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특허 상세정보

Rear section of jet power plant installations

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/04   
미국특허분류(USC) 060/264; 060/265; 060/271; 239/127.3
출원번호 US-0765700 (1958-09-30)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 40  인용 특허 : 0
초록

1. In a gas turbine engine having blades and an exhaust tailpipe, the combination of an exhaust cone axially mounted within the tailpipe and having its rearward end adjacent the discharge opening of the exhaust pipe with substantially all of the externally viewable surfaces of said exhaust cone formed of porous stainless steel material, means to supply cooling air to the interior of the cone for venting thereof through said porous material, a hollow strut member of airfoil configuration spanning the annular gas passageway between the exhaust tailpipe and...

대표
청구항

1. In a gas turbine engine having blades and an exhaust tailpipe, the combination of an exhaust cone axially mounted within the tailpipe and having its rearward end adjacent to discharge opening of the exhaust pipe with substantially all of the externally viewable surfaces of said exhaust cone formed or porous stainless steel material, means to supply cooling air to the interior of the cone for venting thereof through said porous material, a hollow strut member of airfoil configuration spanning the annular gas passageway between the exhaust tailpipe and ...

이 특허를 인용한 특허 피인용횟수: 40

  1. Brennan John M. (Chula Vista CA). Accessory for a turbine engine. USP1980124238092.
  2. Scott, Jonathan Ariel; Chuong, Conway. Angled cut to direct radiative heat load. USP20190310240481.
  3. Porter Kenneth W. (Mercer Island WA) McLaren Douglas (Seattle WA). Apparatus and method for minimizing engine backbone bending. USP1984094471609.
  4. Budnick, Matthew. Bumper for seals in a turbine exhaust case. USP2017119828867.
  5. Byrne, Stuart James; Delaney, Mac Patrick. Exhaust assembly center body. USP2017019551239.
  6. Johnson Joseph M. (Bothell WA) Thornock Russell L. (Seattle WA). Fixed geometry controlled entrainment ventilated convergent nozzle and method. USP1986024567960.
  7. Vo, Tuan David. Flow diverter element and assembly. USP2017129850774.
  8. Scott, Jonathan Ariel; Yeager, William. Frame junction cooling holes. USP20190310240532.
  9. Wakazono,Susumu; Ishizaka,Kouichi; Yuri,Masanori; Takahashi,Ronald. Gas turbine. USP2008087410343.
  10. Durocher, Eric; Gekht, Eugene; Lefebvre, Guy. Gas turbine engine exhaust duct ventilation. USP2010107805925.
  11. Todorovic, Predrag. Gas turbine exhaust cone. USP2014078776946.
  12. Budnick, Matthew; Chuong, Conway. Gas turbine seal assembly and seal support. USP2017129845695.
  13. Chuong, Conway; Budnick, Matthew. Gas turbine seal assembly and seal support. USP2018029903216.
  14. Todorovic, Predrag. Gas-turbine exhaust cone. USP2012118307945.
  15. Budnick, Matthew; Chuong, Conway; Scott, Jonathan Ariel. Heat shield for cooling a strut. USP2018059982561.
  16. Bandera Gianluigi (Gallarate ITX). Helicopter with a turbine power unit fitted with an exhaust screening device. USP1987124713933.
  17. Salunkhe, Anil L.; Orosa, John A.; Shteyman, Yevgeniy; Porter, Matthew R.; Han, Lijuan; Delisa, III, Matthew J.. Industrial gas turbine exhaust system with splined profile tail cone. USP2017059644497.
  18. Bilenas Jonas ; Kosson Robert ; Attard Salvatore. Infrared radiation coanda suppressor. USP2001026182440.
  19. Robertson, Daniel B.; Smith, Dudley E.; Laramee, Robert M.. Infrared suppressing exhaust system. USP2016059334060.
  20. Steyer William ; Higgins Timothy Joseph. Infrared suppressor. USP1998055746047.
  21. Mouritsen Thorvald E. (Dallas TX) Simpkin William E. (Dallas TX). Infrared suppressor device. USP1980074214441.
  22. Steyer,William; Kieffer,Christopher Marlow; Jasany,John Michael; Hoffman,Jacob. Method and apparatus for suppressing infrared signatures. USP2006016988674.
  23. Czachor, Robert P.. Methods and apparatus for minimizing thermal stresses in a centerbody. USP2003076584766.
  24. Budnick, Matthew. Mount with deflectable tabs. USP20181010087843.
  25. Liles, Jason David; Ruby, Charles T.. Multi-piece fairing for monolithic turbine exhaust case. USP2017049631517.
  26. Budnick, Matthew. Multi-ply finger seal. USP20181110138742.
  27. Vo, Tuan David; Chuong, Conway; Budnick, Matthew; Scott, Jonathan Ariel. Multi-purpose gas turbine seal support and assembly. USP20180810053998.
  28. Dionne, Luc. Passive cooling system for auxiliary power unit installation. USP2017059644538.
  29. Chew Thomas ; Steyer William ; Moore Clinton Clark ; Harrold Michael Charles. Removable baffle infrared suppressor. USP2001076253540.
  30. Scott, Jonathan Ariel; Hawke, Larry B.. Scupper channelling in gas turbine modules. USP2018029903224.
  31. Vo, Tuan David; Scott, Jonathan Ariel. Seal support disk and assembly. USP20180810060279.
  32. Vivace Robert T. (Indianapolis IN). Support and seal assembly. USP1987114706453.
  33. Sheoran,Yogendra Y.; Payne,Roger I.. System and method for dumping surge flow into eductor primary nozzle for free turbine. USP2006127152410.
  34. Coffey Clayton G. (Medicine Hat CAX) Murray Stephen B. (Montreal CAX) Bayly Donald L. (Calgary CAX). System for infrared emission suppression (sires). USP1982104355507.
  35. Sheoran, Yogendra Y.; Brown, Daniel V.; Edmonds, David H.. Tortuous path quiet exhaust eductor system. USP2003096615576.
  36. Scott, Jonathan Ariel; Veninger, Albert. Turbine exhaust case architecture. USP20180610006306.
  37. Scott, Jonathan Ariel. Turbine exhaust case multi-piece frame. USP20180810054009.
  38. Scott, Jonathan Ariel. Turbine exhaust case multi-piece frame. USP2018029890663.
  39. Yeager, William; Scott, Jonathan Ariel. Turbine frame assembly and method of designing turbine frame assembly. USP2018059982564.
  40. Whurr,John R.. Variable area nozzle. USP2007027178338.