$\require{mediawiki-texvc}$
  • 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"

특허 상세정보

Apparatus for aircraft with high peak power equipment

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-006/08    F02C-003/13    F02C-007/36    F02C-007/32    F02C-007/00    B64D-013/06    B64D-041/00   
출원번호 US-0667079 (2012-11-02)
등록번호 US-9328661 (2016-05-03)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Lenart, Robert P.
인용정보 피인용 횟수 : 0  인용 특허 : 19
초록

An apparatus is provided for supplying electrical power and cooling for an aircraft. The apparatus includes a cooling turbine coupled to a shaft, a compressor coupled to the shaft, and including an input for receiving engine bleed air or ambient air, and an output for discharging compressed air, a flywheel coupled to the shaft, a power turbine coupled to the shaft, and a starter generator coupled to the shaft between the compressor and the power turbine.

대표
청구항

1. An apparatus for providing electrical power and cooling for an aircraft, the apparatus comprising: a cooling turbine connected to a shaft;a compressor connected to the shaft, and including an input for receiving engine bleed air or ambient air, and an output for discharging compressed air;a flywheel connected to the shaft;a power turbine connected to the shaft; anda starter generator connected to the shaft between the compressor and the power turbine, wherein during periods of transient or peak power requirements, kinetic energy stored in the flywheel...

이 특허에 인용된 특허 (19)

  1. Christoff William J. (Thousand Oaks CA). Aircraft environmental control system with auxiliary power output. USP1985034503666.
  2. Hoppe,Richard J.. Aircraft starter/generator electrical system with mixed power architecture. USP2006107116003.
  3. Farkas,Otto. Backup power system. USP2006057042108.
  4. Fucke,Lars; Daggett,David L.. Combined fuel cell aircraft auxiliary power unit and environmental control system. USP2008067380749.
  5. Bruno, Louis J.; Lents, Charles E.; Sahm, Michael K.; Thresher, Wayne A.. Electric power and cooling system for an aircraft. USP2005016845630.
  6. Langlois, Olivier; Roboam, Xavier; Piquet, Hubert. Electrical emergency source device located on an aircraft. USP2010047692331.
  7. Shander, Mark S.; Cote, Richard A.; Drake, Michael L.; Carter, III, Howard; Peters, John T.; Ng, Casey Y. K.; Hoag, Michael S.; Paterson, John T.. Electrical systems architecture for an aircraft, and related operating methods. USP2010037687927.
  8. Ho, Yuhang. Environmental control system for an aircraft. USP2005096948331.
  9. Lui, Clarence W; Ho, Yu Hang; Lee, Chris. Flexible power and thermal architectures using a common machine. USP2009127624592.
  10. Woodhouse Geoffrey D. (Prescott AZ). Fully integrated environmental and secondary power system. USP1996025490645.
  11. Bates Bradford ; Belaire Richard C. ; Stephan Craig Hammann. Hybrid electric propulsion system using a dual shaft turbine engine. USP1998065762156.
  12. Kern,John Michael; Wiegman,Herman Lucas Norbert. Integrated electrical power extraction for aircraft engines. USP2008127468561.
  13. Claeys Henry M. (Lomita CA) Clarke Kathrine J. (Hermosa Beach CA) Matulich Dan S. (Rolling Hills Estates CA). Integrated power and cooling environmental control system. USP1995085442905.
  14. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  15. Ho, Yu-Hang. Magnetically coupled integrated power and cooling unit. USP2004086776002.
  16. Cronin Michael J. (Sherman Oaks CA). Multi role primary/auxiliary power system with engine start capability for aircraft. USP1985014494372.
  17. Cronin Michael J. (Sherman Oaks CA). Multifunction power system for an aircraft. USP1987084684081.
  18. Glaze Stanley G. (Kingswinford GB3). System for operating aircraft flight controls. USP1992045104062.
  19. Breit, Joseph S.; Szydlo Moore, Joanna A.; Lorhammer, Kurt. Vehicular power distribution system and method. USP2009067550866.