Disclosed is a method for operating an aircraft (1) comprising a wing (5) with a foldable wing tip portion (11), the method comprising the following steps: - Providing an aircraft (1), the aircraft (1) comprising a fuselage (3), wings (5) mounted to the fuselage (3), a sensor system (6), and a control unit (7), wherein the sensor system (6) is configured for detecting an operation parameter related to the operation of the foldable wing tip portion (11), wherein the control unit (7) comprises a system behavior model with respect to the operation parameter, wherein the system behavior model provides a target value of the operation parameter, - Detecting a value of the operation parameter by the sensor system (6), - Comparing the detected value of the operation parameter to the corresponding target value of the operation parameter from the system behavior model, - Upon a predefined deviation of the detected value from the corresponding target value of the operation parameter, detecting a sensor failure or a system failure
СПОСОБ РАБОТЫ ЛЕТАТЕЛЬНОГО АППАРАТА, СОДЕРЖАЩЕГО КОНСОЛЬ КРЫЛА СО СКЛАДЫВАЕМОЙ КОНЦЕВОЙ ЧАСТЬЮ КОНСОЛИ КРЫЛА
2020-05-18
Patent
Elektronische Ressource
Russisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2020
Europäisches Patentamt | 2020
КОМПОЗИТНЫЕ НЕРВЮРЫ КРЫЛА ЛЕТАТЕЛЬНОГО АППАРАТА, ИМЕЮЩИЕ ТОКОПРОВОДЯЩИЕ ДОРОЖКИ ЗАЗЕМЛЕНИЯ
Europäisches Patentamt | 2021
Europäisches Patentamt | 2020