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Contrarotating rotary spraying engine

An engine and counter-rotating shaft technology, which is used in machines/engines, mechanical equipment, jet propulsion devices, etc., can solve the problems of bad working environment of flame tube and turbine, low air compression efficiency, and inability to realize regenerative cycle, and achieve continuous fuel combustion. The effect of cleaning and thoroughness, improving the compression efficiency, and reducing the dependence of the atomization effect

Inactive Publication Date: 2009-01-21
蔡盛龙
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to overcome the shortcomings of the existing turboshaft engine, such as the low compression efficiency of the single rotary compressor, the harsh working environment of the flame tube and the turbine, and the inability to realize the heat recovery cycle, the invention provides a counter-rotating rotary jet engine, which can not only greatly Improve the thermal efficiency of the engine and reduce manufacturing costs, as well as reduce harmful gas emissions and reduce life-cycle maintenance costs

Method used

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  • Contrarotating rotary spraying engine

Examples

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Embodiment Construction

[0021] In Fig. 2, the intermediate gear (3), the central gear (4), the internal gear and the shaft (6) constitute the NGW negative sign mechanism; The other end shaft extension is fixedly connected with a nut (9); the counter-rotating axial flow compressor impeller (10) is installed on the central gear shaft (5) and is fixedly connected with a nut (11); the counter-rotating axial flow compressor impeller (8) and The counter-rotating axial flow compressor impeller (10) rotates in the opposite direction to form a counter-rotating axial flow compressor stage; the wind deflector (17), the rotating jet turbine (18), and the rotating jet turbine disc (19) are mounted on the rotating jet turbine shaft ( 16), fixedly connected with nuts (20); the rotating jet turbine disc (19) is fixedly connected with the main shaft (23) with screws to output torque externally; the combustion chamber shell (13) is equipped with a fuel nozzle (14) and a flame tube The hood (15); the flame tube outer t...

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PUM

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Abstract

The invention provides a contra-rotating rotary-jetting engine which can remarkably raise heat efficiency and reduce pollutant emission, manufacturing cost as well as maintenance cost. The engine works by utilizing a principle that a rotary jet turbine of the engine ejects fuel gas at high speed from a tangential spout to allow the self of the rotary jet turbine to rotate reversely so as to convert fuel gas internal energy into mechanical energy; meanwhile, the engine also utilizes a tangential impact turbine to recycle the kinetic energy of the fuel gas ejected from the rotary jet turbine, utilizes a heat regenerator to realize regenerative cycle, adopts a contra-rotating axial flow and contra-rotating centrifugal pressure gas technique to obtain high total pressure ratio, adopts a rotary flame tube technique to obtain high fuel gas temperature in front of the turbine, adopts the novel structural design to greatly reduce the number of components and the consumption of precious materials, and adopts a power confluence mechanism of a cone gear and an overrunning clutch to realize the power confluent output of the mechanical energy of the rotary jet turbine and the tangential impact turbine. Therefore, the engine has high energy conversion efficiency, low manufacturing cost and pollutant emission.

Description

Technical field [0001] The invention relates to a shaft power engine, in particular to a shaft power engine used for vehicles, ships, aviation, generator sets and engineering machinery. Background technique [0002] At present, the performance goals pursued by the known shaft power engines are: as high as possible heat engine efficiency, as low as possible exhaust pollution and manufacturing cost. For a turboshaft engine, the way to achieve high thermal efficiency is to increase the total boost ratio and increase the gas temperature before the turbine; the way to achieve low exhaust pollution is to improve combustion efficiency; the way to achieve low manufacturing cost is to simplify the structure, Reduce material cost and process cost. However, the compressor of a traditional turboshaft engine adopts a single-rotating rotor blade and a stator blade to form a single-stage compression stage. The working environment of the canister and turbine is even harsher, and the high ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C3/08F02C7/32F02C7/10F02C7/36F23R3/56
Inventor 蔡盛龙
Owner 蔡盛龙
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