Air China Limited

Yuanbin Li

Tang Li

Wenjing Bi

Qixiang Li

Dechao Zhong

Weixi Chai

Xueliang Wu

Chengli Ouyang

Shijun Zhang

The present application relates to a system and a method for handling a fault of an aircraft. The system for handing a fault of an aircraft comprises an interface module for receiving the fault message and a troubleshooting decision-making unit for making a troubleshooting decision against the aircraft faults, wherein the troubleshooting decision is made by the troubleshooting decision-making unit based on fault types/safety risks and cost estimation. The examples in the application allow a cost-effective troubleshooting decision.

System for handling a fault of an aircraft and a method and computer equipment for achieving the same

According to various embodiments, the present invention relates to a platform and method for testing aircraft message trigger logics are disclosed. Apparatus for testing message trigger logics of aircraft comprises: DFDAU (a Digital Flight Data Acquisition Unit), which is adapted to receive message trigger logics to be tested; an input interface, which is adapted to receive data of aircraft condition; and a simulation signal generator, which is adapted to generate simulation signals according to the data of aircraft condition; wherein, the DFDAU is adapted to receive the simulation signals, and generate messages according to the message trigger logics to be tested.

Apparatus and method for testing aircraft message trigger logics

The present invention relates to a test apparatus that includes a simulation signal generation portion and a test portion. Embodiments of the simulation signal generation portion include an input interface, a simulation signal generation module, and an output interface. Embodiments of the test portion include wiring extension apparatus, a Digital Flight Data Acquisition Unit and a comparison module.

Test apparatus and test method based on DFDAU

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Beijing, China

Yuanbin Li