$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

과학기술 지식인프라 ScienceON

상세검색 다국어 입력
도움말도움말

특허 상세정보

MyON담기
내보내기

Missile thrust system and valve with refractory piston cylinder

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-009/56   
미국특허분류(USC) 137/375; 251/368; 060/254; 420/433; 148/407
출원번호 US-0216622 (2002-08-09)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Ingrassia Fisher &
인용정보 피인용 횟수 : 16  인용 특허 : 34
초록
▼

An improved pneumatic valve and a missile with an improved thrust directional valve. In one embodiment, a refractory material lining for a pneumatic valve enables better valve operation and better valve performance. A thin-wall cylindrical sleeve of rhenium or other suitable refractory metal is located inside a cylinder. A valve piston may then travel within the refractory sleeve with greater reliability and better operation. The refractory sleeve cylinder lining can be subject to high temperatures at a rapid rate and remain operational. Under such a hos...

대표
청구항
▼

1. A valve for directing propellant thrust, comprising:a refractory cylinder wall lining defining a cylinder symmetrically disposed about a longitudinal axis; and a piston disposed axially relative to the longitudinal axis and configured to slidably move within the cylinder along the longitudinal axis. 2. A valve for directing propellant thrust as set forth in claim 1, wherein the refractory cylinder wall lining is made from metal of the group consisting of rhenium, tungsten, niobium, tantalum, molybdenum, and alloys thereof.3. A valve for directing prop...

이 특허에 인용된 특허 (34)

  1. Bloch Alexander (Mnzenberg DEX) Ettl Hanns-Ulrich (Maintal DEX) Kuhn Peter (Hanau DEX). Aircraft cabin pressure control system. USP1996055520578.
  2. Wong, Paul P.; Lippold, John B.; Burgess, Glenn A.. Aircraft cabin pressurization system. USP1985114553474.
  3. Olson Robert W. (Tucson AZ). Apparatus for controlling the partial pressure of oxygen in an aircraft cabin. USP1997015590852.
  4. Andersen Blaine W. (Tempe AZ) Tervo John N. (Scottsdale AZ). Balanced-torque butterfly valve. USP1991045005804.
  5. Caruso John T. (Kenmore NY). Bimetallic valve spool. USP1982074337797.
  6. Ball Larry K. (Chandler AZ) Hines Marshall U. (Scottsdale AZ). Butterfly valve apparatus and method. USP1990114967778.
  7. Ball Larry K. (Chandler AZ) Hines Marshall U. (Scottsdale AZ) Miller Terry L. (Mesa AZ). Butterfly valve apparatus and method. USP1990104964431.
  8. Ball Larry K. (Chandler AZ). Butterfly valve method and apparatus. USP1991075029599.
  9. Tervo John N. (Scottsdale) Ball Larry K. (Chandler) Hines Marshall U. (Scottsdale AZ). Butterfly valve method and apparatus. USP1991035000213.
  10. Ball Larry K. (Chandler AZ). Butterfly valve with biased area reduction means. USP1992055113910.
  11. Davis Brian K. (Tempe AZ) Hines Marshall U. (Scottsdale AZ) Ball Larry K. (Chandler AZ) Cronenberg Stephan R. (Mesa AZ). Butterfly valve with plural-fence modulator plate. USP1992045102097.
  12. Ball Larry K. (Chandler AZ) Hines Marshall U. (Scottsdale AZ). Butterfly-type check valve. USP1990104964422.
  13. Stokes Richard F. (Phoenix AZ) Timm James D. (Tempe AZ) LaCroix Stephen R. (Scottsdale AZ) Adams Milton R. (Tempe AZ). Compressor bleed air control apparatus and methods. USP1984014428194.
  14. Ball Larry K. (Chandler AZ) Hines Marshall U. (Scottsdale AZ) Tervo John N. (Scottsdale AZ). Flight craft with fluid systems which incorporate butterfly valves, and butterfly valve methods and apparatus. USP1991115067506.
  15. Abel Stephen G. ; Ryan William F. ; Pepe Michael A. ; Silk Joseph P. ; Hopper Douglas T.. Force driven hot gas proportional thruster valve. USP2001056233919.
  16. Rix John F. (Tucson AZ). Integrated cabin pressure controller. USP1994085334090.
  17. Burkes ; Jr. William M. (McGregor TX) Miller William H. (McGregor TX). Nozzle/valve device for a ducted rocket motor. USP1984044442669.
  18. Louis Ronald J. ; Oboodi Reza. Piezo-resistive position indicator. USP2001106308723.
  19. Cleasby Kenneth G. (Cobham GB2). Pilot valves for two-stage hydraulic devices. USP1988114785839.
  20. Gilchrist Raymond T. (Tucson AZ) McCoy Kevin (Tucson AZ). Pneumatic check valve and method for making same. USP1995025386848.
  21. Abel Stephen G.. Position driven hot gas proportional thruster valve. USP2001056227247.
  22. Tseng Raymond R.. Pressure balanced poppet valve. USP2001086276125.
  23. Mitchell John D. (Phoenix AZ). Pressure regulator system. USP1984054445532.
  24. Wingett Paul. Pressure vessel bottle mount. USP2001036202674.
  25. Jensen Ron B. (Mesa AZ) Guyuax James R. (Chandler AZ). Proportional solenoid valve. USP1994105351934.
  26. Horner Mervyn H. ; Streckert Holger H.. Refractory heat transfer module. USP2000056065284.
  27. Gabrysch Leslie P. (Hewitt TX). Self compensating ducted rocket motor fuel nozzle and method for regulating fuel generation. USP1986034574586.
  28. Cheung Shek Michael. Servo-actuator with fail safe means. USP1999055899064.
  29. Sutton Trevor G. (Maricopa AZ). Small vehicle roll control and steering. USP1988104779821.
  30. Robinson Philip I. (Calabasas CA). Solar rocket absorber. USP1985074528978.
  31. Abel Stephen G. (Chandler AZ). Solenoid valve. USP1988094768555.
  32. Christensen Donald Jeffrey. Spherical chamber fluidic ball diverter valve. USP1999075927335.
  33. Vick Ralph L. (Granada Hills CA). Spool valve and seal having zero leakage. USP1984074458718.
  34. Tseng Raymond R. ; Abel Stephen G.. Two-stage, warm-gas high pressure regulator. USP1999126006780.

이 특허를 인용한 특허 피인용횟수: 16

  1. Hanlon, Casey; Geck, Kellan; Johnson, Andrew T.. Actuation assembly. USP2012128338768.
  2. Searle, Joseph M.; Christensen, Donald J.; Woessner, George T.; Gratton, Jason A.. Cutback poppet valve. USP2009107600737.
  3. Brondum, Klaus; Welty, Richard P.; Jonte, Patrick B.; Richmond, Douglas S.; Thomas, Kurt. Faucet. USP2011017866343.
  4. Brondum, Klaus; Welty, Richard P.; Jonte, Patrick B.; Richmond, Douglas S.. Faucet component with coating. USP2016079388910.
  5. Brondum, Klaus; Welty, Richard P.; Jonte, Patrick B.; Richmond, Douglas S.. Faucet component with coating. USP2018039909677.
  6. Brondum, Klaus; Welty, Richard P.; Jonte, Patrick B.; Richmond, Douglas S.. Faucet component with coating. USP2013108555921.
  7. Brondum, Klaus. Faucet with wear-resistant valve component. USP2012078220489.
  8. Olden, Thomas A.; Wrigglesworth, Walter. Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof. USP2014098826640.
  9. Olden, Thomas A.; Cavalleri, Robert J.. Modular divert and attitude control system. USP2012088242422.
  10. Olden, Thomas A.; Cavalleri, Robert J.. Pellet-loaded multiple impulse rocket motor. USP2014038667776.
  11. Abel, Steve; Tseng, Raymond R.. Pressure assisted direct drive proportional hot-gas thruster. USP2014048707675.
  12. Woessner, George T.; Abel, Stephen G.; Peck, Ronald A.; Baker, Mark H.; Christensen, Donald J.. Solid propellant burn rate, propellant gas flow rate, and propellant gas pressure pulse generation control system and method. USP2011027886519.
  13. Olden, Thomas A.; Wrigglesworth, Walter. Systems and methods for composite structures with embedded interconnects. USP2014088809689.
  14. Brondum, Klaus; Welty, Richard P.; Richmond, Douglas S.; Jonte, Patrick B.; Thomas, Kurt. Valve component for faucet. USP2012028118055.
  15. Brondum, Klaus; Welty, Richard P.; Richmond, Douglas S.; Jonte, Patrick B.; Thomas, Kurt. Valve component for faucet. USP2011017866342.
  16. Walker, Terence B.; Waghray, Akshay; Booker, Laurie A.. Wear pin assemblies for carbon-carbon composite brake systems. USP2010087766130.

IPC 상위 출원인