|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 13 인용 특허 : 0|
A bypass flow system for a gas-side air recuperator of a gas turbine engine. Pressurized air from the compressor section of the gas turbine is caused to pass through a pair of heat exchangers arranged in parallel spaced relationship and located in the hot gas stream between the exhaust gas box and the exhaust stack of the gas turbine engine. The space between the heat exchangers comprises a bypass duct for the exhaust gases and is openable and closeable by a butterfly valve. The longitudinal edges of the bypass duct are each provided with a flow divider ...
A gas-side bypass flow system for an air recuperator of a gas turbine engine, said gas turbine engine comprising a compressor section, a combustor section, and a turbine section followed by a free wheeling power turbine, said gas turbine engine having an exhaust gas emitting end, said recuperator being located in a path of said exhaust gas and comprising a pair of heat exchangers in parallel spaced relationship, a bypass duct being located between said heat exchangers and having longitudinal sides and ends, an inlet opening and an outlet opening for said...