$\require{mediawiki-texvc}$
  • 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

Actively controlled thermal panel and method therefor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/22    B64G-001/24   
미국특허분류(USC) 244/158R ; 244/164 ; 244/170 ; 244/171 ; 244/172 ; 244/173 ; 244/168 ; 701/013 ; 701/03
출원번호 US-0746587 (1996-11-12)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Whitney
인용정보 피인용 횟수 : 21  인용 특허 : 16
초록

One or more deployable thermal panels (24, 28, 70) are actively controlled throughout the orbit of a satellite (20) to provide thermal dissipation. Adjusting the incident angle between the panel (24, 28, 70) and the sun and controlling the flow of fluid through optional flexible heat pipes loads and unloads heat to provide thermal stability for components (62) which have special thermal requirements. An optional antenna panel (70) on a nadir side (64) of the satellite (20) offers an antenna side (74) on one surface and a thermal radiating side (72) on an...

대표
청구항

[ What is claimed is:] [1.] A space vehicle having actively controlled thermal radiating surfaces, said space vehicle comprising:a body;a panel drive unit attached to said body;a thermal panel having an attached end and a free end opposing said attached end, said attached end of said thermal panel being attached to said drive unit so as to reside outside said body, wherein said thermal panel includes a communications antenna, and is configured to have a communications radiating side and a thermal radiating side opposite said communications radiating side...

이 특허에 인용된 특허 (16)

  1. Lievre Jrme (Bagneux FRX). Active damping of satellite nutation. USP1988034732354.
  2. Flament Patrick (Le Cannet FRX) Perdu Michel (Frejus FRX) Portier Jean (Cannes FRX) Brunet Pierre (Auribeau S/Siagne FRX). Apparatus controlling the pitch attitude of a satellite by means of solar radiation pressure. USP1997055626315.
  3. Flament Patrick (Le Cannet FRX). Attitude control device using solar sails for a satellite stabilized on three axes. USP1992075133518.
  4. Guenther Hans-Jrgen (Bremen DEX) Nauck Joachim (Bremen DEX) Renner Udo (Leiden DEX) Fehse Wigbert (Lisse DEX). Attitude control for satellites. USP1986054591116.
  5. Yocum ; Jr. John F. ; Fowell Richard A. ; Lee Raymond S.. Controlled-emission solar tabs for attitude solar sailing. USP1998075775645.
  6. Salvatore Jeremiah O. (Redondo Beach CA) Wittmann Alois (Palos Verdes CA). Method and apparatus for satellite torque balancing. USP1994055310144.
  7. Surauer Michael (Chieming DEX) Bittner Helmut (Munich DEX). Method of adjusting the position of satellites by means of solar pressure torques. USP1997125697582.
  8. Murphy John R. ; Crowley Ross. Optimal solar tracking system. USP1998105816540.
  9. Hubert Bernard (Le Cannet Rocheville FRX) Blancke Bernard (Le Cannet Rocheville FRX). Process and device for aligning the roll axis of a satellite with a desired direction. USP1984014426052.
  10. Rosen Harold A. (Santa Monica CA). Satellite control system. USP1990084949922.
  11. Flament Patrick (Le Cannet FRX). Satellite roll and yaw attitude control method. USP1992095149022.
  12. Zimbelman Darrell F. (Gaithersburg MD). Spacecraft thermal disturbance control system. USP1993055211360.
  13. Johnson Caldwell C. (Dickinson TX) Faget Maxime A. (Dickinson TX) Bergeron ; III David J. (Friendswood TX). Spacecraft with articulated solar array. USP1988054747567.
  14. Caplin Glenn. Spacecraft with large east-west dimensions. USP1998115833175.
  15. Clark John F. (Princeton NJ). Station-keeping using solar sailing. USP1988074759517.
  16. Renner Udo (Leiden NLX). System for controlling the direction of the momentum vector of a geosynchronous satellite. USP1982044325124.

이 특허를 인용한 특허 피인용횟수: 21

  1. Randy Pon. AFT deployable thermal radiators for spacecraft. USP2002046378809.
  2. Walker, Andrew. Artificial Satellite. USP20181110118717.
  3. Walker, Andrew Nicholas. Artificial satellite and method for filling a tank of propellent gas of said artificial satellite. USP2018029902507.
  4. Bertheux, Philippe; Texier, Emmanuel; Jacque, Bernard; Seguin, Jean-Marie. Deployable radiator for a space vehicle. USP2003126669147.
  5. Jondeau, Laurence; Flemin, Christian; Mena, Fabrice. Device for controlling the heat flows in a spacecraft and spacecraft equipped with such a device. USP2012088240612.
  6. Hentosh, David J.; Lafergola, John. Independent East/West thermal management system. USP2010077762499.
  7. Liu, Ketao. Method and apparatus for minimizing solar array sun tracking disturbance by north and south solar array wing cancellation. USP2005076921048.
  8. Kiu, Ketao. Method and apparatus for stepping space craft mechanisms at low disturbance rates. USP2005076917861.
  9. Russell, Adrian G. Payload modules. USP2012018096512.
  10. McKinnon, Douglas V.; Brown, David M.; Hentosh, David J.. Satellite with deployable, articulatable thermal radiators. USP2011017874520.
  11. Liu Ketao. Solar wing thermal shock compensation using solar wing position actuator. USP2001116318675.
  12. David K. Vail ; Thornton Hinshaw. Space vehicle with temperature sensitive oscillator and associated method of sensing temperature in space. USP2002056390672.
  13. Wong, Hamilton. Spacecraft battery thermal management system. USP2011067967256.
  14. Wong, Hamilton; Goodzeit, Neil E.; Buckley, Rok Park; Hentosh, David J.. Spacecraft east-west radiator assembly. USP2015038967547.
  15. Mark A. Blair. Spacecraft sunshield for use in performing solar torque balancing. USP2002116481671.
  16. Tsao,Tung Ching; Liu,Ketao. Target acquisition control for spacecraft gimballed payload. USP2008107437224.
  17. Keramidas, Nikolus A.. Thermal control system for controlling temperature in spacecraft. USP2003016511021.
  18. Prakash,Arun; Wang,Hanching Grant. Transient cancellation technique for spacecraft solar wing stepping. USP2008037343228.
  19. Sebata,Susan; Low,Lenny. Two-sided deployable thermal radiator system and method. USP2006047028953.
  20. Cognata, Thomas Jaspero; Hartl, Darren; Sheth, Rubik; Dinsmore, Craig. Variable heat rejection device. USP20190310228197.
  21. Gernert, Nelson. Vehicle thermal management system. USP20190310225953.