|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/776; 060/787; 060/785|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 5 인용 특허 : 13|
A gas turbine engine integrates the functions of an auxiliary power unit (APU) with one or more functions of an ECS, and that is capable of operating in both an unfired mode and a fired mode. The gas turbine engine includes a combustor system that is configured to allow the gas turbine to quickly transition from the unfired mode to the fired mode, by bypassing a portion of the air flowing to the combustor system around the combustor.
1. A gas turbine engine, comprising:a compressor having an inlet and a compressed air outlet;a turbine having at least an inlet;a combustor system including:a housing having at least a first air inlet in fluid communication with the compressed air outlet, a second air inlet adapted to receive compressed air from a second compressed air source, and an inlet plenum in fluid communication with the first and second air inlets,a combustor mounted at least partially within the housing, the combustor having one or more air inlets in fluid communication with the...