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Tube fittings with leak protection mechanism

A technology for protecting mechanisms and pipe joints, which is applied in the direction of pipes/pipe joints/fittings, mechanical equipment, sleeves/sockets, etc., and can solve problems affecting the safety of aircraft attendance, centering deviations of pipeline joint connections, engines or Aircraft fire and other problems, to achieve the effect of easy maintenance, good sealing stability, and reduce hazards

Active Publication Date: 2018-06-12
AECC COMML AIRCRAFT ENGINE CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, these connection forms basically use rigid seals or single-layer seals with sealing rings. Once the aircraft or engine is heavily loaded (vibration, medium pressure), leakage may occur, which will cause engine or aircraft fire and affect the aircraft. Attendance or safety of personnel
At the same time, if there are errors in the processing of the pipeline, it will lead to deviations in the alignment of the connection of the pipeline joints, resulting in forced assembly of the pipeline. In the case of vibration and increased medium pressure, it is easy to cause pipeline failure. leakage, endangering the safety of the aircraft

Method used

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  • Tube fittings with leak protection mechanism
  • Tube fittings with leak protection mechanism
  • Tube fittings with leak protection mechanism

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Experimental program
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Embodiment Construction

[0027] First, the terms used in this article are explained as follows.

[0028] The mating position refers to the position where each axially extending component that is sealed and locked by the pipe joint is located after the pipe joint with leakage protection mechanism of the present invention is assembled.

[0029] The non-matching position refers to the position where each component is located before the assembly of the pipe joint with leakage protection mechanism of the present invention is completed, or after the assembly of the pipe joint with leakage protection mechanism of the present invention is completed, the pipe joint is released from the locking and sealing position. where each component is located.

[0030] Inner end means that end where the axially extending parts face each other when they move axially from a non-mating position to a mating position.

[0031] Outer end means that end of the axially extending parts facing away from each other.

[0032]As show...

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PUM

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Abstract

The invention provides a pipe joint with a leakage protecting mechanism. The pipe joint comprises a first joint component, a second joint component and a locking ring, wherein the first joint component is provided with a first outer end and a second inner end, and the second joint component is provided with a second outer end and a second inner end. A first sealing joint is formed between the first joint component and the second joint component at the matched position. The locking ring surrounds the first joint component and the second joint component. One end of the locking ring is connected to the first joint component, and the other end of the locking ring is connected to the second joint component, so that at the matched position, the locking ring, the first joint component and the second joint component form a sealed cavity on the periphery of the first seal joint. The sealed cavity is arranged to enable radial seal or axial seal to be formed between the locking ring and the first joint component and to be formed between the locking ring and the second joint component. The pipe joint with the leakage protecting mechanism can be prevented from leaking media.

Description

technical field [0001] The invention relates to a pipe joint for pipeline connection in the mechanical industry field, and these fields relate to industries such as airplanes, airplane engines, and automobiles. In particular, the invention relates to a pipe connection with leakage protection. Background technique [0002] In order to ensure the safety and reliability of aircraft and engines, reliability indicators need to be considered in many aspects during the design process of aircraft and engines, and the connection form of fuel / lubricating oil pipelines is an important aspect of assessment, which is critical to the safe operation of aircraft and engines. have an important impact. Generally, the connection of aircraft and engine fuel / lubricating oil pipelines adopts flared, non-flared, extruded, ferruled, and flanged connections according to different medium pressures, temperatures, and vibration environments. These structures The form is relatively simple, and it can ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16L21/08
CPCF16L21/08
Inventor 贾文强张正王维
Owner AECC COMML AIRCRAFT ENGINE CO LTD