|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/135R; 244/172; 244/1350R; 220/901|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 16 인용 특허 : 6|
The present invention discloses a novel fuel structure for housing and delivering disparate cryogenic fuels to combustion zones in an aerospace vehicle. The tank comprises a plurality of containers having volumes that are separated by common wall bulkheads and which are arranged substantially side-by-side in conformance with the interior of the aerospace vehicle. A tank support structure positioned within the vehicle interior includes lengthwise supports as well as cross-wise supports, with the latter including openings within which the rear ends of the ...
1. A cryogenic propellant fuel tank for a single stage to orbit aircraft, said fuel tank comprising:a propellant container comprising a plurality of chambers for holding first and second cryogenic propellants, the chambers being separated from one another by a common bulkhead, said container having a forward and rearward portions, the width of the rearward portion being greater than the width of the forward portion, and structural support means for securing said container within the aircraft.