利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

22 条记录 (耗时 0.01 秒)

    Flight path control system for aircraft
    3.
    发明公开
    Flight path control system for aircraft 审中-公开
    Flugwegsteuersystemfürein Flugzeug

    公开(公告)号：EP2506109A2

    公开(公告)日：2012-10-03

    申请号：EP12162648.5

    申请日：2012-03-30

    申请人： The Boeing Company

    发明人： Harber, Benjamin A

    IPC分类号： G05D1/10

    CPC分类号： G05D1/105 ,  B64D17/34 ,  G01M1/127 ,  G05D1/0808

    摘要： A method and apparatus for changing a flight path of an air platform. A change for the flight path of the air platform is identified. A weight system associated with the air platform is moved during flight of the air platform such that a center of mass of the air platform changes in a manner that causes the flight path of the air platform to change.

    摘要翻译： 一种改变空中平台飞行路径的方法和装置。 确定了空中平台飞行路径的变化。 与空气平台相关联的重量系统在空中平台的飞行期间移动，使得空气平台的质心以使得空气平台的飞行路径改变的方式改变。

    INSTRUMENT DE SECOURS POUR TABLEAU DE BORD D'UN AÉRONEF DÉTECTANT LES SURCHARGES, NOTAMMENT EN PHASE D'ATTERRISSAGE
    5.
    发明公开
    INSTRUMENT DE SECOURS POUR TABLEAU DE BORD D'UN AÉRONEF DÉTECTANT LES SURCHARGES, NOTAMMENT EN PHASE D'ATTERRISSAGE 审中-公开
    FOR A平面仪表板辅机一种判别拥堵，尤其是在着陆阶段

    公开(公告)号：EP2064118A1

    公开(公告)日：2009-06-03

    申请号：EP07820251.2

    申请日：2007-09-17

    申请人： Thales

    发明人： PAPINEAU, Jérôme ,  COLLOT, Lionel

    IPC分类号： B64D43/00 ,  B64D45/00 ,  G01G19/07

    CPC分类号： G01G23/005 ,  B64D2045/008 ,  G01G19/07 ,  G01M1/127

    摘要： The present invention relates to a backup instrument fitted to the instrument panel of an aircraft to detect overload. The backup instrument comprises means for calculating and displaying flight information on the basis of data supplied by associated sensors (41, 42, 43, 45) incorporated into a backup system. It also comprises a module (403) that detects that the aircraft is overloaded on the basis of the data supplied to display the flight information. The invention applies in particular to the detection of overload during heavy landings. More generally, it applies to the detection and display of overloading of an aircraft in various types of environment.

    Method for real time estimation of aircraft center of gravity
    6.
    发明公开
    Method for real time estimation of aircraft center of gravity 失效
    Verfahren und Vorrichtung zurRealzeitschätzungvom Schwerpunkt eines Flugzeugs。

    公开(公告)号：EP0441007A2

    公开(公告)日：1991-08-14

    申请号：EP90203502.1

    申请日：1990-12-21

    申请人： THE BOEING COMPANY

    发明人： Orgun, Munir ,  Flannigan, Sean Joseph

    IPC分类号： G01M1/12 ,  G05D1/06

    CPC分类号： G01M1/127

    摘要： Disclosed is a method of and an arrangement for real time estimation of the location of the center of gravity of an aircraft. The center of gravity estimate is utilized in an aircraft flight control system for effecting flight control laws in which the center of gravity is a parameter that at least in part establishes open loop compensation or feedback gain. The disclosed method and arrangement are specifically adapted for establishing stabilizer mistrim during a landing procedure in which an aircraft flight control system is automatically controlling the aircraft. The method generally comprises the steps of generating a signal that represents the product of the aircraft stabilizer position and a multiplicative factor, A₁ and adding to that product an additive factor, A₂. The multiplicative factor, A₁, and the additive factor, A₂, both are determined on the basis of the angle of attack of the aircraft and the aircraft flap setting.

    摘要翻译： 公开了一种实时估计飞机重心位置的方法和装置。 重心估计用于飞行器飞行控制系统，用于实现飞行控制规则，其中重心是至少部分地建立开环补偿或反馈增益的参数。 所公开的方法和装置特别适用于在飞行器飞行控制系统自动控制飞机的着陆程序期间建立稳定器错误。 该方法通常包括以下步骤：产生表示飞行器稳定器位置和乘法因子A1的乘积的信号，并向该乘积加上加法因子A2。 乘法因子A1和加法因子A2都是基于飞机的迎角和飞机挡板设置来确定的。

    SYSTEMS AND METHODS FOR MANAGING CENTER OF GRAVITY
    7.
    发明公开
    SYSTEMS AND METHODS FOR MANAGING CENTER OF GRAVITY 有权

    公开(公告)号：EP3336506A1

    公开(公告)日：2018-06-20

    申请号：EP17205923.0

    申请日：2017-12-07

    申请人： Honeywell International Inc.

    发明人： GOWDA, Sushma

    IPC分类号： G01M1/12

    CPC分类号： B64D43/00 ,  G01C21/00 ,  G01M1/127 ,  G06F3/0482 ,  G06F3/14

    摘要： Systems and methods for managing a center of gravity of a vehicle on a display associated with the vehicle are provided. The method includes: determining an initial value of a center of gravity prior to a start of a journey, and receiving a value for a consumption of a fuel for the journey; determining, by a processor, a change in the center of gravity at each waypoint based on the initial value and the fuel consumed; generating a first user interface that illustrates the center of gravity at the waypoints over the journey and that illustrates that the change in the center of gravity exceeds a predefined threshold; based on the change in the center of gravity exceeding the predefined threshold, generating, a second user interface that provides a selection to bring the center of gravity below the predefined threshold; and updating the first user interface based on the selection.

    Flight path control system for aircraft
    8.
    发明公开
    Flight path control system for aircraft 审中-公开
    对于飞机的飞行路径控制系统

    公开(公告)号：EP2506109A3

    公开(公告)日：2014-03-12

    申请号：EP12162648.5

    申请日：2012-03-30

    申请人： The Boeing Company

    发明人： Harber, Benjamin A

    IPC分类号： G05D1/10 ,  B64D17/34 ,  G01M1/12

    CPC分类号： G05D1/105 ,  B64D17/34 ,  G01M1/127 ,  G05D1/0808

    摘要： A method and apparatus for changing a flight path of an air platform. A change for the flight path of the air platform is identified. A weight system associated with the air platform is moved during flight of the air platform such that a center of mass of the air platform changes in a manner that causes the flight path of the air platform to change.