发明名称 Aircraft jet engine heat exchanger - includes water injection system to reduce temp. of inlet gases to safe level during take=off
摘要 <p>The efficiency of a gas turbine can be improved by passing the exhaust gases through a heat exchanger in order to heat the air before it enters the combustion chamber. A water injection system sprays water from jets (10) into the exhaust duct before the exhaust gases from the turbine (TG) reach the heat exchanger (RA) which pre-heats the air from the compressor (CA) before it enters the combustion chamber (CC). Thus during aircraft take-off the safe operating temp. of the heat exchanger is not exceeded.</p>
申请公布号 FR2401319(A1) 申请公布日期 1979.03.23
申请号 FR19770026639 申请日期 1977.08.26
申请人 SNECMA 发明人 RENE GEORGES VOISENET
分类号 F01D25/30;F02C7/08;F02C7/141;(IPC1-7):02C7/10 主分类号 F01D25/30
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