US3914969A - Apparatus for forming dished ion thruster grids - Google Patents

Apparatus for forming dished ion thruster grids Download PDF

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US3914969A
US3914969A US462903A US46290374A US3914969A US 3914969 A US3914969 A US 3914969A US 462903 A US462903 A US 462903A US 46290374 A US46290374 A US 46290374A US 3914969 A US3914969 A US 3914969A
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grids
grid
base member
dished
blanks
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US462903A
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Bruce A Banks
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National Aeronautics and Space Administration NASA
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National Aeronautics and Space Administration NASA
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00Using plasma to produce a reactive propulsive thrust
    • F03H1/0037Electrostatic ion thrusters
    • F03H1/0043Electrostatic ion thrusters characterised by the acceleration grid
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D26/00Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
    • B21D26/02Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
    • B21D26/021Deforming sheet bodies
    • B21D26/025Means for controlling the clamping or opening of the moulds
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D26/00Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
    • B21D26/02Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
    • B21D26/053Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure characterised by the material of the blanks
    • B21D26/059Layered blanks
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J19/00Details of vacuum tubes of the types covered by group H01J21/00
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J2893/00Discharge tubes and lamps
    • H01J2893/0001Electrodes and electrode systems suitable for discharge tubes or lamps
    • H01J2893/0012Constructional arrangements
    • H01J2893/0019Chemical composition and manufacture
    • H01J2893/0022Manufacture

Definitions

  • This invention is concerned with apparatus for forming curved grids.
  • the invention is particularly directed to improving apparatus used in the fabrication of matched pairs of dished grids having high percentage open areas for ion thruster accelerator systems.
  • Electron bombardment ion thrusters are being considered for a variety of space missions for which the optimum specific impulse is between 2000 and 3000 seconds. Achievement of this optimum specific impulse with a thruster having a double grid accelerator system at the desired thrust density and thruster efficiency requires a screen grid that is less than 0.5 mm thick and has a high open area fraction, preferably in excess of 0.7. A grid-to-grid spacing of about 0.25 to 0.75 mm must be maintained over the entire grid system. The ion extraction system must also survive both the launch environment and repeated thermal cycling in space.
  • Accelerator systems having closely spaced grids that have been dished to a hemispheroidal configuration are used without grid supports to satisfy the requirements imposed by near term missions.
  • To obtain uniform small grid spacing between 0.25 and 0.75 mm requires that the contours of the adjacent surfaces of the screen and accelerator grids be nearly identical. Any local irregularity must occur at the same location and to the same degree in both grids.
  • Fabrication apparatus which dish both grids simultaneously tend to minimize grid spacing variations.
  • Numerous devices have been employed in attempts to fabricate dished accelerator grid systems. These include machines for spinning, hot and cold pressing, and hammering. However, irregularities in the resulting grid contours have been so severe that the grids could not be successfully used in a closely spaced system.
  • a hydroforming press has also been proposed for fabricating the grids. This machine inflates the grids individually into a female cavity. With this machine each grid is dished separately, and irregularities in thickness result in nonmatching contours in the screen grid and accelerator grid. This produces uneven spacing between the grids which is undesirable because of ion focusing and electrical breakdown problems.
  • Hydroforming into a female die results in dished grid contours which are different from the female die because of the spring back in the grid material. Such hydroforming is done with a minimal amount of edge clamping of the grid to be dished. This produces a random edge slippagewhich causes wrinkles to be produced in the dished grids.
  • Dishing can also be achieved by simply hydroforming a single grid with no backing sheet. However, this reduces the amount of dish depth possible because catastrophic rupture failure occurs. This further prevents the hydroforming of dished accelerator grids having high open areas.
  • Another object of the invention is to provide apparatus for producing well matched molybdenum grids having space variations of less than 0.1 mm.
  • Another object of the invention is to provide a pair of grids that are uniformly dished to a hemispheroidal configuration.
  • FIG. 1 is a vertical section view of apparatus constructed in accordance with the invention showing an assembly of grid blanks and metal sh-ets prior to dishmg;
  • FIG. 2 is a vertical section view similar to FIG. 1 showing the assembled grid blanks and metal sheets after dishing;
  • FIG. 3 is a vertical section view of an alternate embodiment of the apparatus shown in FIGS. 1 and 2.
  • FIG. 1 a screen grid 10 and an accelerator grid 12 in the form of perforated sheets that are substantially flat prior to dishing.
  • the two perforated sheets are molybdenum.
  • the screen grid 10 preferably has a thickness of less than about 0.5 mm.
  • This screen grid has a high open area fraction, preferably in excess of 0.7.
  • the accelerator grid 12 is usually thicker than the screen grid 10. Accelerator grids having thicknesses up to about 0.75 mm have been satisfactory.
  • the accelerator grid 12 has less open area than the screen grid 10. The percentage open area may be as low as 50% in some accelerator grids.
  • the grid blanks l and 12 may be separated by a metal sheet 14 that is impervious.
  • a stainless steel sheet 14 having a thickness of about 0.4 mm has been satisfactory.
  • a second impervious metal sheet 16 covers the accelerator grid 12 to prevent catastrophic rupture.
  • the assembly of grid blanks and metal sheets is placed on an elastic sheet 18 which covers a rigid base plate 20.
  • the elastic sheet 18 may be either rubber or plastic.
  • a metal clamping ring 22 is placed on top of the solid metal sheet 16 so that the ring 22 is in engagement with a marginal peripheral surface portion of the metal sheet 16.
  • a plurality of clamping bolts 24 engage both the metal ring 22 and the base plate 20 to maintain the clamping ring in engagement with the marginal peripheral surface portion of a top metal sheet 16.
  • a pretuberance on the ring 22 mates with an aligned depression in the base plate 20. This clamps the p-ripheral edges of the grids and metal sheets to prevent random slippage during dishing.
  • a centrally disposed passage 26 is placed in communication with a fluid line 28 by a fitting 30.
  • the end of the line 28 opposite the fitting 30 is connected to a source 32 of high pressure fluid through a valve 34.
  • the source 32 is pressurized by a pump which is not shown.
  • the fluid is preferably a liquid, and satisfactory results have been obtained when the source 32 contains water under high pressure.
  • the fluid is removed from the space between the deformable sheet 18 and the base plate 20.
  • the clamping 24 bolts are then removed to release the metal ring 22.
  • the sheets and grids can then be removed from the base plate 20 and stress relieved.
  • Stress relieving is achievedby heating the matched pair of dished grids to a temperature of about l750 F in matched dies. The grids are maintained at this temperature in the matched dies for about one hour. During this stress relieving an inert gas, such as helium or argon, is provided to the space around the grids to prevent oxidation.
  • an inert gas such as helium or argon
  • the impervious metal sheet 14 is only required when the grid blanks 10 and 12 have high percentage open areas to prevent the metal of the grid 10 from being forced into the opening in the grid 12. When the open area fraction is less than about 0.7 the separating sheet 14 need not be used. Also, if the upper grid 12 is of a much lower open area than the lower grid 10 the metal sheet 14 between the grids can be omitted. Omission of the metal sheet 14 facilitates the aligning of the holes in the two grids.
  • grid alignment is achieved by first matching the holes in the grids.
  • the two grid sheets with holes aligned are then placed on the metal sheet 14.
  • a plurality of holes are then drilled through all three assembled sheets.
  • the impervious metal sheet 14 is then inserted between the grid sheets 10 and 12 with suitable fasteners being passed through the match drilled holes to maintain the alignment of the grid apertures.
  • an intermediate step can be added by hydroforming with the two grids and metal sheets into an intermediate female die 36.
  • This die has a geometry which more uniformly distributes the elongation as shown in FIG. 3.
  • a photoresist can be deposited on impervious grid blanks which are then hydroformed in accordance with the invention.
  • the resulting dished blanks then have the holes chemically etched followed by simultaneous stress relieving.
  • both metal sheets 14 and 16 can be omitted.
  • This embodiment is used when the spring back variation due to differences in open areas must be eliminated.
  • This embodiment is also used where discontinuities in the open areas might cause tearing of the grids during hydroforming because of stress concentrations.
  • Apparatus for forming matched pairs of dished grids having high open areas to substantially hemispheroidal configurations for ion thruster accelerator systems from substantially flat grid blanks comprising a base member for supporting a pair of said grid blanks to substantial alignment,
  • Apparatus for forming matched pairs of dished grids as claimed in claim 5 including an intermediate female die in the ring for distributing the elongation of the grids during dishing.

Abstract

An impervious metal sheet is placed on top of a pair of flat grid blanks which are clamped together at their edges. An elastic sheet contacts the bottom grid blank, and a second impervious metal sheet is inserted between the two grid blanks if the grids have high percentage open areas. All of the blanks and sheets are dished simultaneously by forcing fluid to inflate the elastic sheet. The dished grids are also stress relieved simultaneously.

Description

United States Patent Banks Oct. 28, 1975 APPARATUS FOR FORMING DISHED ION 1,329,969 2/1920 Harrison 72/63 THRUSTER GRIDS 2,284,773 6/1942. Sivian et a1. 72/63 7 2,344,743 3/1944 Smith, Jr..... 72/63 Inventori Bruce Banks, Olmsted P 3,646,653 3/1972 Richard 72/54 Oh1o 3,670,546 6/1972 DeLaSierra 72/63 [731 Assigneel The s; i f g g FOREIGN PATENTS OR APPLICATIONS 5&3? g i' f g i 430,321 3/1934 United Kingdom 72 54 Administration Office of General Counsel-Code GP, Wa hingto Primary Examiner-Milton S. Mehr D C Attorney, Agent, or FirmN. T. Musial; G. E. Shook; 22 Filed: Apr. 22, 1974 John Mannmg;
21 A 1. No.: 462,903 1 pp 57 1 ABSTRACT Related US. Application Data A t h t l d t f n impervious me a s ee 1s p ace on op o a pair [62] gg g fg i 352381 1973 of flat grid blanks which are clamped together at their edges. An elastic sheet contacts the bottom grid blank, 52 US. Cl. 72 63; 72 363; 29 421- and a second impervious metal Sheet is 1 l 4 4 tween the twogrid blanks if the grids have high per- 51 Int. 01. B21D 22/12; 13211) 26/04 Centage areas- I [58] Field of Search 72/54, 63, 363; 29/421 All of the blanks and sheets are dished simultaneously by forcing fluid to inflate the elastic sheet. The dished [56] References Cited grids are also stress relieved simultaneously.
UNITED STATES PATENTS 6 Claims,3 Drawing Figures 91,813 6/1869 Baeuerle 72/363 APPARATUS FOR FORMING DISHEI) ION THRUSTER GRIDS ORIGIN OF THE INVENTION The invention described herein was made by an employee of the United States Government and may be manufactured or used by or for the Government without the payment of any royalties thereon or therefor.
RELATED APPLICATION This application is a division of copending application Ser. No. 352,381 which was filed Apr. 18, 1973, now U.S. Pat. No. 3,864,797.
BACKGROUND OF THE INVENTION This invention is concerned with apparatus for forming curved grids. The invention is particularly directed to improving apparatus used in the fabrication of matched pairs of dished grids having high percentage open areas for ion thruster accelerator systems.
Electron bombardment ion thrusters are being considered for a variety of space missions for which the optimum specific impulse is between 2000 and 3000 seconds. Achievement of this optimum specific impulse with a thruster having a double grid accelerator system at the desired thrust density and thruster efficiency requires a screen grid that is less than 0.5 mm thick and has a high open area fraction, preferably in excess of 0.7. A grid-to-grid spacing of about 0.25 to 0.75 mm must be maintained over the entire grid system. The ion extraction system must also survive both the launch environment and repeated thermal cycling in space.
These factors combine to impose a difficult mechanical problem on the ion thruster accelerator system. Techniques such as holding the grids in tension, supporting the screen grid from the mercury vapor distributor manifold, adding stiffener ribs, and using interelectrode supports have been proposed for the ion extraction systems of thrusters utilized in these missions. However, individual problems have been encountered with each of these techniques.
Accelerator systems having closely spaced grids that have been dished to a hemispheroidal configuration are used without grid supports to satisfy the requirements imposed by near term missions. To obtain uniform small grid spacing between 0.25 and 0.75 mm requires that the contours of the adjacent surfaces of the screen and accelerator grids be nearly identical. Any local irregularity must occur at the same location and to the same degree in both grids.
Fabrication apparatus which dish both grids simultaneously tend to minimize grid spacing variations. Numerous devices have been employed in attempts to fabricate dished accelerator grid systems. These include machines for spinning, hot and cold pressing, and hammering. However, irregularities in the resulting grid contours have been so severe that the grids could not be successfully used in a closely spaced system.
A hydroforming press has also been proposed for fabricating the grids. This machine inflates the grids individually into a female cavity. With this machine each grid is dished separately, and irregularities in thickness result in nonmatching contours in the screen grid and accelerator grid. This produces uneven spacing between the grids which is undesirable because of ion focusing and electrical breakdown problems.
Hydroforming into a female die results in dished grid contours which are different from the female die because of the spring back in the grid material. Such hydroforming is done with a minimal amount of edge clamping of the grid to be dished. This produces a random edge slippagewhich causes wrinkles to be produced in the dished grids.
Dishing can also be achieved by simply hydroforming a single grid with no backing sheet. However, this reduces the amount of dish depth possible because catastrophic rupture failure occurs. This further prevents the hydroforming of dished accelerator grids having high open areas.
SUMMARY OF THE INVENTION These problems have been solved by apparatus constructed in accordance with the present invention wherein an assembly of grid blanks is separated and covered by impervious metal sheets. This assembly is placed on top of an elastic sheet, and the assembled sheets are clamped at their edges. This prevents random slippage and forms an expansible fluid chamber. Pressurized fluid in this chamber inflates the elastic sheet which, in turn, forces the impervious sheets and grid blanks to dish to their natural contour which is approximately hemispheroidal. The impervious sheet between the grid blanks prevents distortion caused by slight misalignment of the holes in the screen and accelerator grids. The dished grids are stress relieved simultaneously in matched dies.
OBJECTS OF THE INVENTION It is, therefore, an object of the present invention to provide well matched pairs of dished screen and accelerator grids having high percentage open areas that are suitable for use as grid systems for ion thrusters.
Another object of the invention is to provide apparatus for producing well matched molybdenum grids having space variations of less than 0.1 mm.
Another object of the invention is to provide a pair of grids that are uniformly dished to a hemispheroidal configuration.
These and other objects of the invention will be apparent from the specification which follows and from the drawing wherein like numerals are used throughout to identify like parts.
DESCRIPTION OF THE DRAWING FIG. 1 is a vertical section view of apparatus constructed in accordance with the invention showing an assembly of grid blanks and metal sh-ets prior to dishmg;
FIG. 2 is a vertical section view similar to FIG. 1 showing the assembled grid blanks and metal sheets after dishing; and
FIG. 3 is a vertical section view of an alternate embodiment of the apparatus shown in FIGS. 1 and 2.
DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to the drawing, there is shown in FIG. 1 a screen grid 10 and an accelerator grid 12 in the form of perforated sheets that are substantially flat prior to dishing. The two perforated sheets are molybdenum.
The screen grid 10 preferably has a thickness of less than about 0.5 mm. This screen grid has a high open area fraction, preferably in excess of 0.7.
The accelerator grid 12 is usually thicker than the screen grid 10. Accelerator grids having thicknesses up to about 0.75 mm have been satisfactory. The accelerator grid 12 has less open area than the screen grid 10. The percentage open area may be as low as 50% in some accelerator grids.
The grid blanks l and 12 may be separated by a metal sheet 14 that is impervious. A stainless steel sheet 14 having a thickness of about 0.4 mm has been satisfactory.
A second impervious metal sheet 16 covers the accelerator grid 12 to prevent catastrophic rupture. The assembly of grid blanks and metal sheets is placed on an elastic sheet 18 which covers a rigid base plate 20. The elastic sheet 18 may be either rubber or plastic.
A metal clamping ring 22 is placed on top of the solid metal sheet 16 so that the ring 22 is in engagement with a marginal peripheral surface portion of the metal sheet 16. A plurality of clamping bolts 24 engage both the metal ring 22 and the base plate 20 to maintain the clamping ring in engagement with the marginal peripheral surface portion of a top metal sheet 16. A pretuberance on the ring 22 mates with an aligned depression in the base plate 20. This clamps the p-ripheral edges of the grids and metal sheets to prevent random slippage during dishing.
A centrally disposed passage 26 is placed in communication with a fluid line 28 by a fitting 30. The end of the line 28 opposite the fitting 30 is connected to a source 32 of high pressure fluid through a valve 34. The source 32 is pressurized by a pump which is not shown. The fluid is preferably a liquid, and satisfactory results have been obtained when the source 32 contains water under high pressure.
When the valve 34 is opened, high pressure hydraulic liquid from the source 32 passes through the line 28 and passage 26 to the bottom surface of the elastic sheet 18. This pressurized liquid inflates the sheet 18 against the bottom grid blank 10. The inflation of the sheet 18 forces the sheets 14 and 16 and grid blanks and 12 above it to dish to their natural controur as shown in FIG. 2. This configuration is approximately hemispheroidal.
During this dishing the solid metal sheet 14 between the grids l0 and 12 prevents distortion caused by slight misalignment of the holes in the screen and accelerator grids. Such distortion occurs when the grids have high percentage open areas because the metal between the apertures in the screen grid 10 is forced into the openings in the accelerator grid 12.
After the grids and sheets have been dished to the configuration shown in FIG. 2 the fluid is removed from the space between the deformable sheet 18 and the base plate 20. The clamping 24 bolts are then removed to release the metal ring 22. The sheets and grids can then be removed from the base plate 20 and stress relieved.
Stress relieving is achievedby heating the matched pair of dished grids to a temperature of about l750 F in matched dies. The grids are maintained at this temperature in the matched dies for about one hour. During this stress relieving an inert gas, such as helium or argon, is provided to the space around the grids to prevent oxidation.
It is pertinent to note that the impervious metal sheet 14 is only required when the grid blanks 10 and 12 have high percentage open areas to prevent the metal of the grid 10 from being forced into the opening in the grid 12. When the open area fraction is less than about 0.7 the separating sheet 14 need not be used. Also, if the upper grid 12 is of a much lower open area than the lower grid 10 the metal sheet 14 between the grids can be omitted. Omission of the metal sheet 14 facilitates the aligning of the holes in the two grids.
When the metal separating sheet 14 is used grid alignment is achieved by first matching the holes in the grids. The two grid sheets with holes aligned are then placed on the metal sheet 14. A plurality of holes are then drilled through all three assembled sheets. The impervious metal sheet 14 is then inserted between the grid sheets 10 and 12 with suitable fasteners being passed through the match drilled holes to maintain the alignment of the grid apertures.
DESCRIPTION OF AN ALTERNATE EMBODIMENT It is contemplated that an intermediate step can be added by hydroforming with the two grids and metal sheets into an intermediate female die 36. This die has a geometry which more uniformly distributes the elongation as shown in FIG. 3.
After the intermediate step illustrated in FIG. 3 the hydroforming is completed in the manner shown in FIGS. 1 and 2. Stress relieving is performed after the intermediate step shown in FIG. 3 without any matched dies. After the final dishing step shown in FIG. 2 stress relieving is achieved with matched dies.
While several embodiments of the invention have been illustrated and described it will be appreciated that other modifications may be made without departing from the spirit of the invention or the scope of the subjoined claims. By way of example, a photoresist can be deposited on impervious grid blanks which are then hydroformed in accordance with the invention. The resulting dished blanks then have the holes chemically etched followed by simultaneous stress relieving. When the grids are dished in this manner prior to forming the holes both metal sheets 14 and 16 can be omitted. This embodiment is used when the spring back variation due to differences in open areas must be eliminated. This embodiment is also used where discontinuities in the open areas might cause tearing of the grids during hydroforming because of stress concentrations.
What is claim is:
1. Apparatus for forming matched pairs of dished grids having high open areas to substantially hemispheroidal configurations for ion thruster accelerator systems from substantially flat grid blanks comprising a base member for supporting a pair of said grid blanks to substantial alignment,
a first substantially flat sheet of impervious metal engaging a surface of one of said grid blanks remote from said base member,
a sheet of elastic material covering a surface of said base member, said sheet of elastic material contacting the other of said grid blanks not engaging said impervious metal sheet,
a second substantially flat sheet of impervious metal interposed between said grid blanks to prevent portions of one of said pair of grids from being forced into the openings of the other of said pair of grids,
a ring contacting said first substantially flat sheet,
means for securing said ring to said base member thereby clamping the marginal peripheral portions of said assembled grid blanks and impervious sheets to hold said assembled blanks and sheets in contact with each other to prevent slippage thereof and forming an expansible fluid chamber within said ring between said elastic. material and said base member, and
means for applying fluid pressure between said elastic material and said base member. thereby inflating said elastic material into said ring whereby said assembled blanks and sheets are dished to the curvature of said inflated elastic material.
2. Apparatus for forming matched pairs of dished grids as claimed in claim 1 wherein the base member has at least one passage therethrough terminating at an aperture in the surface of said base member covered by the elastic material, and
a supply of hydraulic fluid under pressure selectively connected to said passage for introducing fluid under pressure to said elastic sheet.
3. Apparatus for forming matched pairs of dished grids as claimed in claim 1 wherein the ring has a protuberance thereon for engaging said first impervious metal sheet and deforming a portion of the assembled grid blanks into a mating depression in said base member thereby clamping the peripheral edges of the grids and metal sheets to prevent random slippage during dishing.
4. Apparatus for forming matched pairs of dished grids as claimed in claim 3 wherein the base member has a passage therein for placing the expansible chamber in communication with a source of high pressure fluid.
5. Apparatus for forming matched pairs of dished grids as claimed in claim 4 wherein the source contains hydraulic liquid,
6. Apparatus for forming matched pairs of dished grids as claimed in claim 5 including an intermediate female die in the ring for distributing the elongation of the grids during dishing.

Claims (6)

1. Apparatus for forming matched pairs of dished grids having high open areas to substantially hemispheroidal configurations for ion thruster accelerator systems from substantially flat grid blanks comprising a base member for supporting a pair of said grid blanks to substantial alignment, a first substantially flat sheet of impervious metal engaging a surface of one of said grid blanks remote from said base member, a sheet of elastic material covering a surface of said base member, said sheet of elastic material contacting the other of said grid blanks not engaging said impervious metal sheet, a second substantially flat sheet of impervious metal interposed between said grid blanks to prevent portions of one of said pair of grids from being forced into the openings of the other of said pair of grids, a ring contacting said first substantially flat sheet, means for securing said ring to said base member thereby clamping the marginal peripheral portions of said assembled grid blanks and impervious sheets to hold said assembled blanks and sheets in contact with each other to prevent slippage thereof and forming an expansible fluid chamber within said ring between said elastic material and said base member, and means for applying fluid pressure between said elastic material and said base member thereby inflating said elastic material into said ring whereby said assembled blanks and sheets are dished to the curvature of said inflated elastic material.
2. Apparatus for forming matched pairs of dished grids as claimed in claim 1 wherein the base member has at least one passage therethrough terminating at an aperture in the surface of said base member covered by the elastic material, and a supply of hydraulic fluid under pressure selectively connected to said passage for introducing fluid under pressure to said elastic sheet.
3. Apparatus for forming matched pairs of dished grids as claimed in claim 1 wherein the ring has a protuberance thereon for engaging said first impervious metal sheet and deforming a portion of the assembled grid blanks into a mating depression in said base member thereby clamping the peripheral edges of the grids and metal sheets to prevent random slippage during dishing.
4. Apparatus for forming matched pairs of dished grids as claimed in claim 3 wherein the base member has a passage therein for placing the expansible chamber in communication with a source of high pressure fluid.
5. Apparatus for forming matched pairs of dished grids as claimed in claim 4 wherein the source contains hydraulic liquid.
6. Apparatus for forming matched pairs of dished grids as claimed in claim 5 including an intermediate female die in the ring for dIstributing the elongation of the grids during dishing.
US462903A 1973-04-18 1974-04-22 Apparatus for forming dished ion thruster grids Expired - Lifetime US3914969A (en)

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US4482334A (en) * 1981-09-10 1984-11-13 Tokyo Shibaura Denki Kabushiki Kaisha Method for making CRT shadow masks
EP0147676A2 (en) * 1983-12-30 1985-07-10 International Business Machines Corporation Spherical microgrid
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US4770015A (en) * 1985-12-04 1988-09-13 Usinor Aciers Process and device for press-forming sheet material having a small elongation
US4833903A (en) * 1984-05-17 1989-05-30 Union Siderurgique Du Nord Et De L'est De La France (Usinor) Method and device for press-forming sheet metal
US4873467A (en) * 1988-05-23 1989-10-10 Kaufman Harold R Ion source with particular grid assembly
US5076085A (en) * 1991-01-03 1991-12-31 Rudy Fritsch Apparatus for forming a metallic unit having a concave portion bounded by a peripheral edge
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US5865054A (en) * 1989-08-24 1999-02-02 Aquaform Inc. Apparatus and method for forming a tubular frame member
US5992197A (en) * 1997-03-28 1999-11-30 The Budd Company Forming technique using discrete heating zones
US6006568A (en) * 1998-03-20 1999-12-28 The Budd Company Multi-piece hydroforming tool
US6098437A (en) * 1998-03-20 2000-08-08 The Budd Company Hydroformed control arm
US6209372B1 (en) 1999-09-20 2001-04-03 The Budd Company Internal hydroformed reinforcements
US6590324B1 (en) 1999-09-07 2003-07-08 Veeco Instruments, Inc. Charged particle beam extraction and formation apparatus
US20080006073A1 (en) * 2002-07-19 2008-01-10 Minoru Ishihara Metal sheet pressing method
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US4409808A (en) * 1978-03-31 1983-10-18 Swiss Aluminium Ltd. Process for the production of blisters
US4482334A (en) * 1981-09-10 1984-11-13 Tokyo Shibaura Denki Kabushiki Kaisha Method for making CRT shadow masks
WO1984003176A1 (en) * 1983-02-07 1984-08-16 Hughes Aircraft Co Self-compensating hydrostatic flattening of semiconductor substrates
EP0147676A2 (en) * 1983-12-30 1985-07-10 International Business Machines Corporation Spherical microgrid
EP0147676A3 (en) * 1983-12-30 1987-08-05 International Business Machines Corporation Spherical microgrid
US4833903A (en) * 1984-05-17 1989-05-30 Union Siderurgique Du Nord Et De L'est De La France (Usinor) Method and device for press-forming sheet metal
US4770015A (en) * 1985-12-04 1988-09-13 Usinor Aciers Process and device for press-forming sheet material having a small elongation
DE3642208A1 (en) * 1985-12-11 1987-06-25 Hitachi Ltd METHOD FOR PRODUCING WORKPIECES IN THE FORM OF SHELLS WITH A CURVED SURFACE
US4873467A (en) * 1988-05-23 1989-10-10 Kaufman Harold R Ion source with particular grid assembly
US5865054A (en) * 1989-08-24 1999-02-02 Aquaform Inc. Apparatus and method for forming a tubular frame member
US5157969A (en) * 1989-11-29 1992-10-27 Armco Steel Co., L.P. Apparatus and method for hydroforming sheet metal
US5372026A (en) * 1989-11-29 1994-12-13 Armco Steel Company Apparatus and method for hydroforming sheet metal
US5076085A (en) * 1991-01-03 1991-12-31 Rudy Fritsch Apparatus for forming a metallic unit having a concave portion bounded by a peripheral edge
US5992197A (en) * 1997-03-28 1999-11-30 The Budd Company Forming technique using discrete heating zones
US6006568A (en) * 1998-03-20 1999-12-28 The Budd Company Multi-piece hydroforming tool
US6098437A (en) * 1998-03-20 2000-08-08 The Budd Company Hydroformed control arm
US7005782B2 (en) 1999-09-07 2006-02-28 Veeco Instruments, Inc. Charged particle beam extraction and formation apparatus
US6590324B1 (en) 1999-09-07 2003-07-08 Veeco Instruments, Inc. Charged particle beam extraction and formation apparatus
US20030184206A1 (en) * 1999-09-07 2003-10-02 Viktor Kanarov Charged particle beam extraction and formation apparatus
US6774550B2 (en) 1999-09-07 2004-08-10 Veeco Instruments, Inc. Charged particle beam extraction and formation apparatus
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US20060192132A1 (en) * 1999-09-07 2006-08-31 Viktor Kanarov Charged particle beam extraction and formation apparatus
US7414355B2 (en) 1999-09-07 2008-08-19 Veeco Instruments, Inc. Charged particle beam extraction and formation apparatus
US6209372B1 (en) 1999-09-20 2001-04-03 The Budd Company Internal hydroformed reinforcements
US20080006073A1 (en) * 2002-07-19 2008-01-10 Minoru Ishihara Metal sheet pressing method
US20090078021A1 (en) * 2002-07-19 2009-03-26 Minoru Ishihara Metal sheet pressing method
US20100218584A1 (en) * 2002-07-19 2010-09-02 Minoru Ishihara Metal sheet pressing method
US20120292126A1 (en) * 2011-05-19 2012-11-22 Formtech Gmbh Method for processing a surface element

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