|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/39142 ; 60/39461|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 17 인용 특허 : 3|
Duplication of engine and secondary power system components in individual auxiliary and emergency power units is avoided in an integrated power unit including a gas turbine engine 10 having a centrifugal compressor 28 and a turbine 40, a generator 18 coupled to the engine 10, an air inlet 22 to the compressor 28, a first reservoir 82 for combustible fuel, and a first combustor 34, 36 for receiving and combusting compressed air from the compressor 28 and fuel from the reservoir 82 to generate gasses of combustion and feeding the gasses of combustion to th...
An integrated power unit alternatively operable as an auxiliary power unit and as an emergency power unit and comprising: a gas turbine engine including a centrifugal compressor and a turbine; a generator coupled to said turbine engine to be driven thereby; an inlet to said compressor including at least one variable inlet guide vane for controlling the flow of air from said inlet to said compressor; a first reservoir for a combustible fuel; a first combustor for receiving and combusting compressed air from said compressor and fuel from said first reservo...