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특허 상세정보

Liquid oxygen gasifying system for rocket engines

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-009/48    F02K-009/46   
미국특허분류(USC) 60/257 ; 60/267 ; 60/260 ; 60/259
출원번호 US-0850259 (1997-05-05)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Friedland
인용정보 피인용 횟수 : 35  인용 특허 : 6
초록

For a liquid rocket engine including the SSME the gaseous heat exchanger that is in the liquid oxygen turbopump exit flow path that serves to gasify the liquid oxygen for pressurizing the liquid oxygen tank and the POGO is modified by changing the flow circuit to replace the liquid oxygen with high pressure hydrogen tapped off of the low pressure fuel turbopump so that hydrogen/hydrogen at a favorable pressure differential is in indirect heat relation for providing a safe environment and avoiding what may result in a catastrophic failure in the event the...

대표
청구항

[ It is claimed:] [1.] A liquid rocket engine that includes liquid oxygen and liquid hydrogen as the combustion agents comprising: a liquid oxygen turbopump including a first heat exchanger located in a turbine exit flow path of said liquid oxygen turbopump, a preburner for combining oxygen and hydrogen and creating a high pressure hydrogen rich gas to power said turbopump, said first heat exchanger being in indirect heat exchange with said high pressure hydrogen rich gas, a low pressure fuel turbopump, fluid connections for flowing low pressure hydrogen...

이 특허를 인용한 특허 피인용횟수: 35

  1. Hart, Katherine; Held, Timothy James. Automated mass management control. USP2018019863282.
  2. Hart, Katherine; Held, Timothy James. Automated mass management control. USP2014088813497.
  3. Fisher, Steven C.. Bi-propellant injector with flame-holding zone igniter. USP2005076918243.
  4. Held, Timothy James; Vermeersch, Michael Louis; Xie, Tao. Carbon dioxide refrigeration cycle. USP2015069062898.
  5. Balepin, Vladimir V.. Closed-cycle rocket engine assemblies and methods of operating such rocket engine assemblies. USP2013028381508.
  6. Fisher, Steven C.. Coaxial ignition assembly. USP2012028122703.
  7. Knight, Andrew F.. Cool gas generator and ultra-safe rocket engine. USP2005116968673.
  8. Held, Timothy James; Vermeersch, Michael Louis; Xie, Tao. Driven starter pump and start sequence. USP2013128616001.
  9. Held, Timothy James; Vermeersch, Michael; Xie, Tao. Driven starter pump and start sequence. USP2016089410449.
  10. Greene,William D.. Dual expander cycle rocket engine with an intermediate, closed-cycle heat exchanger. USP2008097418814.
  11. Kernilis, Alain; Lemoine, Nicolas; Boulet, Ludivine; Le Gonidec, Serge. Feed system and a method of suppressing the POGO effect. USP2016129528470.
  12. Kline, Korey R.; Smith, Kevin W.; Cesaroni, Anthony Joseph. Flame holder for a hybrid rocket motor. USP2004056739121.
  13. Held, Timothy J.; Miller, Jason D.. Heat engine and heat to electricity systems and methods for working fluid fill system. USP2015038966901.
  14. Held, Timothy J.; Hostler, Stephen; Miller, Jason D.; Vermeersch, Michael; Xie, Tao. Heat engine and heat to electricity systems and methods with working fluid mass management control. USP2013128613195.
  15. Held, Timothy James; Hostler, Stephen; Miller, Jason D.; Vermeersch, Michael; Xie, Tao. Heat engine and heat to electricity systems and methods with working fluid mass management control. USP2016109458738.
  16. Held, Timothy James. Heat engine cycles for high ambient conditions. USP2014108857186.
  17. Kacludis, Alexander Steven; Hostler, Stephen R.; Zakem, Steve B.. Heat engine system with a supercritical working fluid and processes thereof. USP2015089118226.
  18. Held, Timothy James. Heat engines with cascade cycles. USP2014108869531.
  19. Gurin, Michael H.. Heat pump with integral solar collector. USP2016049316404.
  20. Held, Timothy James. Hot day cycle. USP2014078783034.
  21. Gurin, Michael H.. Hybrid power systems. USP2013128616323.
  22. Kline, Korey R.; Smith, Kevin W.. Hybrid rocket motor having a precombustion chamber. USP2004016679049.
  23. Kline, Korey R.; Smith, Kevin W.. Hybrid rocket motor having a precombustion chamber. USP2004116820412.
  24. Kline, Korey R.; Smith, Kevin W.; Bales, Thomas O.. Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent. USP2004026684625.
  25. Kline, Korey R.; Smith, Kevin W.; Schmidt, Eric E.; Bales, Thomas O.. Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent. USP2003116640536.
  26. Gudmundson, Chris. Hydrogen based combined steam cycle apparatus. USP2014038671687.
  27. Vermeersch, Michael Louis; Bowan, Brett A.; Khairnar, Swapnil. Methods for reducing wear on components of a heat engine system at startup. USP2017059638065.
  28. Bowan, Brett A.. Process for controlling a power turbine throttle valve during a supercritical carbon dioxide rankine cycle. USP2017099752460.
  29. Balepin, Vladimir V.. Rocket engine. USP2004086769242.
  30. Xie, Tao; Vermeersch, Michael; Held, Timothy. Supercritical carbon dioxide power cycle for waste heat recovery. USP2016059341084.
  31. Vermeersch, Michael Louis. Supercritical working fluid circuit with a turbo pump and a start pump in series configuration. USP2015079091278.
  32. Held, Timothy James. System and method for managing thermal issues in gas turbine engines. USP2015049014791.
  33. Held, Timothy James. System and method for managing thermal issues in one or more industrial processes. USP2016099441504.
  34. Held, Timothy J.; Hostler, Stephen; Miller, Jason D.; Hume, Brian F.. Thermal energy conversion device. USP2015089115605.
  35. Held, Timothy J.; Hostler, Stephen; Miller, Jason D.; Hume, Brian F.. Thermal energy conversion method. USP2014088794002.