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특허 상세정보

Light weight hydrogen tank

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B65D-025/00   
미국특허분류(USC) 220/00414; 220/5601; 220/586
출원번호 US-0615671 (2000-07-14)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    V. D. Duraiswamy
인용정보 피인용 횟수 : 16  인용 특허 : 6
초록

A light weight fuel tank for a hydrogen powered airplane used as a platform for communication repeaters for communication services. An outer spherical shell member of a sandwich configuration surrounds an inner thin walled spherical shell member in which the liquid hydrogen is contained. A radial gap between the shell members is evacuated to a high vacuum. The facing surfaces of the shell members are coated with a low emissivity material. Electrical heaters are provided to control the evaporation rate of the hydrogen to match the fuel usage and to preven...

대표
청구항

1. A lightweight fuel tank comprising:an outer spherical shell member; an inner spherical shell member positioned inside said outer shell member; said inner shell member and said outer shell member being positioned to provide an insulating radial gap between them; said inner shell member having an outer surface and an inner surface, said outer surface being coated with a low emissivity material; and said outer shell member having an outer surface and an inner surface, said inner surface being coated with a low emissivity material; said inner shell member...

이 특허를 인용한 특허 피인용횟수: 16

  1. Kendall, Greg T.; Lisoski, Derek L.; Morgan, Walter R.; Griecci, John A.. Active dihedral control system for a torisionally flexible wing. USP2015099120555.
  2. Kendall, Greg T.; Lisoski, Derek L.; Morgan, Walter R.; Griecci, John A.. Active dihedral control system for a torsionally flexible wing. USP2017099764819.
  3. Kendall, Greg T.; Morgan, Walter R.. Aircraft control system. USP2010097802756.
  4. Aceves, Salvador M.; Ledesma-Orozco, Elias Rigoberto; Espinosa-Loza, Francisco; Petitpas, Guillaume; Switzer, Vernon A.. Compact insert design for cryogenic pressure vessels. USP2017069677713.
  5. Chang, Donald C. D.; Cha, Alan. Concurrent communications between a user terminal and multiple stratospheric transponder platforms. USP2005096941138.
  6. Hogenson,Peter A.; Chong,Keith; Duong,Peter. Cryogenic fuel tank insulation assembly. USP2007117296769.
  7. Borchert, Matthias; Wolter, Gerd; Lorenz, Harald; Eulitz, Dirk; Kramer, Timo. Fuel tank seam with lead-through means. USP2010107810666.
  8. Wolff, David; Speranza, Antonio John; Chow, Oscar. Hydrogen fueled electrical generator system and method thereof. USP2005066907735.
  9. MacCready, Paul B.; Hibbs, Bart D.; Curtin, Robert F.. Hydrogen powered aircraft. USP2012118308106.
  10. MacCready, Paul B.; Hibbs, Bart D.; Curtin, Robert F.. Hydrogen powered aircraft. USP2011098011616.
  11. MacCready, Paul B.; Hibbs, Bart D.; Swanson, Kyle D.; Curtin, Robert F.. Hydrogen powered aircraft. USP2011108028951.
  12. MacCready,Paul B.; Hibbs,Bart D.; Curtin,Robert F.. Hydrogen powered aircraft. USP2007107281681.
  13. Rosen, Harold A.; Wittmann, Alois; Pano, Scott B.. Light weight hydrogen tank. USP2005036868981.
  14. MacCready, Paul B.; Hibbs, Bart D.; Curtin, Robert F.; Swanson, Kyle D.; Belik, Paul. Liquid hydrogen stratospheric aircraft. USP2003046550717.
  15. Hausberger, Klaus; Meinert, Marius; Döller, Christian; Rauchegger, Bernd. Outer tank for cryogenic fuel. USP2014088794476.
  16. Keip,Charles P.. Pressurized hydrogen storage system. USP2008037337811.