|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 17 인용 특허 : 17|
A starting system for starting the propulsion engines of gas turbine powered aircraft that combines power sources delivered by the APU so that essentially then entire power delivered by the APU for pneumatic, hydraulic and electric power is applied to corresponding starters on each propulsion engine during MES simultaneously.
What is claimed is: 1. A starting system for starting the propulsion engines of gas turbine powered aircraft comprising: an auxiliary power unit (APU) with a pneumatic supply source and an auxiliary supply source; at least one gas turbine propulsion engine with a pneumatic starter and an auxiliary starter; a pneumatic supply path for controlling and distributing pneumatic power from the pneumatic supply source to the pneumatic starter upon main engine start (MES); and an auxiliary supply path for controlling and distributing auxiliary power from the aux...