternately placed, and glue or cement being laid between their joints. Screws are then inserted through the registering holes in each blade, drawing. all joints together and holding them securely until the glue is .set. V A suitable block or I washer, 22, is laid upon the hub portion and the nut, 23, screwed down firmly'to clam all the scarfs and laminations in the hu securely together. For convenience in designing the laminations, theends, 24, of
odges and each blade are left square, as shown by the sultingyeffect as shown by Fig. 5 where the ,sh'a.ded oaken portions, 26, 27 and 28, lie underthewhite spruceportions where they are joined on. InFig. 6 the arrangement of the oaken extremities is alternate, the portion 32,0Verlapping the spruce portion 34 and the portion 33 underlapping 35. After the inner set of laminations has been secured together by the bolt and screws in their correct relation and the glue has set, the screws are removed and the holes are reamed out for the reception of hard wood dowels tightly inserted with glue. This leaves the rough propeller formed of stepped laminations which are then carved down to a smooth and even surface as indicated in Fig. 4, leaving the profile of each lamination, however, substantially unchanged. Hard wood veneers, 12, are secured to each face of the hub with the grain of the wood transversely placed, insuring greater strength and security to the hub portion. With the corners of the blades removed and all surfaces smoothly polished, the propeller is ready for use.
Peculiar advantages appertain' from the form of construction I have described, in which the heavier and more durable wood is placed at the extremities of the blades. Itis not new to arrange alternatelylaminations of hard and soft wood, in which the soft Wood is continuous throughout the full length of the lamination to the extremity of the blade. Using the hard wood extremities, however, placed upon the inner laminations. twopeculiar advantagesaccrue. First the extremities of the blade being formed entirely of hard and durable wood, are far more resistant to the extreme wear to'which these portions of the blades are subjectedin handling as well as in actual use, there being no soft, portions whatever inthe region of the extremities of the blades that would be exposed to damaging influences. A less obvious but even moreimportant result, lies in the fact that with the all hard wood extremities, the radius of gyration of the revolving blade is at a much greater distance from the center than in any other construction. This contributes very materially to the balancing or fly-wheel effect of the propeller. Many aviators prefer a heavy propeller, some of them preferring the heaviest of white oak throughout, on account of its benefit as a fly-wheel upon the engine upon which it is attached. By the use of the heavy oak extremities, with a.
'spruce interior, substantially the same flywheel eflect can be produced and at a considerable saving in weight as compared with the employment of heavy wood throughout.
Besides its very obvious advantages from the mechanical standpoints of durability and fly-wheel effect, this form of construction lends itself to the production of very popular and attractive designs.
Having now fully described my improved construction, what I claim is: 1
1. A laminated propeller consisting of interior laminations of soft wood, exterior laminations of hard wood, and hard wood portions forming the extremities of the interior laminati ons.
2. A laminated propeller consisting of interior laminations of soft wood, exterior laminations of hard wood, and hard wood portions forming the extremities of the interior laminations, the hard wood extremities being joined to the interior laminations by long slanting scarfs.
3. A propeller lamlnation comprising a central portion of light material and a peripheral portion of heavy material.
4. A propeller lamination comprising a central portion of light material and a peripheral portion of heavy material, the two portions being joined together by a long, slanting scarf.
5. A propeller lamination for two blades comprising two similar interior portions of light wood scarfed together at the hub and two similar peripheral portions of heavy wood scarfed to the extremities of the interior portions.
In testimony whereof I aflix my signature 1n the presence of two w tnesses.
SPENCER HEATH.
Witnesses:
N. [CURTIS LAMMOND, N. E. COSTELLO.
US60872811A 1911-02-15 1911-02-15 Propeller. Expired - Lifetime US998897A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4164061A (en) * 1977-08-24 1979-08-14 Bronovsky Grigory A Method of making rotor blades of radial-axial hydraulic machines
US4653985A (en) * 1983-11-18 1987-03-31 Moulded Plywood Products Pty. Ltd. Fan blade
WO2019125778A1 (en) 2017-12-19 2019-06-27 Wing Aviation Llc Fiber sheet stacked rotor design

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4164061A (en) * 1977-08-24 1979-08-14 Bronovsky Grigory A Method of making rotor blades of radial-axial hydraulic machines
US4653985A (en) * 1983-11-18 1987-03-31 Moulded Plywood Products Pty. Ltd. Fan blade
WO2019125778A1 (en) 2017-12-19 2019-06-27 Wing Aviation Llc Fiber sheet stacked rotor design
CN111511641A (en) * 2017-12-19 2020-08-07 Wing航空有限责任公司 Fiber sheet stacked rotor design
EP3728025A4 (en) * 2017-12-19 2021-09-08 Wing Aviation LLC Fiber sheet stacked rotor design
US11214356B2 (en) 2017-12-19 2022-01-04 Wing Aviation Llc Fiber sheet stacked rotor design
AU2018390426B2 (en) * 2017-12-19 2022-02-17 Wing Aviation Llc Fiber sheet stacked rotor design
EP4253038A3 (en) * 2017-12-19 2023-12-20 Wing Aviation LLC Fiber sheet stacked rotor design

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