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A power supply conversion logic circuit and its implementation method

A logic circuit and power supply channel technology, which is applied in the power transfer process under the real flight state of the simulated aircraft, and the field of realization of power supply conversion logic, can solve the problems of cumbersome operation process, many manual operations, and poor consistency of the power transfer process, and achieve simplification The effect of operation steps, accurate test results, and shortened power supply time

Active Publication Date: 2019-12-06
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] 1) Many manual operations make the test process and results susceptible to human factors;
[0004] 2) The consistency of the power transfer process during the test is poor, which is not conducive to the comparative analysis of the test process and test data;
[0005] 3) The operation process is cumbersome and time-consuming, and the simultaneous connection of different power supply channels takes a long time, which is easy to form voltage backfeeding phenomenon, poor safety, and affects the accuracy of test results

Method used

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  • A power supply conversion logic circuit and its implementation method
  • A power supply conversion logic circuit and its implementation method

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Embodiment Construction

[0030] The present invention will be described in detail below in conjunction with the accompanying drawings.

[0031] A power supply conversion logic circuit, comprising DC stabilized power supply 1, DC stabilized power supply 2, relay KM1 5, relay KM2 6, power supply channel 1 7, power supply channel 2 8, switch K1 3, switch K2 4, common load terminal 9;

[0032] The positive terminal of the DC stabilized power supply 1 is connected to the switch K1 3 and then divided into two branches, one branch is connected to the positive terminal of the power supply channel 1 7, and the other branch is connected to the coil positive terminal of the relay KM1 5; the DC stabilized power supply 1 The negative terminal of 1 is connected to the common negative terminal 9 of power supply channel 1 7 and power supply channel 2 8;

[0033] The positive terminal of the DC regulated power supply 2 2 is divided into two branches, one of which is connected to the switch K2 4, and then connected to...

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Abstract

The invention belongs to the technical field of testing and measurement, discloses a power supply conversion logic circuit and an implementation method thereof and relates to an implementation method of a power supply conversion logic circuit. In the scientific research stage of an aircraft, repeated ground bulk part testing and overall testing need to be conducted so as to verify the rationality and effectiveness of the design and the coordination between systems; in the testing process, DC voltage-stabilized sources need to be used for simulating an aerial carrier power supply, an aircraft battery power supply and an aircraft generator power supply and then simulating mutual switching between the power supplies. Switches, relays and other components are utilized and reasonably connected with the DC voltage-stabilized sources to achieve fast switching between different power supply channels, the operation steps of testers are simplified, the influence of human factors on test results is reduced, the time of switching between different power supply channels is shortened, and the test results are more accurate.

Description

technical field [0001] The invention relates to a power supply conversion logic circuit and its implementation method, which belong to the technical field of testing and measurement, and relate to a power supply conversion logic implementation method, which is mainly used in the ground test process to simulate the power transfer process of an aircraft in a real flight state. Background technique [0002] In the scientific research stage of the aircraft, in order to verify the rationality, effectiveness and coordination between the systems, etc., it is necessary to conduct multiple ground component and overall tests. Battery power supply and aircraft generator power supply, and further simulate telemetry external power supply to telemetry internal power supply, aircraft power supply to aircraft battery power supply, and aircraft battery power supply to aircraft generator power supply. The traditional test method is to use multiple switches and toggle the switch according to t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F5/60
Inventor 李贺易水华谢强张高强郑宏海徐玮徐剑梅欢张睿纯万蒋亮吴乐熊静赖庆跃熊竹青
Owner JIANGXI HONGDU AVIATION IND GRP