|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||H01M-008/02 H01M-008/24 B64C-001/12 B64C-001/16 B64D-035/02|
|미국특허분류(USC)||429/462; 429/511; 429/515; 244/054; 244/099.1; 244/119; 244/126|
|우선권정보||DE-10 2007 061 991 (2007-12-21)|
|§371/§102 date||20100812 (20100812)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 5|
A fuel cell system module for use in an aircraft includes at least one fuel cell system component. The fuel cell system module is connectable modularly to a fuselage section of the aircraft. A housing element of the fuel cell system module is designed to form a section of an outer skin of the aircraft when the fuel cell system module is in the state connected to the fuselage section of the aircraft.
1. A fuel cell system module for use in an aircraft having a fuselage section having an outer skin, the fuel cell system module comprising: at least one fuel cell system component, anda fuel tank having a fuel tank housing, wherein the fuel tank housing comprises: an outer shell,an inner shell spaced apart from the outer shell,a first space located between the outer shell and the inner shell of the fuel tank housing and being filled with a material of poor thermal conductivity, anda second space defined within the inner shell for holding fuel to be suppl...