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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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