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Novel turbine engine

A turbine engine, a new type of technology, applied in the direction of engine components, engine cooling, machine/engine, etc., can solve the problems of reducing manufacturing costs and low working efficiency of a single impeller

Pending Publication Date: 2021-06-04
于洁
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The technical problem to be solved by the present invention is to provide a new type of turbine engine with the same effects as multi-stage compressor impellers and multi-stage power impellers on a single compressor unit and a single power unit, aiming at the deficiencies in the prior art. The compressor and work unit of the turbine engine can perform multiple times of compression and work during one revolution, achieving the effect that can only be achieved by a multi-stage impeller mechanism, improving the problem of low working efficiency of a single impeller, and reducing the number of impellers with the same energy conversion efficiency. The number of new turbine engines that can completely replace reciprocating piston engines and can be widely used and popularized in non-aviation fields reduces manufacturing costs

Method used

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Embodiment Construction

[0045] In order to more clearly illustrate the technical characteristics of this solution, the following thirteen embodiments are further elaborated on this solution in conjunction with the accompanying drawings.

[0046] Special note: Among the components and devices marked with numbers above, the components and devices marked with "first" are only used in the description of the following embodiments, such as the first compressor rotor, the first compressor wheel body, and the first compressor wheel Cavity, the first work rotor, the first work wheel body, the first work wheel cavity etc. are all called compressed air rotor, compressed air wheel body, compressed air wheel chamber, work rotor, work wheel body, work wheel cavity, other similarities and differences.

[0047] figure 1 , figure 2 , image 3The first embodiment of the program is shown together. As can be seen from the accompanying drawings, the new turbine engine shown in this embodiment is a basic power engine c...

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Abstract

The invention provides a novel turbine engine. According to the technical scheme, the novel turbine engine is mainly composed of an engine body, an air compression rotor, an acting rotor, a fuel gas generating device and the like, the air compression rotor and the acting rotor are installed on the same axis in the engine body, the air compression rotor is provided with an air inlet and an air outlet, the acting rotor is provided with an air inlet and an air outlet, the fuel gas generating device is composed of a combustion chamber, a fuel injector, a fuel supply device and an igniter, a gas outlet of the air compression rotor communicates with a gas inlet of the combustion chamber, a gas nozzle of the combustion chamber communicates with a gas inlet of an acting impeller, and the air inlet of the air compression rotor and the air outlet of the acting rotor communicate with the atmosphere.

Description

Technical field: [0001] The invention relates to a power machine, especially a turbine engine. Background technique: [0002] Everyone knows that the most widely used reciprocating piston engine has been invented for more than 100 years. It occupies an undeniable and indispensable importance and extensiveness in power applications all over the world. Its various technologies are very mature. In manufacturing technology It can be said that it has reached the peak, but the reciprocating piston engine has a large noise and vibration due to the congenital structural defect of the crank connecting rod, and the contact friction of the piston makes the mechanical loss high, and the diameter of the cylinder is fixed during operation. The stroke of the piston is fixed, so it can only work in the mode of constant volume and constant pressure. In order to overcome these major defects, mechanical design engineers have tried a lot...the most successful typical representative is the turbi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C7/04F02C7/16F02C7/22F02C7/264F01D5/06F04D29/38
CPCF01D5/06F02C7/04F02C7/16F02C7/22F02C7/222F02C7/264F04D29/324
Inventor 于洁
Owner 于洁
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