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Closed electromagnetic thruster capable of storing a certain amount of air

An electromagnetic thrust and closed technology, which is applied in the field of closed electromagnetic thrusters, can solve the problems of high cost and complex structure of the thruster, and achieve the effect of low cost, simple structure and increased selectivity

Inactive Publication Date: 2018-06-15
袁新平
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Aiming at the deficiencies of the prior art, the present invention provides a closed electromagnetic thruster that stores a certain amount of air, which has the advantage of increasing the selectivity of the thruster by inventing a thruster that converts mechanical energy into electromagnetic energy, and solves the problem of existing Some pusher structures are too complex and expensive

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  • Closed electromagnetic thruster capable of storing a certain amount of air
  • Closed electromagnetic thruster capable of storing a certain amount of air

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Embodiment Construction

[0021] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0022] see Figure 1-2 , a closed electromagnetic thruster that stores a certain amount of air, including a body 1, a bearing 2 is fixedly connected to the side of the inner cavity of the body 1, a rotating shaft 3 is movably connected to the inside of the bearing 2, and the end of the rotating shaft 3 away from the bearing 2 is fixed The first gear 7 is connected, the bottom of the first gear 7 is meshed with the second gear 8, the side of the second gear 8 i...

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Abstract

The invention relates to the technical fields of development and utilization of closed thrusting devices and exploration of new thrusters, and discloses a closed electromagnetic thruster capable of storing a certain amount of air. The closed electromagnetic thruster comprises a thruster body, a first gear is movably connected to the side face of an inner cavity of the thruster body through a rotation shaft, a servo motor is fixedly connected to the side face of the first gear, a pulling plate is movably connected to the outer surface of the rotation shaft through a pulling rope, a piston is fixedly connected to the top of the pulling plate through a pulling rod, the outer surface of the piston is movably connected with the inner wall of an air cylinder, the side face of the air cylinder ismovably connected with the top of the pulling plate through a first spring, a turbine generator is fixedly connected to the side face of the air cylinder through a pressurizing air chamber, and an electromagnetic transmitter is fixedly connected to the bottom of the turbine generator through an electric wire. According to the closed electromagnetic thruster capable of storing a certain amount ofthe air, the servo motor drives the first gear to enable the pulling plate to drive the pulling rod and the piston to move, the piston compresses the air in the air cylinder under the reset action ofthe first spring, and the advantage that the turbine generator generates power through the pressurizing air chamber is achieved.

Description

technical field [0001] The invention relates to the development and utilization of a closed thruster, and explores a new thruster technical field, in particular to a closed electromagnetic thruster which stores a certain amount of air. Background technique [0002] The electric thruster, also known as the electric heater, uses electric energy to heat the working medium (hydrogen, amine, hydrazine, etc.) to make it vaporize, and after the expansion and acceleration of the nozzle, it is ejected from the nozzle to generate thrust. [0003] The available options for the existing electric thrusters are too single, mainly including ion thrusters and Hall thrusters. They are essentially the same, and they all use electric energy to ionize the inert gas xenon to form a thruster composed of ions and electrons. The plasma, in which ions are accelerated and ejected under the action of an electric field, generates thrust. The structure is too complicated and the cost is high, which incr...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F03H1/00
CPCF03H1/0081F03H1/0006F03H1/0018
Inventor 袁新平
Owner 袁新平