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Compact multimission aircraft propulsion simulator 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • G01L-003/00
출원번호 US-0860032 (1977-12-12)
발명자 / 주소
  • West Harrison (Cincinnati OH) Delaney Bobby R. (Cincinnati OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 36  인용 특허 : 0

초록

A compact apparatus for simulating the in-flight aerodynamic performance of a multimission aircraft propulsion system of the gas turbine engine variety having an external envelope of a reduced size in relation to the engine to be simulated. The apparatus includes a turbine driven by externally gener

대표청구항

A compact multipurpose aircraft propulsion simulator for simulating the in-flight aerodynamic characteristics of a gas turbine engine comprising: a flow inlet sized to a reduced size linear scale in relation to the engine to be simulated; a compressor sized to pressurize a flow of air from said inle

이 특허를 인용한 특허 (36)

  1. Crutchfield, Jeffrey M; Davies, Daniel O; Peterson, Ross H; Harris, Mark M; Marshall, Natalie L, Advanced hot section materials and coatings test rig.
  2. Davies, Daniel O; Qader, Khalil O; Brostmeyer, Joseph; Wilson, Jack W; Ebert, Todd A, Advanced hot section materials and coatings test rig.
  3. Davis, Jr., Lewis Berkley; Day, Scott Arthur; Jordan, Jr., Harold Lamar; Morgan, Rex Allen, Application of combined probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods.
  4. Davis, Jr., Lewis Berkley; Day, Scott Arthur; Jordan, Jr., Harold Lamar; Morgan, Rex Allen, Application of combined probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods.
  5. Morgan, Rex Allen; Davis, Jr., Lewis Berkley; Day, Scott Arthur; Jordan, Jr., Harold Lamar, Application of combined probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods.
  6. Davis, Jr., Lewis Berkley; Day, Scott Arthur; Jordan, Jr., Harold Lamar; Morgan, Rex Allen, Application of probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods.
  7. Davis, Jr., Lewis Berkley; Day, Scott Arthur; Healy, Timothy Andrew; Jaiven, Rebecca Kathryn; Jordan, Jr., Harold Lamar; Morgan, Rex Allen, Combined probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods.
  8. Karpman, Boris; Meisner, Richard P., Compact aero-thermo model base point linear system based state estimator.
  9. Karpman, Boris; Niemczycki, Thomas; Dinsmore, Ian Michael; Sembiante, David; Luppold, Robert H., Compact aero-thermo model based control system.
  10. Karpman, Boris; Meisner, Richard P., Compact aero-thermo model based degraded mode control.
  11. Karpman, Boris; Dinsmore, Ian Michael; Meisner, Richard P.; Shade, John L., Compact aero-thermo model based engine material temperature control.
  12. Karpman, Boris; Meisner, Richard P.; Donald, Matthew; Case, Thomas E., Compact aero-thermo model based engine power control.
  13. Karpman, Boris; Dinsmore, Ian Michael; Neisner, Richard P.; Shade, John L., Compact aero-thermo model based tip clearance management.
  14. Karpman, Boris; Meisner, Richard P.; Dhingra, Manuj, Compact aero-thermo model real time linearization based state estimator.
  15. Karpman, Boris; Shishkin, Serge L., Compact aero-thermo model stabilization with compressible flow function transform.
  16. Childers, Scott Andrew; Ekanayake, Sanji; Thompson, Brett Matthew, Control system for can-to-can variation in combustor system and related method.
  17. Ellis, Sean P; Challener, Mark G, Engine performance model.
  18. Blanchard, Stephane Pierre Guillaume; Cameriano, Laurent Bernard; Dakowski, Mathieu; Page, Alain Pierre, Exhaust cone for channeling a stream of gas downstream from a turbine.
  19. Reynolds, Bruce David; Nolcheff, Nick, Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereof.
  20. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.
  21. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A., Isentropic compression inlet for supersonic aircraft.
  22. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.
  23. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.
  24. Conners, Timothy R., Low shock strength inlet.
  25. Conners, Timothy R., Low shock strength inlet.
  26. Conners, Timothy R., Low shock strength propulsion system.
  27. Conners, Timothy R., Low shock strength propulsion system.
  28. Davis, Jr., Lewis Berkley; Day, Scott Arthur; Healy, Timothy Andrew; Jaiven, Rebecca Kathryn; Jordan, Jr., Harold Lamar; Morgan, Rex Allen, Machine-specific combined probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods.
  29. Davis, Jr., Lewis Berkley; Day, Scott Arthur; Healy, Timothy Andrew; Jordan, Jr., Harold Lamar; Morgan, Rex Allen, Machine-specific probabilistic control in gas turbine tuning for power output-emissions parameters, related control systems, computer program products and methods.
  30. Sawada, Hideo; Kunimasu, Tetsuya, Method and apparatus for reducing pressure fluctuations in supersonic wind tunnel circuit.
  31. Chan,Jeffrey; Reinker,John Karl; Sharma,Suresh, Method and system for analyzing performance of a turbine.
  32. Brostmeyer,Joseph D; Wilson, Jr.,Jack W; Ebert,Todd A, Process and apparatus for testing a material under a high temperature and pressure environment.
  33. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Supersonic aircraft jet engine installation.
  34. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L., Supersonic aircraft with spike for controlling and reducing sonic boom.
  35. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L., Supersonic aircraft with spike for controlling and reducing sonic boom.
  36. Badenhorst, Sean Michael Johl, System and method for delivering air.
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