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Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-009/00
출원번호 UP-0086084 (2005-03-22)
등록번호 US-7596940 (2009-10-20)
발명자 / 주소
  • Fint, Jeffry A.
  • Hankins, Michael B.
  • Jew, Myron L.
  • Ulmer, Donald G.
  • Wherley, Brian L.
  • Romine, William D.
  • Kuck, Frederick M.
  • Ades, Douglas S.
출원인 / 주소
  • Pratt & Whitney Rocketdyne, Inc.
대리인 / 주소
    Carlson & Gaskey & Olds PC
인용정보 피인용 횟수 : 3  인용 특허 : 24

초록

A method of fabrication of a rocket engine nozzle assembly using pressure brazing generally includes initially assembling a rocket engine nozzle liner into a rocket engine nozzle jacket for a rocket engine nozzle assembly. The rocket engine nozzle assembly may then be sealed. Prior to pressure braz

대표청구항

What is claimed is: 1. A rocket engine nozzle comprising: a rocket engine nozzle jacket; and a rocket engine nozzle liner comprises a multiple of liner pieces, the rocket engine nozzle liner having a plurality of channels, the space between each channel defining a land, and the rocket engine nozzle

이 특허에 인용된 특허 (24)

  1. Weeks,Jack L, Advanced L-channel welded nozzle design.
  2. Wherley, Brian Leigh; Fisher, Steven C.; Litt, Amardeep, Combustion chamber having a multiple-piece liner and associated assembly method.
  3. H채ggander,Jan, Component for being subjected to high thermal load during operation and a method for manufacturing such a component.
  4. Blaum Mario ; Hetzler Steven Robert ; Jaquette Glen Alan ; Kabelac William John, Defect tolerant binary synchronization mark.
  5. Massoudi Firooz, Device and method for detecting synchronization patterns in CD-ROM media.
  6. Ho Son Hong ; Nguyen Hung Cao ; Tran Phuc Thanh, Error-tolerant sync detection for DVD optical disks using programmable sequence of sync marks.
  7. Zook Christopher P., Fault tolerant sync mark detector for comparing a sign and magnitude of a detected sequence to a target sync mark in sam.
  8. Reed David E. ; Bliss William G., Fault tolerant sync mark detector for synchronizing a time varying sequence detector in a sampled amplitude read channel.
  9. Lundgren, Jan, Method for manufacturing outlet nozzles for rocket engines.
  10. Lundgren, Jan, Method for manufacturing outlet nozzles for rocket engines.
  11. Lundgren, Jan, Method for manufacturing outlet nozzles for rocket engines.
  12. Semenov Viktor Nikonorovich,RUX ; Grigoriev Anatoly Ivanovich,RUX ; Derkach Gennady Grigorievich,RUX ; Katorgin Boris Ivanovich,RUX ; Chvanov Vladimir Konstantinovich,RUX ; Movchan Jury Vasilievich,R, Method for producing a welded-brazed combustion chamber.
  13. Schnoor Richard J. (Jupiter FL) Surls Michael M. (Jupiter FL), Method of making cooled rocket combustion chamber construction.
  14. Fisher Steven C. (Simi CA) Adams Theodore C. (Simi CA) Stangeland Maynard L. (Thousand Oaks CA) Rietdyk Jacob (Alta Loma CA) Winans Paul R. (Thousand Oaks CA), Method of making rocket engine combustion chamber utilizing “slide in”port liner.
  15. Pellet Marc (Vernon FRX), Method of manufacture of an enclosure containing hot gases cooled by transportation, in particular the thrust chamber of.
  16. Vandendriessche Georges (Vernon FRX), Method of manufacturing the wall of a combustion chamber, in particular for a rocket engine, and a combustion chamber ob.
  17. Niino Masayuki (No. 110 ; 1 Midorigahama 9-chome Sendai JPX) Suzuki Akio (No. 110 ; 1 Midorigahama 9-chome Shibata JPX) Yatsuyanagi Nobuyuki (No. 110 ; 1 Midorigahama 9-chome Shibata JPX) Kumakawa Ak, Method of producing rocket combustors.
  18. Niino Masayuki (No. 110 ; 1 Midorigahama 9-chome Sendai JPX) Yatsuyanagi Nobuyuki (No. 110 ; 1 Midorigahama 9-chome Shibata JPX) Kumakawa Akinaga (No. 110 ; 1 Midorigahama 9-chome Souma JPX) Suzuki A, Method of producing rocket combustors.
  19. Bales Daniel A. (Palm City FL) Joyce James R. (Jupiter FL), Method of simultaneously forming rocket thrust chamber cooling tubes.
  20. Hawkinson Elden L. (West Hills CA), Production method for a channeled wall thrust nozzle.
  21. Haggander,Jan, Rocket engine member and a method for manufacturing a rocket engine member.
  22. Häggander, Jan; Boman, Arne, Rocket engine member and method for manufacturing a rocket engine member.
  23. Zook Christopher P. ; Glover Neal ; Armstrong Alan J., Thermal asperity compensation using multiple sync marks for retroactive and split segment data synchronization in a magn.
  24. Schmidt Guenther (Taufkirchen DEX) Schmid Peter (Munich DEX), Wall surface structure having an improved radiant heat discharge capability.

이 특허를 인용한 특허 (3)

  1. Gradl, Paul R.; Reynolds, David Christopher; Walker, Bryant H., Freeform deposition method for coolant channel closeout.
  2. Macelroy, Bill, Methods for the controlled reduction of turbine nozzle flow areas and turbine nozzle components having reduced flow areas.
  3. Macelroy, Bill, Turbine nozzle components having reduced flow areas.
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