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    SYSTEM AND METHOD OF PROTECTION OF AIRCRAFT FROM FOREIGN OBJECT STRIKES
    2.
    发明申请
    SYSTEM AND METHOD OF PROTECTION OF AIRCRAFT FROM FOREIGN OBJECT STRIKES 审中-公开

    公开(公告)号：US20200047915A1

    公开(公告)日：2020-02-13

    申请号：US16102229

    申请日：2018-08-13

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Michael Smith ,  Cheng-Ho Tho ,  Anand Kumar Marimuthu

    IPC: B64D45/00 ,  B64C1/12

    Abstract: An aircraft structure protected from collisions with foreign objects includes a first support proximate to an aircraft structure root; first sheets attached to the first support to form a first leading edge portion of the aircraft structure; a second support proximate to an outer end of the aircraft structure; second sheets attached to the second support to form a second leading edge portion; and a door including one or more ribs disposed between the first and second supports and configured to give shape to a third leading edge portion of the aircraft structure; and third sheets, attached to the ribs to form the third portion of the leading edge; wherein the first support, the first sheets, the second support, the second sheets, the one or more ribs, and the third sheets are disposed to mitigate damage from a foreign object collision by absorbing kinetic energy from a collision.

    System and method of protection of aircraft from foreign object strikes
    6.
    发明授权
    System and method of protection of aircraft from foreign object strikes 有权

    公开(公告)号：US11548655B2

    公开(公告)日：2023-01-10

    申请号：US16102229

    申请日：2018-08-13

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Michael Smith ,  Cheng-Ho Tho ,  Anand Kumar Marimuthu

    IPC: B64D45/00 ,  B64C1/12 ,  B64C1/00

    Abstract: An aircraft structure protected from collisions with foreign objects includes a first support proximate to an aircraft structure root; first sheets attached to the first support to form a first leading edge portion of the aircraft structure; a second support proximate to an outer end of the aircraft structure; second sheets attached to the second support to form a second leading edge portion; and a door including one or more ribs disposed between the first and second supports and configured to give shape to a third leading edge portion of the aircraft structure; and third sheets, attached to the ribs to form the third portion of the leading edge; wherein the first support, the first sheets, the second support, the second sheets, the one or more ribs, and the third sheets are disposed to mitigate damage from a foreign object collision by absorbing kinetic energy from a collision.

    CABLE CUTTER SYSTEM
    8.
    发明申请
    CABLE CUTTER SYSTEM 有权
    电缆切割机系统

    公开(公告)号：US20160096621A1

    公开(公告)日：2016-04-07

    申请号：US14506286

    申请日：2014-10-03

    Applicant: Bell Helicopter Textron Inc.

    Inventor： Michael Smith ,  Cheng-Ho Tho ,  Anand Kumar Marimuthu

    IPC: B64C27/00

    CPC classification number: B64C27/006 ,  B26D1/12 ,  B26D1/25 ,  B26D2001/006 ,  B26D2001/0066

    Abstract: Some examples of a cable cutting system include a first cutting apparatus that includes a recess to receive a cable. The system includes a second cutting apparatus separate from and attached to the first cutting apparatus. The second cutting apparatus includes multiple cutting surfaces arranged to cut the cable received at the recess.

    Abstract translation: 电缆切割系统的一些示例包括第一切割装置，其包括用于接收电缆的凹部。 该系统包括与第一切割装置分离并附接到第一切割装置的第二切割装置。 第二切割装置包括多个切割表面，其设置成切割在凹部处接收的电缆。

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