|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3914 ; 60/3915|
|우선권정보||DT-2375592 (1973-05-19); DT-2413882 (1974-03-22); DT-2414918 (1974-03-28)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 48 인용 특허 : 0|
Two aircraft jet engines are associated respectively with two sub-systems each comprised of a gas turbine for starting one of the engines and driving a set of secondary power generators such as hydraulic pump and electric generator and an air conditioning unit. The two sub-systems are drivingly cross-linked so that either gas turbine can drive both sets. The air conditioning units as well as the gas turbines receive tapped air from the engine compressors, whereby the gas turbines may run with or without combustion. An emergency power pack may be provided...
Apparatus for starting aircraft engines and driving auxiliary equipment, comprising two independently operating auxiliary gas turbines respectively individually connected to two aircraft engines for driving them for starting; a first and second plurality of auxiliary equipment each plurality including at least one distribution transmission gearing, an electric generator, an auxiliary compressor and a hydraulic pump all being drivingly connected to the gearing, each of said pluralities establishing a power park operating independently from the respective ...