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公开(公告)号：US20220065318A1
公开(公告)日：2022-03-03
申请号：US17006372
申请日：2020-08-28
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Daniel Petschow , Stephen Abel , Kevin Gardner
IPC: F16F1/12
Abstract: In exemplary embodiments, a caged spring assembly is provided that includes a first end cap, a second end cap, a helical spring, and a locking post. The second end cap is opposite the first end cap. The helical spring extends between the first and second end caps. The locking post is disposed inside the helical spring between the first and second end caps. The locking post allows limited compression of the helical spring and prevents extension of the helical spring beyond a set point.
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2.发明申请AIRCRAFT ELECTRIC TAXI SYSTEM DIAGNOSTIC AND PROGNOSTIC EVALUATION SYSTEM AND METHOD 有权飞机电力系统诊断与预警评估系统及方法公开(公告)号：US20160086396A1
公开(公告)日：2016-03-24
申请号：US14490495
申请日：2014-09-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Joseph Nutaro , Stephen Abel , Grant Gordon
CPC classification number: G07C5/0808 , B64C25/405 , Y02T50/823
Abstract: An aircraft electric taxi system diagnostics and prognostics evaluation method, including receiving, with a computer, an electronically recorded first performance parameter of a first electric taxi system of a first aircraft during a taxi operational event at an airport; and comparing the first performance parameter with a first performance factor statistical model generated in response to the first performance parameter and first comparative performance parameters; and calculating a first performance parameter difference based on the comparison.
Abstract translation: 一种飞机电动出租车系统诊断和预测评估方法，包括在机场的出租车操作事件期间用计算机接收第一飞机的第一电动出租车系统的电子记录的第一性能参数; 以及将所述第一性能参数与响应于所述第一性能参数和所述第一性能参数产生的第一性能因子统计模型进行比较; 以及基于所述比较来计算第一性能参数差异。
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公开(公告)号：US20150375854A1
公开(公告)日：2015-12-31
申请号：US14317112
申请日：2014-06-27
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Stephen Abel , David Lazarovich , Joseph Nutaro
CPC classification number: B64C25/405 , Y02T50/823
Abstract: An aircraft taxi control system may include a left main gear (MG) drive motor, a right MG motor, a first motor drive controller configured to produce a left motor torque signal responsively to nose gear angle (NGA) and nose wheel speed (NGS), and a second motor drive controller configured to produce a right motor toque signal responsively to the NGA and the NGS. The left motor torque signal and the right motor torque signal may be coordinated to reduce lateral loading of the nose wheel during a turning maneuver.
Abstract translation: 飞机出租车控制系统可以包括左主齿轮（MG）驱动马达，右MG马达，第一马达驱动控制器，其构造成响应于前档角（NGA）和前轮速度（NGS）产生左电机转矩信号， 以及第二电动机驱动控制器，被配置为响应于NGA和NGS产生正确的电动机转矩信号。 可以协调左电动机转矩信号和右电动机转矩信号以减少转向操纵期间前轮的横向负载。
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公开(公告)号：US09811950B2
公开(公告)日：2017-11-07
申请号：US14490495
申请日：2014-09-18
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Joseph Nutaro , Stephen Abel , Grant Gordon
CPC classification number: G07C5/0808 , B64C25/405 , Y02T50/823
Abstract: An aircraft electric taxi system diagnostics and prognostics evaluation method, including receiving, with a computer, an electronically recorded first performance parameter of a first electric taxi system of a first aircraft during a taxi operational event at an airport; and comparing the first performance parameter with a first performance factor statistical model generated in response to the first performance parameter and first comparative performance parameters; and calculating a first performance parameter difference based on the comparison.
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