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Steam booster of rocket propeller

A rocket propulsion and steam technology, applied in jet propulsion devices, machines/engines, etc., can solve the problems of large energy consumption, achieve large propulsion, and reduce the effect of greenhouse effect

Inactive Publication Date: 2008-10-15
赖必达
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, a large amount of energy is bound to be consumed

Method used

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  • Steam booster of rocket propeller

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Embodiment Construction

[0009] Such as figure 1 Shown rocket propeller steam booster of the present invention comprises rocket engine combustor 10, engine jet pipe 12, jet outlet 14, oxygen box liquid 20 and steam booster 21, in the engine combustor 10 of existing rocket and liquid A steam booster 21 is installed between the oxygen tanks 20. The steam booster 21 consists of a high-pressure water cylinder 15, a water cylinder piston 16, a piston spring assembly 17, a high-pressure water nozzle 1, a high-pressure water pipe 5, a valve switch 2, and a valve The control rod 3, the switch control line 11 and the metal ring 4 are composed. The high-pressure water cylinder 15 is fixedly installed in the tail of the rocket, and its capacity is designed and determined according to specific requirements. At least one group of piston spring groups 17 (the number of piston spring groups is set according to specific requirements) is connected to the top in the high-pressure water cylinder 15 . Have an air hole 1...

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Abstract

Steam boost device includes combustion chamber of rocket engine, gas nozzle, outlet of gas jet, and liquid oxygen box. The said combustion chamber is positioned above the gas nozzle; and the liquid oxygen box is positioned above the combustion chamber. There is another steam boost device located above the combustion chamber. The invention adds a steam boost device between combustion chamber and liquid oxygen box. When combustion chamber is ignited, gas nozzle jets out high temperature gas, the steam boost device jets water to gas in high temperature in gas nozzle so as to form great amount of steam, and to make quantity of gas flow at outlet increase rapidly. Thus, burning isodose propellant generates larger propulsion. Advantages are: saving energy, reducing pollution, especially, reducing greenhouse effect.

Description

technical field [0001] The invention belongs to a rocket booster steam booster device. Background technique [0002] Existing vehicles such as rockets, missiles, and space shuttles are all propelled by a large amount of high-temperature gas produced by the combustion of propellant and liquid oxygen from the tail. In order to increase the gas flow rate in the existing technology, the combustion amount of the propellant must be increased. Therefore, a large amount of energy is bound to be consumed. Contents of the invention [0003] The purpose of the present invention is in order to overcome the shortcoming that above-mentioned prior art exists, provide a kind of heat that can make full use of the heat of the high-temperature gas after the engine combustion of vehicle (as rocket, missile, space shuttle etc.) gasify high-pressure water rapidly, and produce a large amount of Water vapor is used to increase the rocket propulsion booster of the tail ejected gas flow. [0004...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02K1/78
Inventor 赖必达
Owner 赖必达