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A water-absorbing solid fuel ramjet performance test device

A ramjet, solid fuel technology, applied in gas turbine engine testing, engine testing, jet engine testing, etc., can solve the problems of high cost, difficult to measure performance parameters, complex experimental system, etc., to achieve simple structure and easy daily operation. and maintenance effect

Active Publication Date: 2021-05-04
NANJING UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, it is difficult to complete the underwater experiment of the water-absorbing solid fuel ramjet with the existing technology. Due to the limitation of the underwater conditions and the complex combustion reaction process, the required experimental system is complex and expensive, and the performance parameters are difficult to measure.

Method used

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  • A water-absorbing solid fuel ramjet performance test device

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Embodiment Construction

[0012] The present invention will be further introduced below in conjunction with the accompanying drawings and specific embodiments.

[0013] A water-absorbing solid fuel ramjet performance test device of the present invention comprises a support stand 1, a water-absorbing solid fuel ramjet, a thrust sensor 2, an igniter 3, a solid propellant 4, a temperature sensor 7, a nitrogen cylinder 9, a Pressurized water tank 10; flow regulating valve 11, pressure sensor 12, pneumatic ball valve 14; transmission water pipe 15; atomizing nozzle 16; data transmission line 17; data acquisition computer 18.

[0014] The support stand 1 is used to support the water-absorbing solid fuel ramjet; the combustion chamber 5 of the water-absorbing solid fuel ramjet is provided with a solid propellant 4, and the front end of the combustion chamber 5 is provided with a head baffle; The upper baffle is provided with an igniter 3 for igniting the solid propellant 4; the thrust sensor 2 is fixed on the...

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Abstract

The invention discloses a water-absorbing solid fuel ramjet performance test device, which comprises a support stand, a water-absorbing solid fuel ramjet, a thrust sensor, an igniter, a solid propellant, a temperature sensor, a nitrogen cylinder, a pressurized water tank; and flow adjustment Valves, pressure sensors, pneumatic ball valves; transmission water pipes; atomizing nozzles; data transmission lines; data acquisition computers; support stands for supporting water-absorbing solid fuel ramjet engines; solid propellants are provided in the combustion chambers of water-absorbing solid fuel ramjet engines, The front end of the combustion chamber is provided with a head baffle; the head baffle is provided with an igniter; the thrust sensor is in contact with the thrust sensor; the casing of the mixing chamber of the water-absorbing solid fuel ramjet engine is axially distributed with multiple rows of nozzle holes, each Multiple nozzle holes are arranged in rows, and atomizing nozzles are arranged in the nozzle holes; the atomizing nozzles are connected with pressurized water tanks and nitrogen cylinders through transmission pipes, and the atomizing nozzles are connected with pneumatic ball valves. This device can test the performance of the water-absorbing ramjet engine.

Description

technical field [0001] The invention belongs to the technical field of underwater vehicle power, in particular to a water-absorbing solid fuel ramjet performance test device. Background technique [0002] The water-absorbing ramjet engine uses a specific metal-containing solid propellant, uses water as the working medium, and uses the high-temperature and high-pressure gas produced by the combustion of the solid propellant to chemically react with water or the water is heated and evaporated into water vapor to form a bubble-like gas-liquid two-phase flow , ejected from the nozzle to generate thrust, which can greatly increase its speed and thrust, and has very broad application value. At present, it is difficult to complete the underwater experiment of water-absorbing solid-fuel ramjet in the existing technology. Due to the limitation of underwater conditions and complex combustion reaction process, the required experimental system is complex and expensive, and the performan...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M15/02G01M15/14
CPCG01M15/02G01M15/14
Inventor 李连波黄波周长省陈雄
Owner NANJING UNIV OF SCI & TECH
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