|국가/구분||United States(US) Patent 등록|
|우선권정보||DE-10 2008 048 915 (2008-09-26)|
|§371/§102 date||20110502 (20110502)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 12 인용 특허 : 19|
A power distribution system for an aircraft having at least one engine includes at least one torque transmission means that is movably held and is connected to at least one shaft of the engine and extends from the shaft of the engine to an interior region of the aircraft fuselage, and at an end pointing away from the engine has at least one interface for introducing a torque. At the interface of the torque transmission means it is possible both to operate mechanical and to start the engine. Consequently in the aircraft it is possible to essentially do wi...
1. A power distribution system for an aircraft equipped with at least one engine, comprising: at least one torque transmission means;at least one distribution shaft;at least one first coupling for transmitting a torque between the at least one torque transmission means and the at least one distribution shaft;at least one rotatable device of an environmental control system, the at least one rotatable device located in an interior region of the aircraft fuselage and being coupled with the at least one distribution shaft; andat least one electrical energy s...