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Gas turbine device and operating method thereof

A gas turbine and airframe technology, applied in the field of power, can solve problems such as high equipment cost, easily affected fuel, and potential safety hazards, and achieve the effects of simple device structure, reduced safety, and convenient use

Inactive Publication Date: 2019-01-22
朱辉
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0002] Steam turbines generally use the heat generated by the combustion of fuels such as oil, coal, and natural gas to heat water, turning the water into high-temperature, high-pressure steam, and then the steam drives the turbine blades to drive the output shaft for power output. For some When solid fuel is added to the combustion chamber, due to the high temperature in the combustion chamber and the presence of sparks, it is easy to affect the fuel in the combustion chamber, so there is a great potential safety hazard. When the fuel is insufficient, gas supply is required. When it is hot, there is generally another related gas supply system, and the equipment cost is high

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  • Gas turbine device and operating method thereof
  • Gas turbine device and operating method thereof

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Embodiment Construction

[0018] All features disclosed in this specification, or steps in all methods or processes disclosed, may be combined in any manner, except for mutually exclusive features and / or steps.

[0019] Any feature disclosed in this specification, unless specifically stated, can be replaced by other alternative features that are equivalent or have similar purposes. That is, unless expressly stated otherwise, each feature is one example only of a series of equivalent or similar features.

[0020] Such as Figure 1-2As shown, a gas turbine device of the device of the present invention includes a body 10, a combustion chamber 27 extending up and down is provided on the left side of the body 10, a boiler 32 is fixedly installed on the top of the combustion chamber 27, and a boiler 32 is fixed above the combustion chamber 27. A power chamber 35 is provided, and a steam pipe 34 is arranged in the bottom wall of the power chamber 35. The lower end of the steam pipe 34 communicates with the b...

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Abstract

The invention discloses a gas turbine device. The device comprises a body, a combustion chamber extending up and down is formed in the left side of the device body, a boiler is fixedly installed on the top of the combustion chamber, a power cavity is formed in the upper portion of the combustion chamber, a steam pipe is arranged on the bottom wall of the power cavity, the lower end of the steam pipe is communicated with the boiler, the upper end is communicated with the power cavity, a power shaft extending up and down can be rotatably installed on the top wall of the power cavity, the lower end of the power shaft extends to the power cavity, turbine blades are fixedly installed at the lower end of the power shaft, the upper end extend out of the device body, a gas outlet groove communicated with the exterior is formed in the top wall of the power cavity, a fuel cavity with an upward opening is formed in the machine body, a conical cavity is formed in the bottom of the fuel cavity, a transmission groove extending left and right is formed in the lower portion of the conical cavity, and a feeding spiral rod is rotatably installed in left and right end walls of the transmission groove.

Description

technical field [0001] The invention relates to the field of power, in particular to a gas turbine device and an operating method thereof. Background technique [0002] Steam turbines generally use the heat generated by the combustion of fuels such as oil, coal, and natural gas to heat water, turning the water into high-temperature, high-pressure steam, and then the steam drives the turbine blades to drive the output shaft for power output. For some When solid fuel is added to the combustion chamber, due to the high temperature in the combustion chamber and the presence of sparks, it is easy to affect the fuel in the combustion chamber, so there is a great potential safety hazard. When the fuel is insufficient, gas supply is required. When it is hot, there is generally another related gas supply system, and the equipment cost is high. Contents of the invention [0003] Aiming at the deficiencies of the above technologies, the present invention proposes a gas turbine devic...

Claims

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Application Information

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IPC IPC(8): F01K11/02F01K13/00F22B1/22
CPCF01K11/02F01K13/00F22B1/22
Inventor 朱辉
Owner 朱辉