Gas arrow and gas arrow system

An air arrow and arrow body technology, applied in the field of aircraft, can solve the problems of complex structure of the aircraft, increase the fuel consumption, increase the weight of the aircraft, etc., and achieve the effects of high energy utilization rate, low energy consumption, and reduction of high-pressure gas carrying capacity.

Inactive Publication Date: 2012-10-17
丛洋
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Using fuel as the energy source of aircraft has the following disadvantages: First, the fuel is firstly burned to generate heat energy, and then converted from heat energy into mechanical energy to generate power. Due to multiple energy conversions, the energy utilization rate is low
The second is that complex energy conversion devices must be installed in the aircraft, resulting in a complex and cumbersome structure of the aircraft. This complex aircraft structure will greatly increase the weight of the aircraft and further increase the fuel consumption during launch.
Third, fuel combustion will cause serious environmental pollution

Method used

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  • Gas arrow and gas arrow system

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Effect test

Embodiment

[0029] Embodiment, a kind of air arrow system, such as figure 1 Shown, comprise gas arrow, launch frame 15, high-pressure gas supply device 9 and start booster chamber 13. Among them, the air arrow includes an arrow body 1, a cargo compartment 6, a high-pressure gas storage chamber 5, an air injection control system 7, a nozzle 8, a booster cover 14, a guide device 4 and a sealing device 3, and the cargo compartment 6 is arranged on the rocket body 1. The tail of the high-pressure gas storage chamber 5 is arranged in the rocket body 1, and the high-pressure gas output from the high-pressure gas storage chamber 5 is connected to the jet control system 7, and the high-pressure gas output controlled by the jet control system 7 is connected to the nozzle 8, and the nozzle 8 is arranged on The tail of the rocket body 1, the number of nozzles 8 and the size of the nozzles are flexibly set according to needs, the lower end of the rocket body 1 is fixed with a booster cover 14, and ea...

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Abstract

The invention discloses a gas arrow, which comprises an arrow body and an object carrying bin arranged in the arrow body, and is characterized by comprising a high-pressure gas storage chamber, a gas spraying control system and a nozzle, wherein the high-pressure gas storage chamber is formed in the arrow body; the output of the high-pressure gas storage chamber is connected with the gas spraying control system; the output of the gas spraying control system is connected with the nozzle; and the nozzle is arranged at the tail of the arrow body. The invention also discloses a gas arrow system with the gas arrow. The gas arrow is simple in structure and high in energy utilization rate and cannot pollute the environment.

Description

technical field [0001] The invention relates to an aircraft, in particular to an air arrow and an air arrow system. Background technique [0002] Most of the existing aircraft use fuel as an energy source, and fuel combustion generates power to propel the aircraft to fly. In particular, rockets are one of the most important flying vehicles. [0003] With fuel as the energy source of aircraft, there are following deficiencies: the one, fuel first produces heat energy through combustion, converts heat energy into mechanical energy again and just can produce power, owing to pass through multiple energy conversions, energy utilization rate is low. The 2nd, complex energy conversion device must be set in aircraft, causes the structure of aircraft complex, heavy, and this complex aircraft structure can increase the weight of aircraft greatly, further increases the fuel consumption when launching. Third, fuel combustion will cause serious environmental pollution. [0004] Theref...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B15/00
Inventor 丛洋
Owner 丛洋
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