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    Method and device for determining a backup altitude of an aircraft
    1.
    发明授权
    Method and device for determining a backup altitude of an aircraft 有权

    公开(公告)号：US10883825B2

    公开(公告)日：2021-01-05

    申请号：US16148511

    申请日：2018-10-01

    申请人： Airbus Operations SAS

    发明人： Martin Delporte ,  Guillaume Alcalay

    IPC分类号： G01C5/06 ,  G01L7/12 ,  G01C5/00 ,  G01C21/00 ,  G05D1/04 ,  G01C23/00 ,  G05D1/00

    摘要： A determining method comprises a first computing step implemented by a computational module to compute a static pressure from an altitude determined by a geolocation module, a receiving step implemented by a reception module to receive a static pressure determined by a static pressure sensor, a second computing step implemented by a second computational module to compute a static pressure difference between the static pressure and the static pressure, a step of filtering the static pressure difference, a third computing step implemented by a third computational module in order to compute the backup altitude from the filtered static pressure difference and from the static pressure, and a sending step implemented by a sending module in order to deliver the computed backup altitude to a user device.

    METHOD AND DEVICE FOR ESTIMATING THE MACH NUMBER OF AN AIRCRAFT
    2.
    发明申请
    METHOD AND DEVICE FOR ESTIMATING THE MACH NUMBER OF AN AIRCRAFT 有权
    用于估计飞机数量的方法和装置

    公开(公告)号：US20160025764A1

    公开(公告)日：2016-01-28

    申请号：US14805131

    申请日：2015-07-21

    申请人： Airbus Operations (SAS)

    发明人： Maxime Semat ,  Martin Delporte

    IPC分类号： G01P5/175

    CPC分类号： G01P5/175 ,  G01P5/14 ,  G01P13/025

    摘要： A measurement unit for measuring a first static pressure of the ambient air in a first measurement zone of the aircraft, a measurement unit for measuring a second pressure of the ambient air, at least one static pressure probe, in a second measurement zone of the aircraft, the second pressure having a value lower than the first static pressure, a computation unit for estimating a Mach number using these two measured pressures and a data transmission unit configured to transmit the estimated Mach number to a user system.

    摘要翻译： 一种用于测量飞行器的第一测量区域中的环境空气的第一静态压力的测量单元，用于在飞行器的第二测量区域中测量环境空气的第二压力的测量单元，至少一个静压探头 所述第二压力具有比所述第一静压低的值，用于使用这两个测量压力估计马赫数的计算单元和被配置为将所估计的马赫数发送给用户系统的数据传输单元。

    Method and device for aiding the control of an aircraft during a parabolic flight in order to generate weightlessness in the aircraft
    3.
    发明授权
    Method and device for aiding the control of an aircraft during a parabolic flight in order to generate weightlessness in the aircraft 有权
    用于在抛物线飞行期间帮助飞行器的控制以在飞行器中产生失重的方法和装置

    公开(公告)号：US09321523B2

    公开(公告)日：2016-04-26

    申请号：US14482513

    申请日：2014-09-10

    申请人： AIRBUS OPERATIONS (SAS)

    发明人： Martin Delporte

    IPC分类号： B64C13/04 ,  G01C23/00 ,  G05D1/06

    CPC分类号： B64C13/04 ,  G01C23/00 ,  G01C23/005 ,  G05D1/0607

    摘要： A method and device are disclosed for aiding the control of an aircraft during a parabolic flight in order to generate weightlessness in the aircraft. The device includes a unit for automatically calculating a control stick order corresponding to a current optimum position of the control stick for carrying out a parabolic flight, a unit for automatically determining an actual position of the control stick, and a display unit for automatically displaying, on at least one scale that is displayed on a cockpit screen, simultaneously a first indicator corresponding to the control stick order and a second indicator corresponding to the actual position of the control stick.

    摘要翻译： 公开了一种用于在抛物线飞行期间帮助飞行器的控制以便在飞行器中产生失重的方法和装置。 该装置包括用于自动计算与用于执行抛物面飞行的控制棒的当前最佳位置相对应的控制杆顺序的单元，用于自动确定控制棒的实际位置的单元，以及用于自动显示控制棒的显示单元， 在显示在驾驶舱屏幕上的至少一个刻度上，同时具有对应于控制杆顺序的第一指示器和对应于控制棒的实际位置的第二指示器。