Radiation heat dissipation device for multistage cusped magnetic field plasma thruster

A tangent magnetic field and plasma technology, which is applied in the field of radiation heat dissipation devices for plasma thrusters, can solve the problems of poor working stability and reliability of thrusters, affecting the magnetism of permanent magnets, and short service life, so as to achieve good heat dissipation effect and high heat dissipation Efficiency improvement and material saving effects

Active Publication Date: 2014-05-14
HARBIN INST OF TECH
View PDF4 Cites 13 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention is to solve the problem that the anode temperature of the multi-stage tangential magnetic field plasma thruster is relatively high, and the high temperature at the outlet and the high temperature at the magnetic interface caused by the collision of the ceramic inner wall cause short heating of the inner wall of the thruster channel and the anode. The time increases sharply, and these heat conductions have seriously affected the magnetism of the permanent magnet, as well as the problems of poor working stability and reliability of the thruster and short service life, and then provide a radiation cooling device for a multi-stage tangential magnetic field plasma thruster

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Radiation heat dissipation device for multistage cusped magnetic field plasma thruster
  • Radiation heat dissipation device for multistage cusped magnetic field plasma thruster
  • Radiation heat dissipation device for multistage cusped magnetic field plasma thruster

Examples

Experimental program
Comparison scheme
Effect test

specific Embodiment approach 1

[0008] Specific implementation mode one: combine Figure 1-Figure 5 Explain that the radiation cooling device for the multi-stage tangential magnetic field plasma thruster of this embodiment includes a heat dissipation cylinder 1, a heat dissipation plate 2, two heat dissipation cones 3 and two radiators 4, and the heat dissipation cylinder 1 is closed at one end. As for the heat dissipation cylinder with the other end open, the small diameter ends of the two heat dissipation cones 3 are arranged facing each other, the thruster housing 5 is arranged between the two heat dissipation cones 3, and the two ends of the thruster housing 5 are fixed respectively. In the small-diameter ends of the two radiating cones 3, the upper and lower parts of the thruster housing 5 are each fitted with a radiator 4, and the outer surface of each radiator 4 is composed of a plurality of semicircular arc surfaces 4- 1, the thruster housing 5 is fitted with a cooling plate 2, the cooling plate 2 is...

specific Embodiment approach 2

[0010] Specific implementation mode two: combination Figure 1-Figure 3 To illustrate, the heat dissipation cylinder 1 in this embodiment is made of aluminum. In this way, a heat sink is added to the rear end of the anode, and the heat sink is in close contact with the anode, and the heat sink and the anode can be connected by bolts or welded. The cooling cylinder is made of aluminum with good thermal conductivity and low density, which has a good heat dissipation effect. Others are the same as in the first embodiment.

specific Embodiment approach 3

[0011] Specific implementation mode three: combination figure 1 and figure 2 Note that the heat dissipation cone 3 in this embodiment is made of red copper. In this way, the heat dissipation cone is made of copper, which has good heat conduction effect, and can be connected and fixed with the thruster shell by bolts. Others are the same as in the first or second embodiment.

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention relates to a radiation heat dissipation device, in particular to a radiation heat dissipation device for a multistage cusped magnetic field plasma thruster. The radiation heat dissipation device for the multistage cusped magnetic field plasma thruster aims to solve the problems that due to the high anode temperature of the multistage cusped magnetic field plasma thruster, the high temperature of an outlet and the high temperature of the magnetic separatrix caused by particle collisions on the ceramic inner wall, heating carried out on the channel inner wall and the anode of the thruster is sharply enhanced within a short period, magnetism of a permanent magnet is seriously affected by heat conduction, and the thruster is poor in operation stability and reliability and short in service life. The radiation heat dissipation device for the multistage cusped magnetic field plasma thruster comprises a heat dissipation cylinder, a heat dissipation plate, two heat dissipation conical cylinders and two heat dissipaters, wherein a thruster shell is arranged between the two heat dissipation conical cylinders, the upper portion and the lower portion of the thruster shell are sleeved with the two heat dissipaters respectively, the heat dissipation plate is installed on the thruster shell in a sleeved mode and located between the two hear dissipaters, and the closed end of the heat dissipation cylinder is fixedly connected with the thruster shell. The radiation heat dissipation device is used for the multistage cusped magnetic field plasma thruster.

Description

technical field [0001] The invention relates to a radiation heat dissipation device, in particular to a radiation heat dissipation device for a multi-stage cusp magnetic field plasma thruster. Background technique [0002] The multi-stage cusp magnetic field plasma thruster is a new type of electric propulsion concept emerging in the world. The interior of the thruster is surrounded by multi-stage permanent magnets. The ceramic channel is surrounded by two adjacent permanent magnets with opposite polarities. Under the action of the cathode, the electrons released by the cathode are bound to move in a helical line along the magnetic force line and conduct to the anode through collision to form a discharge circuit. The ions produced by the ionized xenon atoms of the electrons are accelerated and ejected under the action of the axial electric field to generate thrust. . Compared with other electric propulsion devices, the tangential magnetic field plasma thruster has the advan...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): F03H1/00
CPCF03H1/0031
Inventor 刘辉陈蓬勃于达仁马成毓孙国顺赵隐剑
Owner HARBIN INST OF TECH
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap