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.
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
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