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US4124195A Expired / Lapsed US ⏱️ 0.0 years remaining

Control valve, particularly for pulsating rocket engines

Assignee: Airbus Defence and Space GmbH
•
Filing: 1973-10-15
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Granted: 1978-11-07
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Expires: 1993-10-15
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Abstract

Abstract A control valve for a pulsating rocket engine comprises a valve seat and a movable valve part, one of which has a facing surface, of a non-deformable material, having a plurality of concentrically arranged saw-tooth shaped sealing ridges with flat sealing faces at their apices which extend perpendicular to the movement direction or force application direction. The other valve part has a facing surface of polytetrafluorethylene or polyamide which is initially smooth and plain but which, upon the first closing operation of the valve, responsive to a pressure load thereon exceeding a predetermined pressure load, is irreversibly deformed by the saw-tooth shaped sealing ridges, with flat sealing faces, of the other valve part to form therein grooves complementary to the sealing ridges. The included angle between the striking and sealing flanks of the ridges has a value such that, upon subsequent closing operations of the valve, the synthetic resin material, which has not been irreversibly deformed, can flow into the spaces between the annular sealing ridges without exceeding its irreversible deformation yield point, to form an elastic buffer.

Inventors

  • 👤 Karl Braun
  • 👤 Reinhold Tussetschlager

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 19:59
CPC Classifications
F; F16; F16K; F16K1/00; F16K1/32; F16K1/34; F16K1/42

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 233 words
A shut-off control valve, particularly for pulsating rocket engines, comprising a stationary valve seat and a moving valve part having facing surfaces interengageable responsive to movement of said valve part in a valve-closing direction, the facing surface of one of said valve seat and said moving valve part having a plurality of concentrically arranged annular sawtooth-shaped sealing ridges with relatively narrow flat sealing crests extending perpendicularly to the valve-closing direction, and having oblique planar striking flanks on each side of said crests, made of a strong material such as steel, the facing surface of the other one of said valve seat and said moving valve part being made of a relatively soft elastic synthetic resin material that, above a predetermined pressure load thereon, is irreversibly deformable, and having a continuous initially plane smooth facing surface before the first closing operation of the valve, but being irreversibly deformed, to form a facing surface which is complementary to the other facing surface, having said sealing ridges, responsive to a pressure load thereon, exceeding said predetermined pressure lead, upon initial closing of the valve, by interengagement of said facing surfaces; the included angle between said striking flanks having a value such that, upon subsequent closing operation of the valve, said elastic synthetic resin material can flow into the spaces between said annular sealing ridges without exceeding its irreversible deformation yield point, to form an elastic buffer.
Claim 2
Dependent Claim 233 words
A shut-off control valve, particularly for pulsating rocket engines, comprising a stationary valve seat and a moving valve part having facing surfaces interengageable responsive to movement of said valve part in a valve-closing direction, the facing surface of one of said valve seat and said moving valve part having a plurality of concentrically arranged annular sawtooth-shaped sealing ridges with relatively narrow flat sealing crests extending perpendicularly to the valve-closing direction, and having oblique planar striking flanks on each side of said crests, made of a strong material such as steel, the facing surface of the other one of said valve seat and said moving valve part being made of a relatively soft elastic synthetic resin material that, above a predetermined pressure load thereon, is irreversibly deformable, and having a continuous initially plane smooth facing surface before the first closing operation of the valve, but being irreversibly deformed, to form a facing surface which is complementary to the other facing surface, having said sealing ridges, responsive to a pressure load thereon, exceeding said predetermined pressure lead, upon initial closing of the valve, by interengagement of said facing surfaces; the included angle between said striking flanks having a value such that, upon subsequent closing operation of the valve, said elastic synthetic resin material can flow into the spaces between said annular sealing ridges without exceeding its irreversible deformation yield point, to form an elastic buffer.
Claim 3
Dependent Claim 21 words
A control valve, according to claim 1, wherein the angle defined between the flanks of the sealing ridges is about 120°.
Claim 4
Dependent Claim 28 words
A control valve, according to claim 1, wherein the facing surface of said other of said valve seat and said moving valve part is made of a polytetrafluoroethylene.
Claim 5
Dependent Claim 26 words
A control valve, according to claim 1, wherein the facing surface of said other of said valve seat and said moving valve part is a polyamide.

References Cited (Backward Citations)

US341345A Cited
US1234096A Cited
US3022978A Cited
FR1196263A Cited
US3145733A Cited
US3168282A Cited
US3253300A Cited
US3698427A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-11-06 1982-05-08 1982-11-07 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-11-06 1986-05-08 1986-11-07 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-11-06 1990-05-08 1990-11-07 $7700.00 Window Closed / Lapsed

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