| 发明名称 |
GASTURBINENANLAGE |
| 摘要 |
A cooling system 46 for a turbofan gas turbine 10 is disclosed. Various construction details which increase the effectiveness of a heat exchanger 48 located in the secondary flow path 24 are developed. In one embodiment, the cooled air is used for protecting a bearing compartment. |
| 申请公布号 |
DE3447717(A1) |
申请公布日期 |
1985.07.04 |
| 申请号 |
DE19843447717 |
申请日期 |
1984.12.21 |
| 申请人 |
UNITED TECHNOLOGIES CORP. |
发明人 |
J. HOVAN,EDWARD;P. ZIMONIS,JOSEPH |
| 分类号 |
F01D5/18;F01D25/12;F01D25/18;F02C7/06;F02C7/14;F02C7/18 |
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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