发明名称 |
ANTI-ICING APPARATUS AND METHOD FOR AERO-ENGINE NOSE CONE |
摘要 |
An aero-engine nose cone anti-icing system (10) using a rotating heat pipe (12) is provided to replace the current method of blowing hot compressor bleed air over the nose cone surface. Heat is transferred from a hot source (36) within the engine (22) to the nose cone (18) through a rotating heat pipe (12) along the central shaft (16). A condenser (20) and evaporator (14) are provided which are adapted to the heat transfer requirements and space constraints in the engine (22).
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申请公布号 |
US2009199535(A1) |
申请公布日期 |
2009.08.13 |
申请号 |
US20090429230 |
申请日期 |
2009.04.24 |
申请人 |
BRAND JOSEPH HORACE;DOWHAN MICHAEL JOHN |
发明人 |
BRAND JOSEPH HORACE;DOWHAN MICHAEL JOHN |
分类号 |
F02G5/02;F01D25/02;F02C7/047;F28D15/02 |
主分类号 |
F02G5/02 |
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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