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Testing device for aviation fuel temperature adjustment and cleaning

A test device, aviation fuel technology, applied to the fuel valve of the turbine/propulsion device, fuel heating and charging system of the turbine/propulsion device, etc., to achieve good heating effect, increase safety, and improve heating efficiency

Active Publication Date: 2019-01-15
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

[0007] The purpose of this application is to provide a test device for aviation fuel conditioning and cleaning, to overcome or alleviate at least one of the above-mentioned problems

Method used

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  • Testing device for aviation fuel temperature adjustment and cleaning

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Embodiment Construction

[0071] In order to make the purpose, technical solution and advantages of the application more clear, the technical solution in the embodiment of the application will be described in more detail below in conjunction with the drawings in the embodiment of the application. 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 application. The embodiments described below by referring to the figures are exemplary, and are intended to explain the present application, and should not be construed as limiting the present application. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of this application. Embodiments of the present application will be described in detail below in conjunction with th...

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Abstract

The invention belongs to the technical field of aviation fuel system testing design, and particularly relates to a testing device for aviation fuel temperature adjustment and cleaning. The testing device for aviation fuel temperature adjustment and cleaning comprises a first testing fuel tank, a first cleaning pipeline, a heating pipeline, a heat conducting fuel tank and a heat conducting pipeline, wherein the first testing fuel tank stores aviation fuel; the two ends of the first cleaning pipeline communicate with the first testing fuel tank, and a fuel circulating pump, a fuel cleaning adjusting valve, a first fuel filter and a fourth temperature display are sequentially arranged on the first cleaning pipeline; one end of the heating pipeline communicates with a pipeline on which the first cleaning pipeline located between the fuel circulating pump and the fuel cleaning adjusting valve, and the other end of the heating pipeline communicates with a pipeline on which the first cleaningpipeline located between the first fuel filter and the fourth temperature display; the heating pipeline is provided with a heating adjusting valve and a heating heat exchanger, and the heating adjusting valve is close to the fuel circulating pump; the heat conducting fuel tank stores a liquid state heat conducting medium; one end of the heat conducting pipeline communicates with the heat conducting fuel tank, and the other end of the heat conducting pipeline penetrates through the heating heat exchanger and communicates with the heat conducting fuel tank; and a heat conducting fuel circulating pump and a heat conducting fuel heater are arranged on the heat conducting pipeline.

Description

technical field [0001] The application belongs to the technical field of aviation fuel system test design, in particular to a test device for regulating and cleaning aviation fuel. Background technique [0002] Aviation fuel system tests often have requirements for the temperature and cleanliness of aviation fuel. Currently, the following two methods are often used for aviation fuel temperature regulation: [0003] 1) Heating directly through the fuel pipeline heater, because aviation fuel is flammable and explosive, there is a great potential safety hazard in heating it in this way, and the safety is poor; [0004] 2) Heat the heat transfer oil in the heat transfer oil tank through the heating tube, and then exchange heat with the heated heat transfer oil and aviation fuel. In this way, the heating tube is designed to heat the heat transfer oil, and its heating efficiency is low, and the heating effect poor. [0005] In addition, the current temperature adjustment of avia...

Claims

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Application Information

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IPC IPC(8): F02C7/224F02C7/232F02C7/22
CPCF02C7/22F02C7/224F02C7/232
Inventor 赵炜任恒英张炜
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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