Gas turbine air inlet system filter installation frame

A technology for air intake system and installation frame, which is applied in the field of filter installation frame, which can solve the problems of affecting the working efficiency of the air intake system, huge installation and removal workload, and short service life, so as to reduce downtime maintenance and replacement time and shorten fault repair The effect of shortening the time and shortening the installation time

Pending Publication Date: 2022-01-25
九江七所精密机电科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the filter is a consumable product, its service life is shorter than that of the intake system, so the filter needs to be replaced frequently during the service life of the gas turbine intake system. The installation and removal work is huge, time-consuming and laborious, which affects the work of the intake system efficiency

Method used

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  • Gas turbine air inlet system filter installation frame
  • Gas turbine air inlet system filter installation frame
  • Gas turbine air inlet system filter installation frame

Examples

Experimental program
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Embodiment Construction

[0020] The specific implementation will be further described below in conjunction with the accompanying drawings.

[0021] Such as Figure 1-Figure 4 As shown, a gas turbine air intake system filter installation frame includes an outer frame 1 with a U-shaped structure in cross section, a rectangular cutout 5 is provided on the outer frame 1, and one side of the rectangular cutout 4 is installed on the outer frame 1. The clamping mechanism 4, the outer frame 1 is also provided with a clamping device 3, a limiting device 2 and a mounting hole 6 respectively.

[0022] The outer frame 1 is composed of an upper U-shaped bending piece 11, a left U-shaped bending piece 12, a right U-shaped bending piece 13, and a lower U-shaped bending piece 14, all of which are U-shaped in cross-section. All towards the inner side of the outer frame 1, the rectangular cutout 5 is provided on the side of the upper U-shaped bending piece 11, and the left U-shaped bending piece 12 and the right U-sha...

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PUM

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Abstract

A gas turbine air inlet system filter installation frame comprises an outer frame with the section of a U-shaped structure, a rectangular notch is formed in the outer frame, a pressing mechanism installed on the outer frame is arranged on one side of the rectangular notch, and a jacking device, a limiting device and an installation hole are further arranged in the outer frame. A plurality of filters can be quickly mounted, and the mounting time is shortened; the outer frame is of a pure welding structure, so that scattered parts are reduced under the function of mounting and fixing a filter, and the influence of falling of parts on subsequent filtering is avoided; installation is easy and convenient, modular design is adopted, if a single filter breaks down, a standby frame can be utilized, the frame can be integrally replaced, and the fault maintenance time of the filter is greatly shortened; and the disassembly and the reassembly are fast and simple, so that the replacement time after the service life of the filter expires is shortened, the shutdown maintenance and replacement time is further shortened, the economic loss caused by shutdown of the filter replacement is reduced, and the economic benefit of a gas turbine gas inlet system is increased in a disguised manner.

Description

technical field [0001] The invention belongs to the field of air purification, and in particular relates to a filter installation frame for gas turbine intake system. Background technique [0002] The gas turbine drives the impeller to rotate to generate electricity by burning fuel and the air compressed by the compressor, and converts the internal energy of the fuel into electrical energy. During the energy conversion process, the gas turbine will inhale a large amount of air. The dust and pollutants in the air make the gas turbine extremely vulnerable to erosion, scaling, melting, corrosion, etc., resulting in thermal imbalance vibration of the rotor, creep deformation of the turbine blades and Fractures, thermal coating wear, vane wear and burnout of combustion chamber components can have serious consequences. Therefore, a large number of filters capable of purifying the air need to be installed in the air intake system of the gas turbine. [0003] At present, the filte...

Claims

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Application Information

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IPC IPC(8): F02C7/05F02C7/052
CPCF02C7/05F02C7/052
Inventor 刘毅张帆刘世祥黄克波王建平杨晓光陈毅王燎峰
Owner 九江七所精密机电科技有限公司
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