A static test device and test method for power components of a high-altitude all-electric UAV

Abstract

The invention relates to a static test device and method for a power element of a high-altitude full-electric UAV, and belongs to the technical field of performance test of small UAV. The test deviceis mainly composed of a simulated high-altitude pressure chamber and a power element performance test platform. The simulated high-altitude pressure chamber simulates atmospheric pressures in different flight high-altitude environments and realizes axial positioning of the power element performance test platform, and the power element performance test platform measures parameters including a thrust of a power system, the input electric energy power, a rotating speed of a blade and the motor temperature comprehensively. The method based on the test device can be used to measure the performanceparameters of the power elements of the UAV in the simulated high-altitude flight environment accurately, static test of the power elements is effectively combined with the test environment, the method and device are adapted to performance test of different parameter function parts, and the technical problem in evaluating performances of the power system in different flight environments in the research process of the high-altitude full-electric VAV is solved.

Description

technical field [0001] The invention relates to a static test device and a test method for a power component of a high-altitude all-electric unmanned aerial vehicle, and belongs to the technical field of performance test of small unmanned aerial vehicles. Background technique [0002] High-altitude UAV is an unmanned aerial vehicle whose flight action is controlled by an onboard program. It originated as a special combat aircraft for tactical reconnaissance on the military battlefield. With the continuous deepening of military-civilian integration, high-altitude drones are gradually being used in civil aerial photography, meteorological detection, address survey and other fields. Civilian high-altitude UAVs are different from battlefield combat special aircraft, mainly emphasizing functionality and flight stability. Considering that electric power is easy to obtain, transform and transfer, most civilian high-altitude UAVs use electric power as their energy source. The fligh...

AI Technical Summary

Problems solved by technology

The application of standard power components also has potential technical blind spots. From the perspective of their own technology blockade and intellectual property protection, the manufacturers of functional components only provide relevant operating conditions, operating specifications and safety information in the supporting technical documents of the products. Does not involve detailed performance parameter data

On the other hand, most of the performance information comes only from relatively limited airspace and flight time

[0004] The performance test data for the power components of such aircraft is very scarce. No relevant engineering test methods for high-altitude all-electric UAV power components have been found in the existing technology. The development of high-altitude, high-stability UAV product-related design optimization work provides data support, and the performance and reliability of the corresponding all-electric UAV power components cannot be guaranteed, let alone measurement guarantees throughout the life cycle.

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