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특허 상세정보

Systems and methods for integrated power and thermal management in a turbine-powered aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-013/06    F02C-007/143    F02C-009/18    F02C-007/36    F02C-007/268    F02C-007/32    H02K-007/18   
출원번호 US-0923731 (2015-10-27)
등록번호 US-9534538 (2017-01-03)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    General Electric Company
인용정보 피인용 횟수 : 0  인용 특허 : 15
초록

An integrated power and thermal management system for a turbine-powered aircraft is provided. The system may comprise a power turbine, compressor, first cooling turbine, second cooling turbine, and electrical motor-generator disposed on a primary shaft. The compressor may be disposed on the primary shaft to motivate a system airflow and operably joined to the power turbine. The first cooling turbine may be rotatably disposed on the primary shaft in selective fluid communication with the compressor. The second cooling turbine may be rotatably disposed on ...

대표
청구항

1. An integrated power and thermal management system for a turbine-powered aircraft, the system comprising: a power turbine rotatably disposed on a primary shaft;a compressor rotatably disposed on the primary shaft to motivate a system airflow, the compressor being operably joined to the power turbine;a first cooling turbine rotatably disposed on the primary shaft in selective fluid communication with the compressor;a second cooling turbine rotatably disposed on the primary shaft in selective fluid communication with the first cooling turbine; andan elec...

이 특허에 인용된 특허 (15)

  1. Coffinberry, George Albert; Garrigan, Neil Richard. Adaptive power and thermal management system. USP2013098522572.
  2. Jonqueres Michel A.. Air cycle environmental control system with energy regenerative high pressure water condensation and extraction. USP1999075921093.
  3. Massey George. Electric starter system for turbine aircraft engines. USP2000026018941.
  4. Warner John L. (Simsbury CT). Environmental control system condensing cycle. USP1992025086622.
  5. Sanger Roger Reed. Environmental control system no condenser high pressure water separation system. USP2000116148622.
  6. Lui, Clarence W; Ho, Yu Hang; Lee, Chris. Flexible power and thermal architectures using a common machine. USP2009127624592.
  7. Glickstein Marvin R. (North Palm Beach FL) Dixon James T. (Jupiter FL) Podolsky Donald M. (Jupiter FL). High pressure air source for aircraft and engine requirements. USP1996045511374.
  8. Lui,Clarence; Quan,Myron A.. Indirect regenerative air cycle for integrated power and cooling machines. USP2007027171819.
  9. Lui, Clarence W. T.; Derouineau, Jean Luc; Claeys, Henry M.. Integrated environmental control and auxiliary power system for an aircraft. USP2009107607318.
  10. George E. Wilmot, Jr. ; Gregory M. Ott. Integrated thermal management and coolant system for an aircraft. USP2002076415595.
  11. Gaines,Louie T.; Auer,Peter J.; Lane,Glenn H.; Wissinger,James A.. More electric aircraft starter-generator multi-speed transmission system. USP2009017481062.
  12. Williams Kenneth R.. Multi-mode secondary power unit. USP1998095813630.
  13. Cronin Michael J. (Sherman Oaks CA). Multifunction power system for an aircraft. USP1987084684081.
  14. Thompson Robert George. Secondary power integrated cabin energy system for a pressurized aircraft. USP2001096283410.
  15. Sabatino,Daniel; Spadaccini,Louis J.; Kaslusky,Scott. Thermal management system for an aircraft. USP2007087260926.