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公开(公告)号：US09121487B2
公开(公告)日：2015-09-01
申请号：US14079445
申请日：2013-11-13
Applicant: HONEYWELL INTERNATIONAL, INC.
Inventor： Robert E. De Mers , Olukayode Olofinboba , Keith Hughes , Joseph Ott , Alan Griesbach
CPC classification number: F16H59/02 , B64C13/04 , B64C25/405 , B64D31/04 , F16H61/0202 , G05G1/00 , Y02T50/823 , Y10T74/20085 , Y10T74/2011
Abstract: A pilot interface panel may comprise at least one input mechanism configured to receive at least one user input, generate at least one input signal corresponding to the at least one user input, and send the at least one input signal to a controller. The controller may be configured to control movement of an electric taxi system of an aircraft in a manner according to the at least one input signal, wherein the electric taxi system may be configured to rotate at least one wheel of the aircraft by force from a purely electromotive source. The pilot interface panel may further comprise at least one safety mechanism, which may be configured to prevent at least one of the at least one input mechanisms from receiving an inadvertent user input resulting from an unintended action by the user.
Abstract translation: 导频接口面板可以包括至少一个输入机构，其被配置为接收至少一个用户输入，产生对应于至少一个用户输入的至少一个输入信号，并将至少一个输入信号发送到控制器。 控制器可以被配置成以根据至少一个输入信号的方式控制飞行器的电动滑行系统的移动，其中电动滑行系统可以被配置成通过强制从一个纯粹的方式旋转飞行器的至少一个车轮 电动源。 导频接口面板还可以包括至少一个安全机构，其可以被配置为防止至少一个输入机构中的至少一个输入机构接收由用户的非预期动作导致的无意的用户输入。
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公开(公告)号：US20150183511A1
公开(公告)日：2015-07-02
申请号：US14141150
申请日：2013-12-26
Applicant: Honeywell International Inc.
Inventor： Joseph Ott , Keith Hughes , Robert E. De Mers , Olukayode Olofinboba
CPC classification number: B64C19/00 , B64C25/405 , B64D31/04 , Y02T50/823
Abstract: A lever control system integrates taxi operation using an electric motor in an aircraft with speed control of a jet engine in the same aircraft. The lever control system provides a smooth transition between the electric motor system used for aircraft taxi operation, and a jet engine system used to fly the aircraft. The lever control system may include a reverse lockout mechanism to prevent unintended reverse taxi movement of the aircraft.
Abstract translation: 杠杆控制系统将飞机中的电动机的出租车操作与在同一架飞机上的喷气发动机的速度控制相结合。 杠杆控制系统提供用于飞机出租车操作的电动马达系统和用于飞行飞机的喷气发动机系统之间的平滑过渡。 杠杆控制系统可以包括反向锁定机构，以防止飞机的意外的反向出租车运动。
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公开(公告)号：US20150210383A1
公开(公告)日：2015-07-30
申请号：US14163332
申请日：2014-01-24
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Robert E. De Mers , Olukayode Olofinboba , Keith Hughes , Joseph Ott
CPC classification number: B64C25/405 , B64D31/04 , Y02T50/823
Abstract: An electric taxi system (ETS) for an aircraft may include a ground speed sensor, a speed selection unit and a speed computer coupled to the ground speed sensor and to the speed selection unit. The speed computer may produce a speed error signal. A motor controller coupled to a wheel motor may control speed of the wheel motor responsively to the speed error signal.
Abstract translation: 用于飞机的电动出租车系统（ETS）可以包括地面速度传感器，速度选择单元和耦合到地面速度传感器和速度选择单元的速度计算机。 速度计算机可能产生速度误差信号。 耦合到车轮电动机的电动机控制器可以响应于速度误差信号来控制车轮电动机的速度。
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公开(公告)号：US09457896B2
公开(公告)日：2016-10-04
申请号：US14163332
申请日：2014-01-24
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Robert E. De Mers , Olukayode Olofinboba , Keith Hughes , Joseph Ott
CPC classification number: B64C25/405 , B64D31/04 , Y02T50/823
Abstract: An electric taxi system (ETS) for an aircraft may include a ground speed sensor, a speed selection unit and a speed computer coupled to the ground speed sensor and to the speed selection unit. The speed computer may produce a speed error signal. A motor controller coupled to a wheel motor may control speed of the wheel motor responsively to the speed error signal.
Abstract translation: 用于飞机的电动出租车系统（ETS）可以包括地面速度传感器，速度选择单元和耦合到地面速度传感器和速度选择单元的速度计算机。 速度计算机可能产生速度误差信号。 耦合到车轮电动机的电动机控制器可以响应于速度误差信号来控制车轮电动机的速度。
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