发明授权
- 专利标题： Efficient low carbon emission airplane integrating jet fuel and cryogenic fuel systems
-
申请号： US13897452申请日： 2013-05-20
-
公开(公告)号： US10800525B2公开(公告)日： 2020-10-13
- 发明人: Mithra M. K. V. Sankrithi , Arvin Shajanian , Sergey D. Barmichev , Victor Ken Stuhr , Joshua M. Kusnitz , Ismail Robbana
- 申请人： The Boeing Company
- 申请人地址： US IL Chicago
- 专利权人： The Boeing Company
- 当前专利权人： The Boeing Company
- 当前专利权人地址： US IL Chicago
- 代理机构： McDonnell Boehnen Hulbert & Berghoff LLP
- 主分类号： B64D37/06
- IPC分类号： B64D37/06 ; B64C39/04 ; B64D37/30 ; B64D37/04 ; F02C3/20 ; B64C30/00 ; B64C39/00 ; B64C1/00
摘要：
A hybrid fuel airplane and methods are presented. A cryogenic fuel is transferred to an airplane propulsor from an airplane fuel system comprising a cryogenic fuel tank and a jet fuel tank. The cryogenic fuel tank conforms to an outer mold line and carries a cryogenic fuel, and is located in a portion of the airplane body while not extending beyond the outer mold line. The jet fuel tank carries a jet fuel and is located in an airplane wing, or an airplane body, or both. A dynamic aircraft load is born on the cryogenic fuel tank, and the airplane propulsor is operated using the cryogenic fuel to generate thrust for the hybrid fuel airplane. An aerodynamic lift is generated using the airplane wing coupled to the airplane body.
公开/授权文献
信息查询
