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Novel air seal for combustion gas turbine tail barrel and manufacturing method for novel air seal

A technology for gas turbines and manufacturing methods, applied in the direction of gas turbine devices, mechanical equipment, jet propulsion devices, etc., can solve the problems of overall scrapping and large losses, and achieve the effects of simple processing, high yield, and easy control

Inactive Publication Date: 2014-12-10
JIANGSU TURBINE SEAL HIGH TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The brush-type air seal used in traditional gas turbines is an integral structure, and errors in the intermediate process will lead to the overall scrapping and large losses
[0005] Brush gas seals for gas turbines are vulnerable parts and need to be replaced regularly

Method used

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  • Novel air seal for combustion gas turbine tail barrel and manufacturing method for novel air seal
  • Novel air seal for combustion gas turbine tail barrel and manufacturing method for novel air seal
  • Novel air seal for combustion gas turbine tail barrel and manufacturing method for novel air seal

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Embodiment Construction

[0027] The present invention will be further described below in conjunction with the accompanying drawings. The following examples are only used to illustrate the technical solution of the present invention more clearly, but not to limit the protection scope of the present invention.

[0028] Such as figure 1 , figure 2 , image 3 As shown, a new type of gas turbine tailpipe air seal, the tailpiece air seal includes a brush 3 and a seal body 1, the brush 3 is composed of a brush tuft 7 and two metal strips 8, the brush tuft 7 is installed on the two metal strips 8 is in the shape of a "T" in the middle; the seal body 1 is provided with a brush mating surface 5, the brush cluster 7 of the brush 3 is fixed on the brush mating surface 5, and the metal strip 8 is close to the side of the brush mating surface 5, through Welded fixing points 2 secure the brush 3 to the seal body 1 .

[0029] The aforementioned metal strips 8 are of any geometric shape.

[0030] Cooling air hol...

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Abstract

The invention discloses a novel air seal for a combustion gas turbine tail barrel and a manufacturing method for the novel air seal. The air seal comprises a brush and a sealing piece body, wherein the brush comprises a brush wire cluster and two metal strips; the brush wire cluster is arranged between the two metal strips, so as to form a T shape; the sealing piece body is provided with a brush wire matching surface; the brush wire cluster of the brush is fixed on the brush wire matching surface; the metal strips are clung to the side surfaces of the brush wire matching surface; the brush and the sealing piece body are fixed by welding fixing points. According to the novel air seal, high-temperature gas at an outlet part of the combustion gas turbine tail barrel can be effectively sealed, the problem of sealing failure caused by severe factors such as high-temperature fuel gas can be well controlled by reasonably selecting a material and a processing process. The novel air seal comprises the brush and the sealing piece body, and can resist the oxidation and corrosion caused by the high-temperature gas of a combustion gas turbine. According to the novel air seal and the manufacturing method of the novel air seal, the processing is easy, the control is easy to implement, the rate of finished products is high, and the aims of saving energy and reducing the consumption can be realized.

Description

technical field [0001] The invention relates to a novel gas turbine tailpipe air seal and a manufacturing method thereof, belonging to the technical field of sealing equipment. Background technique [0002] During the operation of the gas turbine, high-temperature gas passes through the tailpiece and before entering the turbine vane, a special sealing structure is required to prevent the leakage of high-temperature gas. Oxidation corrosion, and can maintain a good seal between components deformed by thermal stress, relying on the excellent performance of high-performance brush filaments, and the rationality of the sealing structure design, can meet the sealing requirements of the unit. [0003] The tailpiece brush air seal is composed of high temperature resistant body material and brush, which forms a contact seal with the sealing working surface. The sealing layer is composed of dense and elastic brush wire. When the high temperature gas passes through the brush wire, it w...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C7/28
Inventor 邹毅申先念顾文武
Owner JIANGSU TURBINE SEAL HIGH TECH
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