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Fuel gas turbine

A technology of impeller and gas, applied to gas turbine devices, mechanical equipment, engine components, etc., can solve the problems of insufficient combustion, complex device structure, discontinuous work, etc., and achieve simple structure, high heat utilization rate, and convenient starting Effect

Active Publication Date: 2013-05-08
苏州市东挺河智能科技发展有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Most of the traditional internal combustion engines are piston-type, and the piston is driven to do work by igniting the mixture of compressed air and fuel. Due to the discontinuity of its work (four strokes do work once), there is a problem that vibration will occur. In addition, the self-ignition air-breathing type The engine is destined to burn insufficiently. If the compressed air is used to make it burn fully, it will generate a high temperature, which will put forward higher requirements for the cylinder block, piston and lubrication system, and their requirements for fuel are also relatively simple. Different machines only Ability to use fuel suitable for it
However, the structure of the device provided by this patent is relatively complicated, and high-temperature gas is used as the power source, which has high requirements for bearings and sealing devices

Method used

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Embodiment Construction

[0039] In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific illustrations.

[0040] like Figure 1-10 As shown, a gas turbine includes a main casing 1, the main casing 1 is formed by splicing casing one 11 and casing two 12, the diameter of casing two 12 is smaller than that of casing 11, casing one 11 and casing two There are ring-shaped protrusions correspondingly arranged in the circumferential direction of 12. When the first casing 11 and the second casing 12 are spliced ​​together, there is an annular space at the junction of the two side projections, and the spokes of the impeller (which will be described in detail below) pass through the Space, further, the impeller rim and the outer periphery of the main casing 1 jointly form an annular airtight area, and there are three work areas uniformly arranged on the circu...

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Abstract

The invention discloses a fuel gas turbine. The fuel gas turbine comprises a power system and a pressurizing system, wherein the power system comprises a main machine shell, the main machine shell is coaxially provided with an impeller, the impeller is provided with a power output shaft, and the edge of the impeller is provided with blades, the periphery of the main machine shell is provided with an annular sealing region, the blades are arranged in the annular sealing region, and the annular sealing region is at least provided with a work-doing region for causing fuel gas to push the blades to work; one side of the annular sealing region is a non-work-doing region which is provided with a waste gas outlet, and the outer edge of the work-doing region is provided with a cylinder end for generating the fuel gas; and the pressurizing system is used for providing compressed gas for the cylinder end, and the pressurizing system comprises a turbocharger, a pressurizing machine and a startup pressurizing device. The fuel gas turbine provided by the invention has the advantages that the structure is simple, the maintenance is convenient, the power property is better, and the heat utilization ratio is high.

Description

technical field [0001] The invention relates to a gas turbine. [0002] Background technique [0003] Most of the traditional internal combustion engines are piston-type, and the piston is driven to do work by igniting the mixture of compressed air and fuel. Due to the discontinuity of its work (four strokes do work once), there is a problem that vibration will occur. In addition, the self-ignition air-breathing type The engine is destined to burn insufficiently. If the compressed air is used to make it burn fully, it will generate a high temperature, which will put forward higher requirements for the cylinder block, piston and lubrication system, and their requirements for fuel are also relatively simple. Different machines only Suitable fuel can be used. At present, gas turbines use gas to pass through the turbine, so that the turbine rotates to drive the rotor to rotate and work. Its characteristic is that the fuel volume must be large enough to provide sufficient power...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C6/08F02C7/12F02C7/057
Inventor 邓小波
Owner 苏州市东挺河智能科技发展有限公司
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