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Micro-flow throttling device

A technology of throttling device and flow rate, which is applied to valve devices, safety valves, engine components, etc., can solve problems such as inability to achieve flow accuracy, and achieve the effects of improving convenience, simple structure and convenient installation.

Active Publication Date: 2022-04-15
SHANGHAI INST OF SPACE PROPULSION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Patent document CN1118180A discloses a throttling device for an internal combustion engine and a method for manufacturing the throttling device. This invention enables throttling by using a metal butterfly throttle valve, but the throttling of the valve cannot achieve the above-mentioned flow accuracy. It is even more impossible to achieve flow regulation in this tiny flow

Method used

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Embodiment Construction

[0030] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0031] The invention provides: according to figure 1 and Figure 7 As shown, a small flow throttling device includes a casing 2, the casing 2 is used for assembly, and the throttling structure 5 is installed inside the casing 2 to form resistance to control the fluid flow. The adjustment structure 1 includes internal threads Sleeve 3, the internally threaded sleeve 3 is installed inside the casing 2, the inner wall of the internally threaded sleeve 3 is provided with an internally threaded body 10, and...

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Abstract

The invention provides a micro-flow throttling device which comprises a sleeve shell, the sleeve shell is used for assembling and installing a throttling structure in the sleeve shell to form resistance to control fluid flow, the throttling structure comprises a first axial hole, the first axial hole is formed in a thin threaded rod, a first radial hole is formed in one side of the first axial hole, and a second radial hole is formed in the other side of the first axial hole. A first radial hole is formed in the sleeve shell, a fine thread flow channel is formed in one side of the first radial hole, a second cavity adjusting structure is arranged between the fine thread flow channel and the coarse thread flow channel and installed on the sleeve shell to adjust the fluid flow, and a butt joint structure is installed on the inner wall of the sleeve shell to conduct disassembly and assembly limiting on the throttling structure. According to the micro-thrust single-component engine, through mutual matching of the four parts, micro runners (lower than 0.3 g / s) can pass through the parts where gaps are formed among the parts, and the throttling problem in the field of micro-thrust single-component engines is solved through resistance of flowing of propellants.

Description

technical field [0001] The invention relates to the throttling field, in particular to a tiny flow throttling device. Background technique [0002] Single-component liquid rocket engines are mostly micro and small liquid rocket engines, which are a branch of liquid rocket engines. They are used to provide momentum and perform attitude control for missiles, launch vehicles, satellites, spacecraft, detectors and other aircraft. The injector is A very important component in a mono-element engine, it affects the working life, starting performance, efficiency and working stability of the thrust chamber. [0003] The pressure drop of the injector is a key parameter of the injector, which affects the performance of the engine from different angles. If the pressure drop of the injector is too small, it will lead to unstable operation of the engine, increase the roughness of the chamber pressure, and generate low-frequency oscillations. Therefore, to ensure For the stability of engi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16K17/20
CPCF16K17/20
Inventor 关亮施伟杨茗黄佳婕杨芳芳王子模张一弛
Owner SHANGHAI INST OF SPACE PROPULSION