发明名称 |
Support bracket for turboprop engine nozzle |
摘要 |
<p>The bridge has two legs (5A, 5B), each constituting an end of a metal blade and contacting a thermal plastic liner. An arched central portion (8) connects the legs and constitutes a zone of contact with a sleeve of a support channel (2) of a jet pipe. The portion has an inverted central camber defining two top zones (4) constituting two points contacting the sleeve. An independent claim is also included for a device for positioning and adapting to the differential expansions between the thermal plastic liner and a sleeve of a support channel of a jet pipe of a jet prop engine.</p> |
申请公布号 |
EP1577505(A2) |
申请公布日期 |
2005.09.21 |
申请号 |
EP20050102022 |
申请日期 |
2005.03.15 |
申请人 |
SNECMA |
发明人 |
MANDET, EMMANUEL CHRISTOPHE;ROCHE, JACQUES-A;SALPERWYCK, LAURENT CLAUDE PATRICK |
分类号 |
F01D25/24;F02C7/00;F01D25/26;F02C3/14;F02C7/20;F02K1/78;F02K1/82;F23R3/00;F23R3/28;F23R3/60;(IPC1-7):F01D25/24 |
主分类号 |
F01D25/24 |
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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