发明名称 |
System driving the displaceable fairing of a turbojet-engine thrust reverser |
摘要 |
A thrust reverser having an annular duct bounding a bypass flow and including a set of vane cascades configured in a stationary pod portion, a displaceable fairing slidably mounted on the stationary pod portion to permit sliding motion along a slotted cylindrical shell and to be translated between a stowed position blocking access of the bypass flow to the vane cascades and a deployed position wherein the vane-cascades are exposed to the bypass flow, a drive system driving the displaceable fairing, and flaps arranged to seal the annular duct in order to deflect a flow toward the vane cascades. The drive system further includes linear actuators substantially configured in the central axis of the slotted cylindrical shells.
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申请公布号 |
US6592074(B2) |
申请公布日期 |
2003.07.15 |
申请号 |
US20020092881 |
申请日期 |
2002.03.08 |
申请人 |
HUREL-HISPANO |
发明人 |
DEHU MICHEL PHILIPPE;LESBOS DAMIEN BENO&ITILDE,T MARIE;VAUCHEL GUY BERNARD |
分类号 |
F02K1/72;F02K1/76;(IPC1-7):F02K1/62 |
主分类号 |
F02K1/72 |
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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