-
Patent Agency Ranking
公开(公告)号：US08880245B2
公开(公告)日：2014-11-04
申请号：US13956872
申请日：2013-08-01
Applicant: Airbus Operations (S.A.S.)
Inventor： Charles Renault Leberquer , Florian Constans , Josep Boada-Bauxell , Pascale Louise
CPC classification number: B64C19/00 , G01C23/00 , G05D1/042 , G05D1/0607
Abstract: The device comprises servocontrol means which automatically control, in a combined manner, an automatic thrust system of the aircraft and airbrakes of the aircraft, as a supplement to usual means for steering the vertical trajectory, so that the aircraft attains a speed setpoint and/or altitude setpoint, at the location defined by a geographical constraint.
Abstract translation: 该装置包括伺服控制装置，其以组合的方式自动控制飞行器的自动推力系统和飞行器的空气制动器，作为用于转向垂直轨迹的通常装置的补充，使得飞行器达到速度设定点和/或 高度设定点，在由地理约束定义的位置。
-
2.发明申请公开(公告)号：US20140039731A1
公开(公告)日：2014-02-06
申请号：US13956872
申请日：2013-08-01
Applicant: AIRBUS OPERATIONS (S.A.S.)
Inventor： Charles Renault Leberquer , Florian Constans , Josep Boada-Bauxell , Pascale Louise
IPC: B64C19/00
CPC classification number: B64C19/00 , G01C23/00 , G05D1/042 , G05D1/0607
Abstract: The device comprises servocontrol means which automatically control, in a combined manner, an automatic thrust system of the aircraft and airbrakes of the aircraft, as a supplement to usual means for steering the vertical trajectory, so that the aircraft attains a speed setpoint and/or altitude setpoint, at the location defined by a geographical constraint.
Abstract translation: 该装置包括伺服控制装置，其以组合的方式自动控制飞行器的自动推力系统和飞行器的空气制动器，作为用于转向垂直轨迹的通常装置的补充，使得飞行器达到速度设定点和/或 高度设定点，在由地理约束定义的位置。
-
公开(公告)号：US09862499B2
公开(公告)日：2018-01-09
申请号：US15137891
申请日：2016-04-25
Applicant: Airbus Operations (S.A.S.)
Inventor： Florian Constans , Mathieu Deroo , Benjamin Mazoin
Abstract: A human machine interface linked to the throttle lever of an aircraft used to control the energy of an aircraft is disclosed. The HMI has upper part, which corresponds to the forward stroke of the lever, and a lower part, which corresponds to the rearward stroke of the lever. An upper shutter is positioned over the upper part, and a lower shutter is positioned over the lower part. A “cursor” acts as a visual representation in the HMI of the lever and its handle. The cursor moves forward or backward as the pilot acts on the lever/handle. The cursor indicates an ordered release of more or less aircraft energy, depending on its position on the display. The upper and lower shutters also indicate the ordered release of more or less aircraft energy, depending on the respective lengths of the two shutters. The HMI also includes a column in the display having a length symbolizing a current value in actual aircraft push or braking, depending on whether an aircraft push or braking has been ordered by releasing of more or less aircraft energy. The column changes in length as the actual aircraft push or braking changes. The cursor is further depicted in the HMI display as containing a memorizing button on the handle and a Go-Lever button on the lever below the handle.
-
公开(公告)号：US09550562B2
公开(公告)日：2017-01-24
申请号：US14283290
申请日：2014-05-21
Applicant: Airbus Operations S.A.S.
Inventor： Florian Constans , Josep Boada-Bauxell , Pierre Scacchi
Abstract: A system for controlling an aircraft control parameter including a control interface including a mobile element configured to move on a travel, of which at least two portions are separated by a neutral position; a return element bringing the mobile element back to the neutral position when it is not actuated; and an interaction element, and a control unit configured to memorize an item of information corresponding to a first position of the mobile element at an instant of activation of the interaction element; and generate a setpoint of the aircraft control parameter, as a function of a control associated with the first position of the mobile element for which said information has been memorized; or a current position of the mobile element, when this current position is situated on the same portion of travel as the first position and is more remote than the latter from the neutral position.
Abstract translation: 一种用于控制飞行器控制参数的系统，其包括控制接口，所述控制接口包括被配置为在行程上移动的移动元件，其中至少两个部分被中立位置分隔; 返回元件，当移动元件未被启动时返回到中立位置; 以及控制单元，被配置为在所述交互元件的激活时刻存储对应于所述移动元件的第一位置的信息项; 并且根据与已经存储了所述信息的移动元件的第一位置相关联的控制来生成飞行器控制参数的设定点; 或当该当前位置位于与第一位置相同的行进部分上并且比中立位置更远离移动元件的当前位置时，移动元件的当前位置。
-
公开(公告)号：US20140346280A1
公开(公告)日：2014-11-27
申请号：US14283290
申请日：2014-05-21
Applicant: AIRBUS OPERATIONS S.A.S.
Inventor： Florian Constans , Josep Boada-Bauxell , Pierre Scacchi
Abstract: A system for controlling an aircraft control parameter including a control interface including a mobile element configured to move on a travel, of which at least two portions are separated by a neutral position; a return element bringing the mobile element back to the neutral position when it is not actuated; and an interaction element, and a control unit configured to memorize an item of information corresponding to a first position of the mobile element at an instant of activation of the interaction element; and generate a setpoint of the aircraft control parameter, as a function of a control associated with the first position of the mobile element for which said information has been memorized; or a current position of the mobile element, when this current position is situated on the same portion of travel as the first position and is more remote than the latter from the neutral position.
Abstract translation: 一种用于控制飞行器控制参数的系统，其包括控制接口，所述控制接口包括被配置为在行程上移动的移动元件，其中至少两个部分被中立位置分隔; 返回元件，当移动元件未被启动时返回到中立位置; 以及控制单元，被配置为在所述交互元件的激活时刻存储对应于所述移动元件的第一位置的信息项; 并且根据与已经存储了所述信息的移动元件的第一位置相关联的控制来生成飞行器控制参数的设定点; 或当该当前位置位于与第一位置相同的行进部分上并且比中立位置更远离移动元件的当前位置时，移动元件的当前位置。
-
-
-
-
Search Results
5
records
(took 0.035 seconds)
