发明名称 |
HYBRID TORQUE BOX FOR A THRUST REVERSER |
摘要 |
A hybrid torque box comprising a plurality of composite tubes and metal fittings attached together in alternating succession and configured to attach a thrust reverser to an engine fan case of an aircraft. The hybrid torque box may be substantially hollow and may comprise two V-blades for attaching the torque box to the engine fan case. The hybrid torque box may also be attached to or integral with a bull nose fairing configured for attachment with a cascade of the thrust reverser. Furthermore, the hybrid torque box may comprise and/or attach to a cowl interface flange configured for interfacing with an outer cowl of the thrust reverser.
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申请公布号 |
US2011215193(A1) |
申请公布日期 |
2011.09.08 |
申请号 |
US20100717501 |
申请日期 |
2010.03.04 |
申请人 |
SPIRIT AEROSYSTEMS, INC. |
发明人 |
WELCH JOHN M.;SCHAEFER HENRY ARNOLD;TYMES MATTHEW SCOTT;URBAN MICHAEL PATRICK |
分类号 |
B64D27/26;B23P15/00;B64D27/00;F02K1/54 |
主分类号 |
B64D27/26 |
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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