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Self-sealed valve device for oil draining

A valve device and a valve technology, which are applied in the aviation field, can solve the problems such as leak detection of oil leaking devices, unusable oil drain devices, etc., and achieve the effects of easy installation and maintenance, light weight and simple structure.

Active Publication Date: 2016-03-23
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Before the flight, it is necessary to check the quality of various oils inside the aircraft. Different oils will flow out through the fuel selector. Since the fuel selector / oil filter is generally arranged according to the shape of the aircraft, often the oil inlet of the oil drain device After aligning with the fuel selector, the oil outlet will interfere with the shape of the aircraft, making the oil drain device unusable, and there is an oil leakage problem during the oil drain process.
At present, there is no effective oil discharge device for general-purpose aircraft in China, which can flexibly discharge oil to any part of the fuel system, and can effectively seal after oil discharge to prevent oil leakage

Method used

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  • Self-sealed valve device for oil draining

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Embodiment Construction

[0019] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention. Embodiments of the present invention will be described in detail b...

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Abstract

The invention relates to a self-sealed valve device for oil draining. The device comprises a shell (1), a connector pipe (2), a valve element (3), a top piece (4), a spring (5) and a valve seat (6). An oil inlet (101) and an oil outlet (102) are formed in the shell, and the angles of the oil inlet (101) and the oil outlet (102) are preset, and therefore an oil draining device can more adapt to the shape of the oil draining position; and on the fuel passing path, a spring (5) is arranged between the valve element (3) and the valve seat (6), and an oil path can be sealed by itself, and the problem of oil leakage in the oil draining process can be solved. The oil draining device has the beneficial effects of being simple in structure, light, high in reliability, convenient to mount and maintain and the like.

Description

technical field [0001] The invention belongs to the field of aviation technology, in particular to an oil discharge self-sealing valve device. Background technique [0002] Before the flight, it is necessary to check the quality of various oils inside the aircraft. Different oils will flow out through the fuel selector. Since the fuel selector / oil filter is generally arranged according to the shape of the aircraft, the oil inlet of the oil discharge device is often After aligning with the fuel selector, the oil outlet will interfere with the shape of the aircraft, making the oil drain device unusable, and there is an oil leakage problem during the fuel drain process. At present, there is no effective oil discharge device for domestic general-purpose aircraft that can flexibly discharge oil to any place in the fuel system, and can effectively seal after the oil discharge to prevent it from leaking. Contents of the invention [0003] The purpose of the present invention is ...

Claims

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Application Information

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IPC IPC(8): B64D37/28
CPCB64D37/28Y02T50/40
Inventor 罗海涛熊桂碧苟晓龙
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA