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Large-scale civil aircraft power supply and distribution system ground test integrated verification test platform architecture

A technology for power supply and distribution systems and civil aircraft, which is applied in the field of integrated verification test platform architecture for large-scale civil aircraft power supply and distribution system ground tests. It can solve the problems of many test points and difficult test signal analysis to ensure homology and synchronization sexual effect

Active Publication Date: 2019-04-26
NORTHWESTERN POLYTECHNICAL UNIV
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Problems solved by technology

[0005] In order to overcome the problems of many test points and difficult analysis of test signals in the existing aircraft ground test system, the present invention proposes a large-scale civil aircraft power supply and distribution system ground test integrated verification test platform architecture

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  • Large-scale civil aircraft power supply and distribution system ground test integrated verification test platform architecture

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Embodiment Construction

[0013] This embodiment is an integrated verification test platform architecture for the ground test of the power supply and distribution system of a large civil aircraft.

[0014] refer to figure 1 In this embodiment, the integrated verification test platform architecture of the large-scale civil aircraft power supply and distribution system ground test is used in a certain type of civil aircraft electrical system ground test platform; the aircraft power supply and distribution system ground test integrated verification test platform architecture can be used in civil aircraft electrical systems Power system, including generator, control protector GCU, main bus bar contactor analysis of various power quality parameters, control protection logic and information for comprehensive testing, can analyze voltage modulation and frequency modulation of output voltage and current of three-phase generator , Voltage distortion parameters, and various status information of the GCU can be o...

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Abstract

The invention discloses a large-scale civil aircraft power supply and distribution system ground test integrated verification test platform architecture, which constructs a large-scale distributed measurement and control system based on Ethernet, achieves exchange of network data based on a multi-machine synchronous data acquisition technology and a Client-Server technology, achieves system time nanosecond synchronization under a distributed network structure, and guarantees homology and synchronization between power distribution control logic communication data and measurement data. A digitalsimulator based on a flight profile function of an aircraft is adopted, which solves the problem of decoupling between an aircraft electrical system and avionics and other systems in a ground test and achieves cross-linking measurement and control of the aircraft electrical system, the avionics and the other systems and a man-machine interface verification function of a power supply system and apilot operation program. By the adoption of the integrated verification test platform architecture, reliable experimental basis and means can be provided for design optimization and fault location ofthe electrical system of the large-scale civil aircraft.

Description

technical field [0001] The invention mainly belongs to the technical field of aircraft power supply system experiments, and in particular relates to an integrated verification test platform architecture for ground tests of power supply and distribution systems of large civil aircraft. Background technique [0002] In recent years, with the introduction of multi-electric and all-electric aircraft, distributed power distribution technology has been widely used in independent power systems such as multi-electric and all-electric aircraft in the future. Traditional secondary energy systems such as hydraulic, pneumatic, and environmental control Replaced by electric energy, the role of the power system in the aircraft is becoming more and more important. Therefore, in order to meet the requirements for the design verification and airworthiness test of the aircraft electrical system, it is necessary to design a number of integrated test systems that meet the design specifications a...

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Application Information

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IPC IPC(8): G05B23/02
CPCG05B23/0213
Inventor 雷涛张晓斌董延军郑先成陈光巳
Owner NORTHWESTERN POLYTECHNICAL UNIV
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