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    TRANSLATING COWL THRUST REVERSER WITH DOOR PIVOTS AFT OF REVERSE FLOW PATH
    3.
    发明申请
    TRANSLATING COWL THRUST REVERSER WITH DOOR PIVOTS AFT OF REVERSE FLOW PATH 审中-公开
    翻转车轮倒车者与门面转弯逆行道路

    公开(公告)号：US20160305370A1

    公开(公告)日：2016-10-20

    申请号：US14688779

    申请日：2015-04-16

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Danis Burton Smith ,  Mark Knowles ,  Robert Romano ,  Shawn Alstad ,  David Robinson ,  Israel Picazo

    IPC: F02K1/60 ,  F02K1/72

    CPC classification number: F02K1/605 ,  F02K1/72 ,  Y02T50/671

    Abstract: A thrust reverser system capable of providing high efficiency within a tightly constrained nacelle is provided. The thrust reverser system provides a displaceable internal door pivotally mounted within a transcowl. The displaceable internal door is rotatable about a pivot axis that is positioned aft of a front edge of the transcowl when the transcowl is in a deployed position.

    Abstract translation: 提供了能够在紧密限制的机舱内提供高效率的推力反向器系统。 推力反向器系统提供可枢转地安装在转子内的可移动内门。 可移动的内部门可以围绕枢转轴线旋转，当枢轴转动器处于展开位置时，该枢转轴线定位在转子的前边缘的后方。

    NACELLE INLET AND ENGINE FAN HOUSING ASSEMBLY AND METHOD FOR MAKING SAME
    4.
    发明申请
    NACELLE INLET AND ENGINE FAN HOUSING ASSEMBLY AND METHOD FOR MAKING SAME 审中-公开
    NACELLE入口和发动机风扇壳体组件及其制造方法

    公开(公告)号：US20160084108A1

    公开(公告)日：2016-03-24

    申请号：US14494868

    申请日：2014-09-24

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Justin C. Mickelsen ,  Shawn Alstad ,  Mark Knowles ,  Bill Russell Watson

    IPC: F01D25/04 ,  F01D25/24

    CPC classification number: F01D25/04 ,  F01D25/24 ,  F02C7/045 ,  F05D2220/36 ,  F05D2230/53 ,  F05D2230/70 ,  F05D2230/72 ,  F05D2260/96

    Abstract: A system and method is provided for coupling a nacelle inlet assembly to an engine fan housing structure that provides adequate clearance and access for removing a blisk fan from a turbofan engine. This is accomplished by utilizing a nacelle inlet forward compartment, referred to herein as the “D-lip”and an acoustic liner that are inseparable and removable as an integral unit, providing sufficient clearance for removable of the blisk fan. The nacelle inlet assembly may be slidably coupled to the engine fan housing structure, minimizing assembly interfaces and therefore overall aircraft engine weight.

    Abstract translation: 提供了一种用于将机舱入口组件耦合到发动机风扇壳体结构的系统和方法，该发动机风扇壳体结构提供足够的间隙和通路以从涡轮风扇发动机移除叶轮风扇。 这是通过利用这里称为“D唇”的机舱前进舱和作为整体单元不可分离和可拆卸的声学衬垫来实现的，为空挡风扇提供足够的间隙。 机舱入口组件可以可滑动地联接到发动机风扇壳体结构，使组装界面最小化，从而使整个飞机发动机重量最小化。

    Translating cowl thrust reverser that prevents unintended door rotation
    5.
    发明授权
    Translating cowl thrust reverser that prevents unintended door rotation 有权

    公开(公告)号：US10451002B2

    公开(公告)日：2019-10-22

    申请号：US15004020

    申请日：2016-01-22

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Danis Burton Smith ,  Mark Knowles ,  Robert Romano ,  Shawn Alstad ,  David Robinson

    IPC: F02K1/70 ,  F02K1/62 ,  F02K1/68 ,  F01D25/24 ,  F01D25/28 ,  F02K1/72 ,  F02K1/76

    Abstract: A thrust reverser system for a turbine engine includes a support structure, a transcowl, a door, and an anti-rotation structure. The transcowl is mounted on the support structure and has an inner surface. The transcowl is axially translatable, relative to the support structure, between first and second positions. The door is pivotally coupled to the turbine engine, and has a forward edge and an aft edge. The door is rotatable between stowed and deployed positions when the transcowl translates between the first and second positions, respectively. The anti-rotation structure extends from the transcowl and is disposed adjacent to the aft edge of the door when the transcowl is in the first position and the door is in the stowed position. The anti-rotation structure is configured such that door rotation out of the stowed position only occurs subsequent to or concurrently with translation of the transcowl out of the first position.

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