$\require{mediawiki-texvc}$
  • 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

Redundant electrical DC power system for aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) H02J-009/00   
미국특허분류(USC) 307/064; 244/0070A; 290/0010C; 307/080
출원번호 US-0411616 (1999-10-01)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Gardere Wynne Sewell, LLP
인용정보 피인용 횟수 : 30  인용 특허 : 3
초록

A DC electrical power generation system for aircraft having primary and emergency generation systems is disclosed. The system includes a transmission driven power generator, a dedicated generator control unit and a distribution network for providing sufficient capacity to all electrical loads on the aircraft. The emergency power system includes at least one engine driven starter generators, with an associated controller unit and associated distribution network for providing sufficient backup capacity to electrical loads assigned thereto.

대표
청구항

1. A redundant DC electrical power system for an aircraft having at least two rotors mechanically driven by a common main driveshaft, comprising:a primary power system including a power generator driven by said common main driveshaft, a dedicated generator control unit and an isolated distribution network that further includes electrical busses for providing sufficient capacity to electrical loads on the aircraft; and an emergency power system including at least one engine driven starter generator with an associated controller unit and associated distrib...

이 특허를 인용한 특허 피인용횟수: 30

  1. Hoppe,Richard J.. Aircraft starter/generator electrical system with mixed power architecture. USP2006107116003.
  2. White, Jeffrey Joseph; Currier, Thomas F.. Aircraft supplemental electrical power systems and methods. USP20181010093250.
  3. Nehmeh, Jody N.. Aircraft utilities and power distribution system. USP2016059327600.
  4. Eisenhauer, Mark P.; Bourne, Frederick L.. Battery current regulation. USP2018039909502.
  5. Mares,Mircea; Liu,Zhenning. Electric load management center. USP2006027007179.
  6. Mares,Mircea. Electric load management center including gateway module and multiple load management modules for distributing power to multiple loads. USP2006037020790.
  7. Mares,Mircea; Liu,Zhenning. Electric power distribution center having a plurality of ASICS each with a voltage to frequency converter that use an RMS current value. USP2007017162653.
  8. Rozman, Gregory I; Futrell, Michael Anthony. Electric power system for a space vehicle. USP20181010103549.
  9. Aubert, Roger; Truchon, Martin; Sinusas, Eric; Boussetoua, Mohammed; Ouhrouche, Mohand; Fortin, Guy; Mercier, Carol; Perron, Jean. Electrical generator for rotating structure. USP2017089725179.
  10. Michalko,Rodney G.. Electrical starting, generation, conversion and distribution system architecture for a more electric vehicle. USP2008107439634.
  11. Derouineau,Jean Luc. Engine power extraction control system. USP2007107285871.
  12. Smiley, Alfred Russell; Strauss, Michael Peter; Cycon, James Peter. Engine starting system for rotorcraft in flight. USP2016029248907.
  13. Eisenhauer, Mark P.; Sullivan, Christopher Patrick. Fault clearing without a DC backup power source. USP2013108564914.
  14. Rozman, Gregory I.; Dooley, Kevin; Maddali, Vijay K.. Generator for gas turbine engine having DC bus fault short circuit control using a battery. USP2011017876542.
  15. Waltner, Peter James. Hybrid contingency power drive system. USP20180810040566.
  16. Arguello, Gustavo. Ignition system for a gas turbine engine. USP2009097595568.
  17. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2015028950703.
  18. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2014028657227.
  19. Bauer, Ronald P.; Stevens, Clifford G.; Betterini, William; Schroeder, Joshua N.; Webster, Robert W.. Load shedding circuit for RAM air turbines. USP2015079083201.
  20. Krenz, Michael; Wagner, Carl A.; Jacques, David L.; Finney, Adam M.. Methods for aircraft emergency power management. USP2014098829707.
  21. Greene,Leonard M.. Missile defense system and methods for evading heat seeking missiles. USP2008057370836.
  22. Eick, Chris D.; Gaines, Louie T.; Laidlaw, Mitchell J.; Benson, Dwayne M.; Portolese, Larry A.; Flaherty, Brian L.; Pearson, Wayne T.. More electric aircraft power transfer systems and methods. USP2009067552582.
  23. Gaines,Louie T.; Auer,Peter J.; Lane,Glenn H.; Wissinger,James A.. More electric aircraft starter-generator multi-speed transmission system. USP2009017481062.
  24. Sullivan, Christopher P.; Eisenhauer, Mark P.; Loch, Raymond Andrew. Multi-directional electrical power protection system. USP2017059660435.
  25. Finney, Adam M.. Multi-source emergency power optimization. USP2013048424800.
  26. Beneditz, Bruce D.; Stoneback, Russell G.; Bouton, Marc A.; Spear, Kenneth; Dickey, John A.. Power distribution assembly with redundant architecture. USP2005026856045.
  27. Rozman, Gregory I; Futrell, Michael Anthony. Power management and distribution architecture for a space vehicle. USP20181010110000.
  28. White, Jeffrey J.; Toy, David K.; Groat, J. Everett. Systems and methods for controlling aircraft electrical power. USP2012048155876.
  29. Greene,Leonard M.. Systems and methods for evading heat seeking missles. USP2008057367531.
  30. Karimi, Kamiar J.; Liu, Shengyi; Liffring, Mark E.; Helton, Steven B.; Fu, Sheau-Wei (Johnny). Vehicle electrical power management and distribution. USP2014058738268.