|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 6 인용 특허 : 0|
A gas turbine engine of simple construction having a compressed air cooler between the first and second stages of compression. A turbine with a heat recuperator is arranged to transfer heat from the exhaust gas stream to the combustion inlet. The air cooler and recuperator are of tubular type, formed by a plurality of small diameter tubes uniformly distributed forming coaxial cylindrical bodies placed one within the other. Heat exchange flanges are joined to each other and are situated in the same plane. The stator parts of the engine constitute a shell ...
1. A gas turbine engine, comprising a compressor with a compressed air cooler between stages and a turbine with a heat recuperator for exhaust gases, characterized by the fact that the air cooler is formed by a set of parallel tubes joined at both ends to a first flange and uniformly distributed so as to form a hollow body in the inner part of which the heat recuperator is housed, said heat recuperator being formed by a set of parallel tubes joined at both ends to a second flange, both flanges being joined to each other and to the body of the engine, the...