发明名称 |
Turbojet engine comprising a connector arm for ancillary systems, and the connector arm for ancillary systems |
摘要 |
A turbofan jet engine includes an outer fan duct, an inner fan duct, fluid-conveying ancillaries located outside the outer fan duct, fluid-conveying ancillaries located inside the inner fan duct. At least one removable modular arm forming a connection for ancillaries is arranged between the outer fan duct and the inner fan duct. The removable arm provides a connection of ancillaries outside the outer fan duct to ancillaries inside the inner fan duct.
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申请公布号 |
US7543442(B2) |
申请公布日期 |
2009.06.09 |
申请号 |
US20050031004 |
申请日期 |
2005.01.10 |
申请人 |
SNECMA |
发明人 |
DERENES JACKY;MAZEAUD GEORGES |
分类号 |
F01D25/24;F02C7/00;F01D9/06;F02K3/06 |
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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