发明名称 |
COMPLIANT INTERMEDIATE COMPONENT OF A GAS TURBINE ENGINE |
摘要 |
The present application provides an intermediate structure (130) in a gas turbine engine. The intermediate structure is positioned between a first component (120) and another component (110). The first component (120) may be a composite component. The components may be interlocking. The intermediate structure may be load bearing. Also disclosed is a method using the intermediate structure (130). |
申请公布号 |
CA2897965(A1) |
申请公布日期 |
2014.10.09 |
申请号 |
CA20132897965 |
申请日期 |
2013.12.27 |
申请人 |
ROLLS-ROYCE CORPORATION |
发明人 |
THOMAS, DAVID J.;CHAMBERLAIN, ADAM L.;USKERT, RICHARD C. |
分类号 |
B60H1/02;F01D5/28;F01D5/30;F01D5/32 |
主分类号 |
B60H1/02 |
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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