Poppet valve fixing type gas flow adjusting device of solid rocket ramjet

A gas flow regulation, ramjet technology, applied in rocket engine devices, machines/engines, jet propulsion devices, etc., can solve the problems of easy gas leakage, large space occupation, large experimental system volume, etc., to reduce eccentricity , to ensure the neutrality, reduce the effect of ablation

Active Publication Date: 2017-01-11
NANJING UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although the structure is simple and the response speed is fast, it needs to add a gas source device, which occupies a large space. Since the gas is prone to leakage, it is not easy to achieve precise control in the process of adjusting the gas flow.
Wang Yilin of Northwestern Polytechnical University proposed a non-coaxial needle-valve gas flow regulation system with a 90-degree angle between the nozzle and the combustion chamber. Although the throat plug rod is easy to seal and thermal protection is easy to achieve, the experimental system is large and cannot achieve precise control.

Method used

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  • Poppet valve fixing type gas flow adjusting device of solid rocket ramjet
  • Poppet valve fixing type gas flow adjusting device of solid rocket ramjet

Examples

Experimental program
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Embodiment

[0015] combine figure 1 and figure 2 , a cone valve fixed solid rocket ramjet gas flow regulating device, comprising a combustion chamber 1, a vent valve rod 2, a nozzle 3, a fixed base 4, a sealing ring groove 5, a vent hole 6, a cone valve 7, an engine Housing 8, motor 9, gear 10, gear 11; the valve stem 2 with vent hole is fixedly connected with the engine, the vent valve stem 2 is coaxially slidably connected with the nozzle 3, and the nozzle 3 and the fixed base 4 adopt screw transmission, Ventilation hole 6 communicates with nozzle pipe 3, cone valve 7 is threadedly connected with vent valve rod 2, motor 9 is fixedly connected with engine housing 8, motor 9 is fixedly connected with gear 10, gear 10 meshes with gear 11, gear 11 is connected with nozzle Tube 3 is coaxially fixed. The throat of the engine is formed by a fixed cone valve 7 and a movable nozzle 3 that can move axially, and the size of the throat area can be changed by the axial movement of the nozzle 3 . ...

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PUM

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Abstract

The invention discloses a poppet valve fixing type gas flow adjusting device of a solid rocket ramjet. A combustion chamber is connected with a cylindrical hollow valve rod, a poppet valve is connected with the hollow valve rod in a fastened manner through a groove, and two opposite spray pipe holes are formed in the positions, close to the end face, of a cylindrical structure; partial external threads are formed the periphery of a movable spray pipe, the partial external threads are meshed with the internal threads of a fixed base, and three sealing ring grooves are formed in the inner edge of the movable spray pipe; and a stepping motor is fixed below the fixed base through a motor connecting plate, a straight gear is installed on the shaft of the stepping motor through a key, the gear is meshed with a big gear, the big gear and the movable spray pipe are fastened to form a whole, and the spray pipe moves in the direction of the central axis of the fixed base. The poppet valve fixing type gas flow adjusting device of the solid rocket ramjet is simple in structure, accurate to control, reliable in work and low in cost, and is good in realizability.

Description

technical field [0001] The invention belongs to the technical field of gas flow adjustment for solid rocket ramjet engines, in particular to a gas flow adjustment device for solid rocket ramjet engines with fixed cone valves. Background technique [0002] The solid rocket ramjet has the advantages of both ramjet and rocket engines, and has the advantages of high specific impulse, small size, light weight, compact structure, reliable operation, and low cost. In order to ensure that the engine has the best working performance and good thrust adjustment capability, the gas flow of the solid rocket ramjet should be adjusted. At present, there are four main schemes for gas flow regulation: fixed flow type, choke type, non-choke type and swirl valve type. Flow regulating valves usually adopt a variety of configurations, such as plunger spool valve, rotary cam valve, rotary slide disc valve, and cone valve. The transmission mechanisms used in traditional control systems generally...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K9/08F02K9/97
CPCF02K9/08F02K9/97
Inventor 何坤陈雄卜庆伟
Owner NANJING UNIV OF SCI & TECH
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