Cascade thrust reverser for an aircraft turbojet engine

    公开(公告)号:US09617955B2

    公开(公告)日:2017-04-11

    申请号:US14620543

    申请日:2015-02-12

    Applicant: AIRCELLE

    CPC classification number: F02K1/625 F02K1/72 F02K1/763 F02K1/766

    Abstract: The present disclosure relates to a cascade thrust reverser providing that when a sliding cowl and a flap are in a direct jet position, a hook is held in engagement with another hook and the flap is immobilized inside of a housing of the sliding cowl by a stem of a telescopic connecting rod subjected to pre-stress generated by a compressed spring located in the body of the connecting rod. When the sliding cowl starts to slide from the direct jet position toward the reverse jet position, the hooks disengage each other and the stem engages with an extension in the body of the connecting rod, so that the flap is rotated from the direct jet position toward the reverse jet position due to the tensile force exerted by the stem.

Patent Agency Ranking