CN202768080U - Liquid high pressure air turbine engine - Google Patents

Liquid high pressure air turbine engine Download PDF

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Publication number
CN202768080U
CN202768080U CN 201220257740 CN201220257740U CN202768080U CN 202768080 U CN202768080 U CN 202768080U CN 201220257740 CN201220257740 CN 201220257740 CN 201220257740 U CN201220257740 U CN 201220257740U CN 202768080 U CN202768080 U CN 202768080U
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CN
China
Prior art keywords
pressure air
high pressure
liquid high
turbine engine
liquid
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN 201220257740
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Chinese (zh)
Inventor
王常利
王晨松
吴迪
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
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Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
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Priority to CN 201220257740 priority Critical patent/CN202768080U/en
Application granted granted Critical
Publication of CN202768080U publication Critical patent/CN202768080U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a liquid high pressure air turbine engine, which is a high pressure air turbine engine using evaporated and vaporized high pressure air as power. The liquid high pressure air turbine engine is characterized in that the liquid high pressure air turbine engine comprises a liquid high pressure air storage tank, a liquid high pressure air distribution valve and a high pressure air spray valve, wherein the liquid high pressure air is distributed to the high pressure air spray valve by the liquid high pressure air storage tank through the liquid high pressure air distribution valve and then injected into the a cylinder of the turbine engine; and the air expands to push a turbine, a shaft is driven to rotate through the rotation of the turbine, power is output by the shaft to enable the engine to work. The liquid high pressure air turbine engine has the advantages of energy conservation and environmental friendliness, and the power of the engine is enhanced; only a power producing turbofan at the back end of a combustion chamber is used by the liquid high pressure air turbine engine, an inlet air compression turbofan of the original turbine engine is not even used, the processes of air inlet, compression and high pressure compression are conducted at the front end of the combustion chamber and the combustion chamber is not even used, so that no work is consumed at the front end of the combustion chamber. The turbine engine disclosed by the utility model has a smaller volume, does not spray fire and cannot be detected by infrared rays.

Description

A kind of liquid high-pressure air turbogenerator
Technical field
The utility model relates to motor, more particularly, relates to a kind of motor take liquid high-pressure air as power.
Background technique
At present, existing motor comprises the power category motors such as fuel oil, combustion gas, the mixing of oil electricity, although the technology comparative maturity of this type of motor, but this type of motor all is to produce power by the burning non-renewable energy resources, the energy of burning or the discarded battery of production, all are pollution sources, and the consumption non-renewable resources, infrared visual (burning produces heat energy), hidden performance is not good.
Summary of the invention
In order to solve the fuel non-renewable resources, environmental pollution, the problem of infrared visual, the utility model provides a kind of liquid high-pressure air turbogenerator, and this a kind of liquid high-pressure air turbogenerator is take liquid high-pressure air as power, and is free from environmental pollution.
The technological scheme that its technical problem that solves the utility model adopts is as described below: a kind of liquid high-pressure air turbogenerator, this motor is the high-pressure air turbogenerator take the high-pressure air of carburation by evaporation as power, it is characterized in that, comprise liquid high-pressure air accumulator tank, liquid high-pressure air distributing valve, high-pressure air sprays into valve, described liquid high-pressure air accumulator tank is assigned to high-pressure air with liquid high-pressure air by liquid high-pressure air distributing valve and sprays into valve injection turbogenerator cylinder, gas expansion promotes turbine, turn round by turbine rotating band moving axis, by axle outputting power, engine operation.
According to the utility model of said structure, its beneficial effect is, the utility model energy-conserving and environment-protective strengthen engine power.
The utility model only uses the turbofan of the generation power of rear end, firing chamber, and former turbogenerator air inlet pressurization turbofan does not use, front end airflow, compression, high pressure compressed, and does not use the firing chamber, and will there be the consumption effect in front end.The utility model turbogenerator, volume is less, flame not, infrared detection less than.
Description of drawings
Below in conjunction with accompanying drawing and embodiment the utility model is described further.
Fig. 1 is the utility model structural representation;
Fig. 2 is the utility model turbogenerator cylinder sectional structure chart.
Among the figure, 1, liquid high-pressure air accumulator tank; 2, liquid high-pressure air distributing valve; 3, high-pressure air sprays into valve; 4, turbogenerator cylinder; 5, turbine.
Embodiment
Such as Fig. 1-shown in Figure 2, a kind of liquid high-pressure air turbogenerator, this motor is the high-pressure air turbogenerator take the high-pressure air of carburation by evaporation as power, comprise that liquid high-pressure air accumulator tank 1, liquid high-pressure air distributing valve 2, high-pressure air spray into valve 3, described liquid high-pressure air accumulator tank 1 is assigned to high-pressure air with liquid high-pressure air by liquid high-pressure air distributing valve 2 and sprays into valve 3 injection turbogenerator cylinders 4, gas expansion promotes turbine 5 rotations, by turbine 5 band moving axis runnings, the axle outputting power, engine operation.
Although the utility model is described with reference to the above embodiments; it only is for explanation the utility model that but those of ordinary skill in the art can very clearly be recognized above embodiment fully; wherein can make various changes and revise and do not break away from a broad sense the utility model; so be not that conduct is to restriction of the present utility model; as long as in connotation scope of the present utility model, all will fall within the protection domain that the utility model requires above-described embodiment's variation, distortion.

Claims (1)

1. liquid high-pressure air turbogenerator, this motor is the high-pressure air motor take the high-pressure air of carburation by evaporation as power, it is characterized in that: comprise that liquid high-pressure air accumulator tank, liquid high-pressure air distributing valve, high-pressure air spray into valve, described liquid high-pressure air accumulator tank is assigned to high-pressure air with liquid high-pressure air by liquid high-pressure air distributing valve and sprays into valve injection turbogenerator cylinder, gas expansion promotes turbine, turn round by turbine rotating band moving axis, the axle outputting power, engine operation.
CN 201220257740 2012-06-04 2012-06-04 Liquid high pressure air turbine engine Expired - Fee Related CN202768080U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220257740 CN202768080U (en) 2012-06-04 2012-06-04 Liquid high pressure air turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220257740 CN202768080U (en) 2012-06-04 2012-06-04 Liquid high pressure air turbine engine

Publications (1)

Publication Number Publication Date
CN202768080U true CN202768080U (en) 2013-03-06

Family

ID=47774663

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220257740 Expired - Fee Related CN202768080U (en) 2012-06-04 2012-06-04 Liquid high pressure air turbine engine

Country Status (1)

Country Link
CN (1) CN202768080U (en)

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Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130306

Termination date: 20160604