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    Rear mounted reverse core engine thrust reverser
    12.
    发明授权
    Rear mounted reverse core engine thrust reverser 有权

    公开(公告)号：US09897040B2

    公开(公告)日：2018-02-20

    申请号：US14190171

    申请日：2014-02-26

    Applicant: United Technologies Corporation

    Inventor： Gabriel L. Suciu ,  Jesse M. Chandler ,  Brian D. Merry

    IPC: F02K1/60

    CPC classification number: F02K1/60 ,  F05D2210/40 ,  F05D2250/314

    Abstract: In one embodiment, a gas turbine engine for mounting to a rear of an aircraft fuselage has a propulsor that rotates on a first axis, and an engine core including a compressor section, a combustor section, and a turbine section, with the turbine section being closer to the propulsor than the compressor section. The engine core is aerodynamically connected to the propulsor and has a second axis. A nacelle is positioned around the propulsor and engine core. The nacelle is attached to the wing of the aircraft. A downstream end of the nacelle has at least one pivoting door with an actuation mechanism to pivot the door between a stowed position and a vertical deployed position in which the door inhibits a flow to provide a thrust reverse of the flow.

    ELECTRONIC MODULE MOUNTING TO VIBRATION ISOLATING STRUCTURE
    16.
    发明申请
    ELECTRONIC MODULE MOUNTING TO VIBRATION ISOLATING STRUCTURE 审中-公开

    公开(公告)号：US20170306850A1

    公开(公告)日：2017-10-26

    申请号：US15137561

    申请日：2016-04-25

    Applicant: United Technologies Corporation

    Inventor： Joseph Stack ,  Jesse M. Chandler ,  Gabriel L. Suciu ,  Kurt J. Sobanski

    IPC: F02C7/24 ,  F02C3/04 ,  F02C7/20

    CPC classification number: F02C7/24 ,  F02C3/04 ,  F02C7/20 ,  F02C7/25 ,  F05D2220/32 ,  F05D2260/96

    Abstract: An electromechanical component arrangement for a gas turbine engine includes a mechanical component located at a first side of a firewall. An electronic module assembly of the electromechanical component is connected to the mechanical component and includes a housing, a mounting frame located in the housing and an electronic module secured to the mounting frame. The electronic module is operably connected to the mechanical component via a module cable. A vibration isolator is located in the housing to locate and support the mounting frame therein. The vibration isolator is configured to vibrationally isolate the electronic module from gas turbine engine vibrations. A cover plate is secured to the housing and the first side of the firewall, while the housing extends from the cover plate through a module opening in the firewall to a second side of the firewall having a lower operating temperature than the first side.

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