发明名称 |
INTEGRATED THRUST REVERSER ASSEMBLY |
摘要 |
Assembly for supporting a gas turbine engine comprises a support member (14) including mounting sites for attachment to an associated aircraft. The support member includes integral slider tracks (78) disposed on opposed sidewalls for selective engagement with a translatable cowl. The translatable cowl (22) is translatable along the slider tracks to selectively cover and expose a cascade thrust- reversing structure (24). The cascade structure includes arcuate segments (24a) mounted in hinged relationship to the support member. Rearward translation of the translatable cowl (22) to a service position permits the cascade structure (24) to be opened for access to the core engine.
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申请公布号 |
CA2769313(A1) |
申请公布日期 |
2011.02.03 |
申请号 |
CA20102769313 |
申请日期 |
2010.07.12 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
STUART, ALAN ROY;FEHRMANN, JOHN ROBERT |
分类号 |
F02K3/02 |
主分类号 |
F02K3/02 |
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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