发明名称 |
GAS TURBINE ENGINE NOSE CONE |
摘要 |
A nose cone for a turbofan gas turbine engine includes a central tip, an outer perimeter and a substantially conical outer wall extending therebetween which encloses a cavity therewithin. The outer wall includes an inner substrate layer facing the cavity and an outer layer which overlies and at least partially encloses the inner substrate layer. The outer layer is composed entirely of a nanocrystalline metal forming an outer surface of the nose cone.
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申请公布号 |
US2013255277(A1) |
申请公布日期 |
2013.10.03 |
申请号 |
US201213435738 |
申请日期 |
2012.03.30 |
申请人 |
MACCHIA ENZO;ELEFTHERIOU ANDREAS;MCDONOUGH THOMAS PETER;GUGLIELMIN GEORGE;LANZINO JOE;BARNETT BARRY |
发明人 |
MACCHIA ENZO;ELEFTHERIOU ANDREAS;MCDONOUGH THOMAS PETER;GUGLIELMIN GEORGE;LANZINO JOE;BARNETT BARRY |
分类号 |
F02C7/00;B05D1/18;F01D25/00;F02C3/04 |
主分类号 |
F02C7/00 |
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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