Abstract: A display module includes a substrate, a plurality of pixel units are arrayed on the substrate, and each of the pixel units is provided with at least three light-emitting chips, and the centers of at least three light-emitting chips are not collinear; and the projections of at least three light-emitting chips along a first direction at least partially overlap, and the projections of at least three light-emitting chips along a second direction at least partially overlap where the first direction is perpendicular to the second direction.

Abstract: 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.

Abstract: 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.

Abstract: The maintenance method comprises: accessing the maintenance task database to obtain the location and timing of the current aircraft maintenance task; accessing the maintenance person database to obtain a list of available maintenance person and classify the available maintenance person as the first collection of candidates; determining whether each candidate in the first collection of candidates meets the requirements for the location and timing of the current aircraft maintenance task, and then classifying the candidates meeting such requirements in the first collection of candidates as the second collection of candidates; selecting the first maintenance person from the second collection of candidates to perform the current aircraft maintenance task, and determining the estimated start time ti and the estimated end time te of the current aircraft maintenance task based on the information of the first maintenance person.

Abstract: 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.

Abstract: 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.

Abstract: The present invention relates to a platform and method for testing aircraft message trigger logics. Apparatus for testing message trigger logics of aircraft comprises: DFDAU (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.

Abstract: The present invention relates to a test apparatus based on DFDAU (Digital Flight Data Acquisition Unit), comprising: a simulation signal generation portion; and a test portion; wherein, the simulation signal generation portion comprises: an input interface, which receives test data; a simulation signal generation module, which generates simulation signal according to the test data; and an output interface, which is adaptive to be connected to one end of one or more signal transmission device to be tested and output the simulation signal; wherein, the test portion comprises: wiring extension apparatus, which is used to form a gating wiring apparatus and is adaptive to be connected to the other end of the one or more signal transmission devices to be tested, and receive the simulation signal passing through the one or more signal transmission devices to be tested; DFDAU, which is adaptive to receive simulation signal from the wiring extension device, and obtain the transmitted test data; a comparison module, wh