- 专利标题： Turbojet engine cold stream flow path suspended from the exhaust case by radial crevice mounts and link rods
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申请号： US14116597申请日： 2012-05-07
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公开(公告)号： US09828877B2公开(公告)日： 2017-11-28
- 发明人: Thomas Gérard Daniel Riviere , François Robert Bellabal , Olivier Renon , Guilhem Seize
- 申请人： Thomas Gérard Daniel Riviere , François Robert Bellabal , Olivier Renon , Guilhem Seize
- 申请人地址： FR Paris
- 专利权人： SNECMA
- 当前专利权人： SNECMA
- 当前专利权人地址： FR Paris
- 代理机构： Oblon, McClelland, Maier & Neustadt, L.L.P.
- 优先权： FR1153946 20110509
- 国际申请： PCT/FR2012/051011 WO 20120507
- 国际公布： WO2012/153056 WO 20121115
- 主分类号： F01D25/24
- IPC分类号： F01D25/24 ; F01D25/16 ; F02C7/20
摘要：
A bypass turbojet engine including a cylindrical cold stream flow path supported by link rods which are attached to a cylindrical outer shell ring of an exhaust case at attachment points. The attachment points for the exhaust case are crevice mounts including lugs that extend radially from the outer shell ring, a bore of the crevice mounts being directed in a direction of generatrices of the outer shell ring.
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