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公开(公告)号：US20170008637A1
公开(公告)日：2017-01-12
申请号：US14793331
申请日：2015-07-07
申请人： The Boeing Company
IPC分类号： B64D39/00
CPC分类号： B64D39/00
摘要： A control system for an aircraft refueling boom controls the movements of the boom in certain areas in a total field of movement volume of possible boom movements based on the location of the boom in the total field of movement volume and based on the current rate of movement of the boom in the total field of movement volume.
摘要翻译： 用于飞机加油吊杆的控制系统基于在整个移动体积的体积中的起重臂的位置并且基于当前的移动速度来控制在可能的起重臂运动的总运动体积中的某些区域中的起重臂的运动 的总体运动量的繁荣。
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公开(公告)号：US09061756B2
公开(公告)日：2015-06-23
申请号：US13868407
申请日：2013-04-23
申请人： The Boeing Company
发明人： Jung Soon Jang , John Lyle Vian
CPC分类号： B64C19/00 , G05B23/0286 , G05D1/0055
摘要： A method and apparatus for monitoring an aircraft. A current performance of the aircraft is identified during operation of the aircraft using a model of the aircraft and flight state data. A current capability of the aircraft is identified from the current performance of the aircraft. An operation is performed based on the current capability of the aircraft.
摘要翻译： 一种用于监视飞行器的方法和装置。 飞机使用飞机和飞行状态数据的模型在运行期间确定飞机的当前性能。 从飞机的当前性能中确定飞机的当前能力。 基于飞行器的当前能力进行操作。
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公开(公告)号：US20240253814A1
公开(公告)日：2024-08-01
申请号：US18162222
申请日：2023-01-31
申请人： The Boeing Company
IPC分类号： B64D45/00
CPC分类号： B64D45/0005 , B64D39/00
摘要： Methods and systems for determining the connection status of a boom of a tanker aircraft with a receiver aircraft. The detection utilizes sensors mounted on the boom. Signals from the sensors are converted from a time domain to a frequency domain. Modes within the frequency domain are identified and analyzed to determine the connection status of the boom with the receiver aircraft.
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公开(公告)号：US20140316613A1
公开(公告)日：2014-10-23
申请号：US13868407
申请日：2013-04-23
申请人： The Boeing Company
发明人： Jung Soon Jang , John Lyle Vian
IPC分类号： B64C19/00
CPC分类号： B64C19/00 , G05B23/0286 , G05D1/0055
摘要： A method and apparatus for monitoring an aircraft. A current performance of the aircraft is identified during operation of the aircraft using a model of the aircraft and flight state data. A current capability of the aircraft is identified from the current performance of the aircraft. An operation is performed based on the current capability of the aircraft.
摘要翻译： 一种用于监视飞行器的方法和装置。 飞机使用飞机和飞行状态数据的模型在运行期间确定飞机的当前性能。 从飞机的当前性能中确定飞机的当前能力。 基于飞行器的当前能力进行操作。
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公开(公告)号：US11427345B2
公开(公告)日：2022-08-30
申请号：US16835962
申请日：2020-03-31
申请人： The Boeing Company
IPC分类号： B64D39/02
摘要： Described are systems and methods for deploying and stowing a refueling boom. In certain examples, deploying the refueling boom includes lowering a refueling boom structure with a hoist while a boom aerodynamic control surface of the refueling is deactivated, determining that first transition conditions have been met, switching the hoist actuator state mode, and activating the boom aerodynamic control surface. In other examples, stowing the refueling boom includes flying the refueling boom towards a fuselage, determining that second transition conditions have been met, switching the hoist actuator state mode, and raising a refueling boom structure of the refueling boom with the hoist.
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公开(公告)号：US10436583B1
公开(公告)日：2019-10-08
申请号：US16189384
申请日：2018-11-13
申请人： THE BOEING COMPANY
发明人： Richard Golob , Justin Cleve Hatcher , Jung Soon Jang , Kimberly Ann Hinson , Jeffrey L. Musgrave
摘要： A system for detecting a sensor fault of an aerial refueling boom. The system comprises a data collector configured to receive sensor data from a plurality of sensors and determine an aerial refueling boom elevation angle of the aerial refueling boom based on the sensor data, wherein the sensor data comprises at least one of cable length data, a dynamic pressure data or aerial refueling boom position data. The system further comprises a processing unit configured access a database table in a storage unit to determine an estimated aerial refueling boom elevation angle, a comparator configured to compare the estimated aerial refueling boom elevation angle to the determined aerial refueling boom elevation angle, and a fault detector configured to generate a sensor fault signal based on the comparison.
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公开(公告)号：US20190092486A1
公开(公告)日：2019-03-28
申请号：US15716151
申请日：2017-09-26
申请人： The Boeing Company
摘要： Systems and methods according to one or more embodiments are provided for rate and position control modes used in the operations of a telescoping refueling boom system. In one example, a system includes a telescoping tube and an actuator coupled to the telescoping tube and configured to extend and/or retract the telescoping tube. A processor is coupled to the actuator and configured to select a telescoping tube rate control mode and/or a telescoping tube position control mode based on a telescoping tube current position error, a telescoping tube current rate of movement, and a value of a telescoping tube rate command.
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公开(公告)号：US20210300583A1
公开(公告)日：2021-09-30
申请号：US16835962
申请日：2020-03-31
申请人： The Boeing Company
IPC分类号： B64D39/02
摘要： Described are systems and methods for deploying and stowing a refueling boom. In certain examples, deploying the refueling boom includes lowering a refueling boom structure with a hoist while a boom aerodynamic control surface of the refueling is deactivated, determining that first transition conditions have been met, switching the hoist actuator state mode, and activating the boom aerodynamic control surface. In other examples, stowing the refueling boom includes flying the refueling boom towards a fuselage, determining that second transition conditions have been met, switching the hoist actuator state mode, and raising a refueling boom structure of the refueling boom with the hoist.
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公开(公告)号：US10343788B2
公开(公告)日：2019-07-09
申请号：US15716151
申请日：2017-09-26
申请人： The Boeing Company
摘要： Systems and methods according to one or more embodiments are provided for rate and position control modes used in the operations of a telescoping refueling boom system. In one example, a system includes a telescoping tube and an actuator coupled to the telescoping tube and configured to extend and/or retract the telescoping tube. A processor is coupled to the actuator and configured to select a telescoping tube rate control mode and/or a telescoping tube position control mode based on a telescoping tube current position error, a telescoping tube current rate of movement, and a value of a telescoping tube rate command.
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公开(公告)号：US10132628B2
公开(公告)日：2018-11-20
申请号：US14640878
申请日：2015-03-06
申请人： THE BOEING COMPANY
发明人： Richard Golob , Justin Cleve Hatcher , Jung Soon Jang , Kimberly Ann Hinson , Jeffrey L. Musgrave
摘要： An aerial refueling boom elevation estimation (“ARBEE”) system for estimating an elevation angle of an aerial refueling boom on an aerial refueling aircraft is described. The ARBEE system may include a data collector, storage unit, optimizer, and comparator.
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