Multi-pin micro-Newton colloid thrustor

A thruster and gel technology, applied in jet propulsion devices, machines/engines, rocket engine devices, etc., can solve the problem of few research units, the impact of thruster structural parameters on thruster performance is not considered, and the detailed design of gel thrusters Unpublished reports, etc.

Inactive Publication Date: 2009-09-23
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

This technology allows for easy creation of thruster configurations that have specific features such as emission area size, spacing between an emitting element and its extractor plate, and how many times it needs to change from one mode to another mode based on factors like efficiency or power output. Additionally, this design enables more flexibility when selecting which type of propellant should work best depending upon their desired use scenario.

Problems solved by technology

This patented technical problem addressed by this patents relates to developing an improved type of thrust mechanism that overcomes issues associated with traditional methods like pulses and impellers due to their complex structures and limitations during operation.

Method used

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  • Multi-pin micro-Newton colloid thrustor
  • Multi-pin micro-Newton colloid thrustor

Examples

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Embodiment Construction

[0029] The multi-needle microcolloid thruster of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0030] A kind of multi-needle microcolloid grade colloid thruster of the present invention, as figure 1 , figure 2 As shown, it includes insulating envelope 1, sleeve 2, through-wall joint 12, multi-way 16, capillary line 15, insulating base 3, metal gasket 4, extraction pole 5, accelerating pole 6, insulating gasket 7, insulation Collar 8 , insulating stud 9 , emitter 11 and wire 14 .

[0031] One of the capillary lines 15 is connected to the through-wall joint 12, and is connected to the multi-way 16 inside the sleeve 2 through the insulating envelope 1. The multi-way 16 is connected to a plurality of capillary lines 15 for propellant output. , which can realize single inflow and multiple outflow of propellant. The multiple capillary pipelines 15 for output are respectively connected to the through-wall joints 12 on the in

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Abstract

The invention discloses a multi-pin micro-Newton colloid thrustor which comprises an insulating envelope, a sleeve, through-wall joints, multi-pass, capillary pipelines, an insulating base, a metal gasket, an extracting pole, an accelerator, an insulating spacer, an insulating sleeve ring, an insulating bolt, emitting poles and leads; wherein, the capillary pipelines are connected with the multi-pass in the sleeve, the multi-pass is connected with a plurality of capillary pipelines used for outputting, and the capillary pipelines are respectively connected with the through-wall joints on the insulating base; the other end of each through-wall joint is connected with one emitting pole; the two ends of the leads are fixed on the insulating base and the insulating envelope; the bottom end of the sleeve is connected with the insulating envelope, and the top end thereof is connected with the insulating base by the insulating bolt; the insulating bolt is sequentially provided with nuts, the extracting pole, the insulating sleeve ring, the accelerator and the insulating spacer. The invention can conveniently form different types of thrustors by changing the internal diameter of the emitting pole, adjusting the distance between the emitting poles and the extracting pole, increasing or decreasing the number of the through-wall joints and the emitting poles as well as replacing the multi-pass, thus realizing different regulating ways of the performance of the thrustor.

Description

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Claims

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Application Information

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Owner BEIHANG UNIV
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