Integrated control system for airtight inspection of aircraft and using method of integrated control system

A technology of air tightness inspection and comprehensive control, which is applied in the direction of liquid tightness measurement using liquid/vacuum degree, fluid tightness test, machine/structural component test, etc. It can solve reading deviation, pipeline parts, connectors, etc. Damage, insufficient measurement accuracy and other problems, to achieve the effect of convenient transportation, protection of pipelines, and accurate testing

Pending Publication Date: 2018-03-13
闫晓红
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] 1. The existing air tightness testing equipment is bulky and heavy, with a weight of 20-40 kg, a length and width of 48-65 cm, and a height of 30-50 cm. In view of the weight and size of the above-mentioned equipment, two people are required to carry it And it is equipped with a special transport rack, which brings great inconvenience to the testers
[0003] 2. Due to the problem of the range of the mechanical meter, the existing measuring equipment needs to be equipped with multiple measuring pipelines. When measuring the cavity parts of the aircraft with different air tightness requirements, the measuring pipelines need to be replaced, which increases the workload of the testers. At the same time Due to the multi-pipeline design of the existing equipment, the number of instruments, pipelines, parts and connectors used is large, and the use of mechanical meters is likely to cause insufficient measurement accuracy, easy to produce reading deviations, and cause inaccurate measurements.
[0004] 3. Due to the multi-pipeline design, the surveyor needs to accurately select the applicable pipeline. Selecting an inappropriate pipeline for measurement will cause measurement data deviation, and in severe cases, it will also cause damage to the corresponding pipeline parts and connectors. The operation is complicated and easy. cause misuse

Method used

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  • Integrated control system for airtight inspection of aircraft and using method of integrated control system

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Embodiment Construction

[0022] An aircraft airtight inspection comprehensive control system, including an air intake and exhaust system and a pipeline docking system, the air intake and exhaust system includes an air source pipeline, an air supply pipeline and a detection pipeline, and the air source pipeline includes an air source Pipe 1 and air source valve 2, the air supply pipeline includes an air supply pipe 3 and an air supply valve 4, and the detection pipeline includes a detection pipe 5, a detection exhaust valve 6 and a detection pressure gauge 7; the air source pipe 1 communicates with the air supply pipe 3; The pipeline docking system includes a gas supply connection port 8, a detection connection port 9 and an air source connection port 10, the gas supply connection port 8 is set on the gas supply pipe 3, the detection connection port 9 is set on the detection tube 5, and the gas source connection port 10 Located in the gas source pipe 1, the gas supply connection port 8 and the detection...

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Abstract

The invention relates to the technical field of detection equipment, in particular to an integrated control system for airtight inspection of an aircraft and a using method of the integrated control system. The integrated control system is mainly applied to airtight performance detections of relating pasts of the aircraft. The integrated control system comprises an intake and exhaust system and apipeline butting system, wherein the intake and exhaust system comprises a gas source pipeline, a gas supply pipeline and a detection pipeline, which facilitates the connection between a gas source and a pressure chamber to be detected, and the gas source pipeline comprises a gas source pipe and a gas source valve; the gas supply pipeline comprises a gas supply pipe and a gas supply valve, and thedetection pipeline comprises a detection pipe, a detection exhaust valve and a detection pressure gauge; the gas source pipe is communicated with the gas supply pipe, and the pipeline butting systemcomprises a gas connecting port, a detection connecting port and a gas source connecting port; the gas supply connecting port is arranged on the gas supply pipe, and the detection connecting port is arranged on the detection pipe; the gas source connecting port is arranged on the gas source pipe, and the gas supply connecting port and the detection connecting port are communicated with the pressure chamber to be detected. The pipeline can be quickly communicated or cut off by the three-valve design, so that the ventilation pressure of each pipeline can be conveniently determined, and the accuracy of testings is ensured.

Description

technical field [0001] The invention relates to the technical field of detection equipment, in particular to an aircraft airtight inspection comprehensive control system and a method for using the same. It is mainly suitable for airtight performance testing of relevant parts of the aircraft. Background technique [0002] 1. The existing air tightness testing equipment is bulky and heavy, with a weight of 20-40 kg, a length and width of 48-65 cm, and a height of 30-50 cm. In view of the weight and size of the above-mentioned equipment, two people are required to carry it And it is equipped with a special delivery rack, which brings great inconvenience to the testers. [0003] 2. Due to the problem of the range of the mechanical meter, the existing measuring equipment needs to be equipped with multiple measuring pipelines. When measuring the cavity parts of the aircraft with different air tightness requirements, the measuring pipelines need to be replaced, which increases the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M3/32
CPCG01M3/3272
Inventor 闫晓红钟伟锋
Owner 闫晓红
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