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公开(公告)号：US10266250B2
公开(公告)日：2019-04-23
申请号：US15166478
申请日：2016-05-27
Applicant: Bell Helicopter Textron Inc.
Inventor： ShyhPyng Jack Shue
Abstract: In some embodiments, a control manager is disposed between the rotor system and the flight control inceptor. The control manager is configured to receive control commands wirelessly from a ground control station, translate the control commands into one or more axes associated with the flight control inceptor, and transmit the translated control commands to the rotor system in place of the instructions received from the pilot via the flight control inceptor.
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Patent Agency Ranking
公开(公告)号：US20160378121A1
公开(公告)日：2016-12-29
申请号：US14750746
申请日：2015-06-25
Applicant: Bell Helicopter Textron Inc.
Inventor： ShyhPyng Jack Shue
CPC classification number: G05D1/105 , G05D1/0072 , G05D1/0676 , G05D1/102 , G08G5/0013 , G08G5/0034 , G08G5/025
Abstract: Methods, systems, and apparatus, including computer programs encoded on a computer storage medium, for landing aircrafts with optimal landing spot selection. In one aspect, a method includes initiating an autorotation of an aircraft in response to detecting all engine failure, determining a plurality of flight characteristics and conditions of the aircraft at a time of initiating the autorotation, the plurality of flight characteristics and conditions comprising an aircraft altitude, an aircraft velocity, and wind direction, determining total air-time for glideslope and flare control, and a geographic area within which to land the aircraft by autorotation based on the plurality of flight characteristics and conditions, and controlling the aircraft to land the aircraft by autorotation within the geographic area.
Abstract translation: 方法，系统和装置，包括在计算机存储介质上编码的计算机程序，用于着陆具有最佳着陆点选择的飞机。 在一个方面，一种方法包括响应于检测到所有发动机故障，确定在启动自转时的飞行器的多个飞行特性和状况，启动航空器的自动转换，所述飞行特征和条件包括飞行器 高度，飞机速度和风向，确定滑坡和火炬控制的总时间，以及基于多个飞行特征和条件通过自转落地飞机的地理区域，并且控制飞机着陆 飞机在地理区域内自转。
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公开(公告)号：US09645582B2
公开(公告)日：2017-05-09
申请号：US14750746
申请日：2015-06-25
Applicant: Bell Helicopter Textron Inc.
Inventor： ShyhPyng Jack Shue
CPC classification number: G05D1/105 , G05D1/0072 , G05D1/0676 , G05D1/102 , G08G5/0013 , G08G5/0034 , G08G5/025
Abstract: Methods, systems, and apparatus, including computer programs encoded on a computer storage medium, for landing aircrafts with optimal landing spot selection. In one aspect, a method includes initiating an autorotation of an aircraft in response to detecting all engine failure, determining a plurality of flight characteristics and conditions of the aircraft at a time of initiating the autorotation, the plurality of flight characteristics and conditions comprising an aircraft altitude, an aircraft velocity, and wind direction, determining total air-time for glideslope and flare control, and a geographic area within which to land the aircraft by autorotation based on the plurality of flight characteristics and conditions, and controlling the aircraft to land the aircraft by autorotation within the geographic area.
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公开(公告)号：US20160209290A1
公开(公告)日：2016-07-21
申请号：US14598986
申请日：2015-01-16
Applicant: Bell Helicopter Textron Inc.
Inventor： ShyhPyng Jack Shue
CPC classification number: G01M1/127 , B64C19/00 , B64C27/28 , B64C29/0033
Abstract: A computer-implemented method for determining center of gravity of a tiltrotor aircraft includes storing a multi-dimensional matrix mapping multiple tiltrotor aircraft parameters to a plurality of three-dimensional (3D) centers of gravity of the tiltrotor aircraft, where each 3D center of gravity includes a respective longitudinal center of gravity, lateral center of gravity, and vertical center of gravity. The method includes receiving input signals from corresponding on-board sensors, where the input signals represent characteristics of the tiltrotor aircraft, determining tiltrotor aircraft parameters from the input signals, identifying, from the multi-dimensional matrix mapping, a longitudinal center of gravity, a lateral center of gravity, and a vertical center of gravity that corresponds to the determined tiltrotor aircraft parameters, and providing the identified longitudinal center of gravity, the identified lateral center of gravity, and the identified vertical center of gravity in response to receiving the input signals.
Abstract translation: 用于确定倾斜旋翼飞行器的重心的计算机实现的方法包括存储将多个倾斜旋转飞机参数映射到多个三维（3D）重心的倾斜旋翼飞机重心的多维矩阵，其中每个3D重心 包括相应的纵向重心，横向重心和垂直重心。 该方法包括从相应的车载传感器接收输入信号，其中输入信号表示倾斜旋翼飞行器的特性，根据输入信号确定倾斜旋翼飞行器参数，从多维矩阵映射识别纵向重心， 横向重心和垂直重心对应于所确定的倾斜旋翼飞行器参数，并且响应于接收到输入信号而提供所识别的纵向重心，所识别的横向重心和所识别的垂直重心 。
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公开(公告)号：US20170036753A1
公开(公告)日：2017-02-09
申请号：US15166478
申请日：2016-05-27
Applicant: Bell Helicopter Textron Inc.
Inventor： ShyhPyng Jack Shue
CPC classification number: B64C13/22 , B64C13/04 , B64C13/20 , B64C29/0033 , B64C39/024 , B64D45/0015 , B64D2045/0055 , G05D1/0022 , G05D1/0061 , G05D1/0858
Abstract: In some embodiments, a control manager is disposed between the rotor system and the flight control inceptor. The control manager is configured to receive control commands wirelessly from a ground control station, translate the control commands into one or more axes associated with the flight control inceptor, and transmit the translated control commands to the rotor system in place of the instructions received from the pilot via the flight control inceptor.
Abstract translation: 在一些实施例中，控制管理器设置在转子系统和飞行控制受体之间。 控制管理器被配置为从地面控制站无线地接收控制命令，将控制命令转换成与飞行控制受体相关联的一个或多个轴，并将转换的控制命令传送到转子系统，代替从 飞行员通过飞行控制受体。
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公开(公告)号：US09464958B2
公开(公告)日：2016-10-11
申请号：US14598986
申请日：2015-01-16
Applicant: Bell Helicopter Textron Inc.
Inventor： ShyhPyng Jack Shue
CPC classification number: G01M1/127 , B64C19/00 , B64C27/28 , B64C29/0033
Abstract: A computer-implemented method for determining center of gravity of a tiltrotor aircraft includes storing a multi-dimensional matrix mapping multiple tiltrotor aircraft parameters to a plurality of three-dimensional (3D) centers of gravity of the tiltrotor aircraft, where each 3D center of gravity includes a respective longitudinal center of gravity, lateral center of gravity, and vertical center of gravity. The method includes receiving input signals from corresponding on-board sensors, where the input signals represent characteristics of the tiltrotor aircraft, determining tiltrotor aircraft parameters from the input signals, identifying, from the multi-dimensional matrix mapping, a longitudinal center of gravity, a lateral center of gravity, and a vertical center of gravity that corresponds to the determined tiltrotor aircraft parameters, and providing the identified longitudinal center of gravity, the identified lateral center of gravity, and the identified vertical center of gravity in response to receiving the input signals.
Abstract translation: 用于确定倾斜旋翼飞行器的重心的计算机实现的方法包括存储将多个倾斜旋转飞机参数映射到多个三维（3D）重心的倾斜旋翼飞机重心的多维矩阵，其中每个3D重心 包括相应的纵向重心，横向重心和垂直重心。 该方法包括从相应的车载传感器接收输入信号，其中输入信号表示倾斜旋翼飞行器的特性，根据输入信号确定倾斜旋翼飞行器参数，从多维矩阵映射识别纵向重心， 横向重心和垂直重心对应于所确定的倾斜旋翼飞行器参数，并且响应于接收到输入信号而提供所识别的纵向重心，所识别的横向重心和所识别的垂直重心 。
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