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    Optimization of Cross-Sectional Profile Shapes for Manufacture of Structural Parts
    1.
    发明申请
    Optimization of Cross-Sectional Profile Shapes for Manufacture of Structural Parts 有权

    公开(公告)号：US20220067223A1

    公开(公告)日：2022-03-03

    申请号：US17377084

    申请日：2021-07-15

    申请人： The Boeing Company

    发明人： Eric S Lester, JR. ,  Vivek Mohan ,  Venkata Narasimha Ravi Udali ,  Shobhit Rastogi ,  John Gilotti ,  John Henry Moselage, III

    IPC分类号： G06F30/10 ,  G06F16/953 ,  G06Q10/08 ,  G06N20/00 ,  G06N5/04

    摘要： A method of manufacturing a structural part includes accessing memory storing code for a software tool to determine a template profile for the structural part. The method includes executing the code to cause an apparatus to execute the software tool for accessing a 3D model of the structural part. The method also includes generating a profile from the 3D model and dimensioning the profile, and accessing and searching a database for stock profiles that match search criteria that include the dimension measurements of the profile set as lower bounds of the corresponding dimension measurements. The method also includes performing a decision analysis to evaluate attributes of the matching stock profiles and identify a selected stock profile. The method also includes outputting an indication of the selected stock profile for manufacturing the structural part from a stock structural part having a cross-sectional profile corresponding to the selected stock profile.

    Deployable apparatus for use with air vehicles
    3.
    发明授权
    Deployable apparatus for use with air vehicles 有权
    可用于机动车辆的可部署设备

    公开(公告)号：US09296470B1

    公开(公告)日：2016-03-29

    申请号：US13797115

    申请日：2013-03-12

    申请人： The Boeing Company

    发明人： John Henry Moselage, III

    IPC分类号： B64C1/10 ,  B64C7/00 ,  B64D1/02 ,  B64D1/14

    CPC分类号： B64C7/00 ,  A62C3/025 ,  B64D1/02 ,  B64D1/14 ,  F42B12/58 ,  F42B12/62 ,  F42B25/00

    摘要： An apparatus includes a first tube portion forming a portion of an air vehicle deployable pod and a second tube portion. The first and second tube portions are slidably coupled. The apparatus also includes a cavity formed between the tube portions. The second tube portion slides relative to the first tube portion to reduce the size of the cavity and dissipate energy upon impact of the first tube portion.

    摘要翻译： 一种装置包括形成气动车辆可展开的容器的一部分的第一管部分和第二管部分。 第一和第二管部分可滑动地联接。 该装置还包括在管部之间形成的空腔。 第二管部分相对于第一管部分滑动以减小空腔的尺寸并在第一管部分的冲击时耗散能量。