System and Method for Determining a Center of Gravity of an Aircraft
    1.
    发明申请
    System and Method for Determining a Center of Gravity of an Aircraft 有权
    确定飞机重力中心的系统和方法

    公开(公告)号:US20090064769A1

    公开(公告)日:2009-03-12

    申请号:US12167983

    申请日:2008-07-03

    IPC分类号: B64C17/02

    CPC分类号: G01M1/125

    摘要: According to one embodiment of the disclosure, a method of determining a center of gravity of an aircraft includes receiving a strut length for each of the gears of an aircraft, determining an arm length for each of the gears, and determining a center of gravity of the aircraft based on a relationship between the center of gravity and respective arm lengths for each of the gears. The arm length of each of the gears is determined according to the strut length of a gear strut of a respective gear and a relationship between the strut length of the gear strut to another gear of another aircraft and the arm length of the respective gear.

    摘要翻译: 根据本公开的一个实施例,一种确定飞行器重心的方法包括:接收用于飞行器的每个齿轮的支柱长度,确定每个齿轮的臂长度,以及确定重心的重心 基于重心之间的关系和每个齿轮的相应臂长度的飞机。 每个齿轮的臂长根据相应齿轮的齿轮支柱的支柱长度和齿轮支柱的支柱长度与另一架飞机的另一个齿轮之间的关系以及相应齿轮的臂长度确定。

    System and method for determining a center of gravity of an aircraft
    2.
    发明授权
    System and method for determining a center of gravity of an aircraft 有权
    用于确定飞行器重心的系统和方法

    公开(公告)号:US07890249B2

    公开(公告)日:2011-02-15

    申请号:US12167983

    申请日:2008-07-03

    IPC分类号: G06G7/70 G01M1/12 G06F17/17

    CPC分类号: G01M1/125

    摘要: According to one embodiment of the disclosure, a method of determining a center of gravity of an aircraft includes receiving a strut length for each of the gears of an aircraft, determining an arm length for each of the gears, and determining a center of gravity of the aircraft based on a relationship between the center of gravity and respective arm lengths for each of the gears. The arm length of each of the gears is determined according to the strut length of a gear strut of a respective gear and a relationship between the strut length of the gear strut to another gear of another aircraft and the arm length of the respective gear.

    摘要翻译: 根据本公开的一个实施例,一种确定飞行器重心的方法包括:接收用于飞行器的每个齿轮的支柱长度,确定每个齿轮的臂长度,以及确定重心的重心 基于重心之间的关系和每个齿轮的相应臂长度的飞行器。 每个齿轮的臂长根据相应齿轮的齿轮支柱的支柱长度和齿轮支柱的支柱长度与另一架飞机的另一个齿轮之间的关系以及相应齿轮的臂长度确定。