| 发明名称 |
GAS TURBINE COOLER BY AIR SENT AT COMPRESSOR LEVEL |
| 摘要 |
<p>A system for cooling a gas turbine by bleeding air from the compressor and channeling the air at the center of the engine towards the turbine in order to cool it. The air is bled from the plane of the disc bearing the blades of the compressor, said disc having radial ducts for the flow of the air. The invention is utilized in gas turbine engines to cool the turbine.</p> |
| 申请公布号 |
JPS5793634(A) |
申请公布日期 |
1982.06.10 |
| 申请号 |
JP19810159368 |
申请日期 |
1981.10.06 |
| 申请人 |
NASHIONAARE DECHIYUUDO E DO KONSUTORAKUSHION DE MONIYUURU TABIASHION:SOC |
发明人 |
JIYAN JIYORUJIYU BUIEERU;FURANSOWA EMIIRU JIYORUJIYU KUROZE;MARUSERU ROBEERU SORINII |
| 分类号 |
F01D5/18;F02C7/18;F04D27/02;F04D29/58 |
主分类号 |
F01D5/18 |
| 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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