$\require{mediawiki-texvc}$
  • 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

Pneumatically controlled wide heat load space radiator

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F28F-013/00    F28F-001/22   
미국특허분류(USC) 165/96 ; 126/271 ; 165/154 ; 165/171
출원번호 US-0764564 (1977-01-28)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 15  인용 특허 : 1
초록

A three way valve selectively charges or discharges gas under pressure within the annular gaps between a series of transversely extending longitudinally spaced radiator tubes fixed to a radiator panel to control waste heat rejection and coaxial inner tubes which may comprise heat pipes or turns of a sinuous coolant flow tube for spacecraft, earth satellites and the like to thermal couple and decouple the heat pipe or coolant flow tube to the space radiator.

대표
청구항

A pneumatically controlled, wide heat load, space radiator assembly for a spacecraft, earth satellite, or the like, said radiator assembly comprising in combination: a heat radiator mounted to the spacecraft for thermal radiation to space, said heat radiator having a face, at least one tube array mounted to the face of the heat radiator in thermal conducting fashion, said array comprising concentric, radially spaced, longitudinally extending inner and outer heat conductive tubes, means defining a sealed annular gap between said tubes of a given longitudi...

이 특허를 인용한 특허 피인용횟수: 15

  1. Robert T. Bigelow ; Russell J. Common ; John Mezits ; David A. Cavaleri. Apparatus for spacecraft thermal management. USP2002116481670.
  2. Antoniuk David ; Baker Jeffrey L. ; Wittkopp Garrett R.. Embedded heat pipe structure. USP2000056065529.
  3. Phillips,Alfred L.; Khrustalev,Dmitry K.; Wert,Kevin L.; Wilson,Michael J.; Wattelet,Jonathan P.; Broadbent,John. Flexible loop thermosyphon. USP2006037013955.
  4. Egbert Mark A.. Heat exchanger with heat-pipe amplifier. USP1999075924479.
  5. O\Neill Richard F. (Carlsbad CA). Heat sink/fluid-to-fluid mechanical coupling of spacecraft coolant systems. USP1982044324375.
  6. Lee A. Tobias. Hot gas valve construction for reducing thermal shock effects. USP2002096453937.
  7. Hwang Jaw-Yeu (Tampa FL). Method for limiting heat flux in double-wall tubes. USP1982044325425.
  8. Keeton, Alvin R.; Down, Michael G.. Passive emergency core cooling system for a liquid metal fast. USP198609H000119.
  9. McKinnon, Douglas V.; Moran, Timothy P.. Spacecraft heat dissipation system. USP2014098820684.
  10. Mims James (Albuquerque NM) Buden David (Albuquerque NM) Williams Kenneth (Albuquerque NM). Survivable pulse power space radiator. USP1989054832113.
  11. Almgren David W. (Concord MA) Bartoszek John T. (Bolton MA) Lucas Robert M. (Melrose MA) Berthiaume Richard P. (Winchester MA) Spencer Richard H. (Winchester MA) Saia William H. (Danvers MA). Thermal control system. USP1983064388964.
  12. Arik,Mehmet; Rohling,Kenneth William; Watkins,Ronald Dean. Thermal management apparatus and uses thereof. USP2008107439741.
  13. Arik,Mehmet; Rohling,Kenneth William; Watkins,Ronald Dean. Thermal management apparatus and uses thereof. USP2006117140420.
  14. Kuo Ying-Yan (Palo Alto CA). Variable conductance thermal insulation blanket. USP1989104871012.
  15. Cho, Wei-Lin; Adamson, Gary A.. Variable heat rejection using heat pipe heat exchanger. USP2018049939203.