-
公开(公告)号：EP4042250A1
公开(公告)日：2022-08-17
申请号：EP20789033.6
申请日：2020-10-05
-
公开(公告)号：EP3931084A1
公开(公告)日：2022-01-05
申请号：EP20753680.6
申请日：2020-07-16
-
公开(公告)号：EP4230521A1
公开(公告)日：2023-08-23
申请号：EP23157648.9
申请日：2023-02-20
发明人： BIDMEAD, Ashley , HEBBORN, Andrew , GALE, Julian
摘要： A method of parking an aircraft (100) comprises flight crew pedal braking to cause a brake force to be applied to the aircraft wheel brakes (112) to slow the aircraft to a stationary state in which it is ready to be parked. Flight crew then activate a parking brake device (136) and then release the pedal braking (134). An electronic control device (120), forming part of the aircraft's braking system for example, automatically intervenes, following the manual release of the pedal braking, to cause a brake force to continue to be applied to the wheels (106). This may be until sufficient brake force is applied, as a result of the activation of the parking brake device (136), to hold the aircraft (100) in its parked state or may be for a predetermined period of time, say, ten seconds.
-
公开(公告)号：EP4082901A1
公开(公告)日：2022-11-02
申请号：EP22170809.2
申请日：2022-04-29
摘要： Disclosed is an aircraft landing event system comprising a processor, the processor being configured to receive aircraft braking performance information from a plurality of aircraft (40) that have performed a landing event on a particular runway (20). The processor is configured to determine an aircraft braking performance indicator on the basis of the aircraft braking performance information of the plurality of aircraft, and communicate the aircraft braking performance indicator to an aircraft landing system of an approaching aircraft (10) that is about to perform a landing event on the particular runway (20).
-
公开(公告)号：EP4063266A1
公开(公告)日：2022-09-28
申请号：EP22163731.7
申请日：2022-03-23
发明人： HOWELL, George , HEBBORN, Andrew
IPC分类号： B64C25/50
摘要： Disclosed is a monitoring system (300) for an aircraft (100). The monitoring system comprises a controller (301) to determine, based on one or more conditions, one or more expected operating characteristics of a steering system of the aircraft. The one or more conditions comprise one or more aircraft conditions indicative of an internal condition of the aircraft and/or one or more external conditions indicative of an external influence on the aircraft. The controller is to compare the one or more expected operating characteristics with the one or more actual operating characteristics. The controller is configured to determine, based on the compare, whether to issue a signal indicating a condition of the aircraft. Also disclosed is an avionics system (3000) comprising the monitoring system, an aircraft comprising the monitoring system or the avionics system, and a method (600) of monitoring an aircraft.
-
公开(公告)号：EP4043303A1
公开(公告)日：2022-08-17
申请号：EP22156313.3
申请日：2022-02-11
发明人： HAYES, Alexander , BIDMEAD, Ashley , STORME, Thierry , COOMBE, Robert , JOHNSON, Mark , HEBBORN, Andrew
摘要： The present invention provides an aircraft brake control system 60 for controlling antiskid braking of at least first 11 and second 12 wheels in a wheel set of an aircraft 100, the system comprising a control assembly 60 having wheel speed inputs including an input of an indication of the wheel speed 13 of the first wheel 11, and an input of an indication 14 of the wheel speed of the second wheel 12, a wheel speed comparator 62 for determining which of the wheel speeds indicated is a lowest wheel speed 63, and an output 66 for indicating a wheel speed 64 other than the lowest wheel speed 63. The invention also provides an aircraft landing gear 10, an aircraft 100 and methods of braking an aircraft 100.
-
-
-
-
-
搜索结果
6 条记录 (耗时 0.009 秒)
