首页> 外国专利> METHOD TO RECOVER NON-RECOGNIZED ERRORS IN AIRCRAFT WEIGHT DETERMINATIONS TO INCREASE WEIGHT AND CENTER OF GRAVITY LIMITATIONS FOR REGULATED AIRCRAFT

METHOD TO RECOVER NON-RECOGNIZED ERRORS IN AIRCRAFT WEIGHT DETERMINATIONS TO INCREASE WEIGHT AND CENTER OF GRAVITY LIMITATIONS FOR REGULATED AIRCRAFT

机译:恢复飞机重量确定中无法识别的误差以增加重量和调节飞机重力极限的方法

摘要

A method of establishing a justification basis to Aircraft Regulatory Authorities, to allow a regulated aircraft to operate at increased maximum weight limitations, through the statistical identification of non-recognized weight errors being allowed in today's aircraft weight determination methods, with the recovery and utilization of the non-recognized weight errors to increase weight limitations through a Regulatory Authority finding of an Equivalent Level of Safety. A system for use in measuring aircraft weight and center of gravity, providing a method to reveal non-recognized weight errors. Sensors are attached to the landing gear struts, so to periodically and randomly measure and monitor aircraft weight and center of gravity.
机译:一种方法,通过对当今飞机重量确定方法中允许的无法识别的重量误差进行统计识别,并恢复和利用航空器管理当局的理由,从而使受管制的飞机在增加的最大重量限制下运行。通过监管机构发现的等效安全水平,发现无法识别的重量错误,从而增加了重量限制。一种用于测量飞机重量和重心的系统,提供一种揭示无法识别的重量误差的方法。传感器安装在起落架支柱上,以便定期和随机地测量和监控飞机的重量和重心。

著录项

  • 公开/公告号US2017116617A1

    专利类型

  • 公开/公告日2017-04-27

    原文格式PDF

  • 申请/专利权人 C. KIRK NANCE;

    申请/专利号US201514924332

  • 发明设计人 C. KIRK NANCE;

    申请日2015-10-27

  • 分类号G06Q30/00;G01G19/07;

  • 国家 US

  • 入库时间 2022-08-21 13:49:47

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