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A Pressure Control System for Engine Nozzle Test

A nozzle test and pressure control technology, applied in the direction of electric fluid pressure control, etc., can solve problems such as pressure measurement interference, slow adjustment, and difficult convergence of the adjustment system, so as to reduce labor intensity, fast pressure adjustment, and improve adjustment stability. Effect

Active Publication Date: 2017-10-03
AECC AVIATION POWER CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When it is necessary to change the working pressure from low to high, the change of the external pressure given value and the delay of the measured value fed back by the pressure sensor make the comparison between the two in the pressure controller and the calculation of the value out of sync, resulting in pressure overshoot, Overshoot, at the same time, because the spring fluctuation in the nozzle interferes with the pressure measurement of the feedback link, making the adjustment system difficult to converge and the adjustment slow

Method used

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  • A Pressure Control System for Engine Nozzle Test
  • A Pressure Control System for Engine Nozzle Test
  • A Pressure Control System for Engine Nozzle Test

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Embodiment Construction

[0022] The present invention is described in further detail below in conjunction with accompanying drawing:

[0023] Such as figure 2 As shown, the pressure control system of the engine nozzle test of the present invention: a new feedback pressure sensor is added, and the pressure sensor is installed on the side of the nozzle behind the regulating valve and is set away from the nozzle, and the fuel pressure entering the nozzle is controlled by the pressure sensor. Measure, and feed back the measured value to the pressure controller synchronously in real time for comparison and calculation, so as to adjust the regulating valve to achieve closed-loop control, close to the nozzle by setting a low-range pressure sensor and a high-range pressure sensor for segmental measurement of nozzle inlet pressure , as a reference for the given value of the external pressure of the oil supply pipeline.

[0024] Install it on the oil supply pipeline after the regulating valve far away from th...

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Abstract

The invention provides a pressure control system for an engine nozzle test. A pressure sensor is installed on the side, adjacent to a nozzle, of the back of a regulating valve and is arranged far from the nozzle. The pressure sensor is used for measuring the pressure of fuel oil entering the nozzle and synchronously feeding back measured values to a pressure controller in real time for comparison and calculation, and therefore the regulating valve can be regulated and closed-loop control can be achieved. A low-range pressure sensor and a high-range pressure sensor are arranged close to the nozzle respectively to measure the pressure on the inlet of the nozzle in a segmented mode. The pressure sensor is installed on the side, adjacent to the nozzle, of the back of the regulating valve and is arranged far from the nozzle, the measured values can be synchronously fed back to the controller in real time, so pressure regulation is free of overregulation and overshoot, interference of fluctuation of a spring in the nozzle in pressure measurement in a feedback link is avoided, and regulation stability is greatly improved. The two high-accuracy pressure sensors, namely the low-range pressure sensor and the high-range pressure sensor, are used for measuring the pressure on the inlet of the nozzle in a segmented mode, so pressure display is accurate, and work efficiency is improved.

Description

technical field [0001] The invention belongs to the engine nozzle test technology, and relates to a pressure control system for the engine nozzle test. Background technique [0002] In the engine nozzle test, the working pressure is the key control parameter for nozzle detection, which directly affects the detection of parameters such as nozzle flow rate and atomization angle. The test specification requires: at the working pressure of 0.2, 0.557, 1.38, 1.432, 1.48, 1.53, 1.84, 2.35MPa and other pressures, the flow rate, atomization angle and mist cone eccentricity angle are measured. The pressure must be accurately controlled in place from low to high, no overshoot callback is allowed, and the accuracy is ±0.5%. Although the general pressure adjustment method can realize PID automatic adjustment, it cannot realize fast, accurate and stable automatic adjustment without overshoot of multiple pressure control points. Whether the test pressure control is accurate and whether ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D16/20
Inventor 张在望田小京王莉秦锋蒋学军张光明刘京春冯茂龙
Owner AECC AVIATION POWER CO LTD
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