|국가/구분||United States(US) Patent 등록|
|우선권정보||DE-10 2009 010 243 (2009-02-24)|
|§371/§102 date||20110824 (20110824)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 3 인용 특허 : 17|
A power generation system for integration into an aircraft system, including a secondary power supply device having a generator turbine arranged in a duct running between a forward opening and a rearward opening on the fuselage of the aircraft. An electromagnetic unlocking device locks and unlocks a covering device on the forward opening, depending on a signal strength supplied to the unlocking device. The system also includes an actuation device that generates an opening or closing signal for an opening and closing device, and an opening function switch...
1. A power generation system for integration into an aircraft fuselage, the power generation system comprising: a secondary power supply device, comprising: a duct running between two openings on the fuselage, wherein one is a forward opening and the other a rearward opening along an aircraft longitudinal direction,a turbine arranged in the duct with a generator coupled to the turbine,a covering device, movable between a closed and an open position for covering the forward opening in its closed position,an opening and closing device, andan unlocking devi...