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Head device of combustion chamber, combustion chamber and gas turbine

A combustion chamber and head technology, which is applied in the field of gas turbines, can solve the problems of incompatibility with the installation of the combustion chamber and the length of the head device.

Active Publication Date: 2018-12-28
新奥能源动力科技(上海)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the prior art, the head device of the combustion chamber adopts a welded structure, and the distance between the mounting flange and the head inlet is fixed. When the axial dimensions of the casing and the flame tube change, the head device often exceeds Long or too short to match the combustion chamber installation

Method used

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  • Head device of combustion chamber, combustion chamber and gas turbine
  • Head device of combustion chamber, combustion chamber and gas turbine
  • Head device of combustion chamber, combustion chamber and gas turbine

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Embodiment Construction

[0046] In order to make the head device match and adjust according to the axial dimensions of the casing and the flame tube, thereby meeting assembly requirements and expanding the scope of application, embodiments of the present invention provide a head device of a combustion chamber, a combustion chamber and a gas turbine. In order to make the purpose, technical solution and advantages of the present invention clearer, the following examples are given to further describe the present invention in detail.

[0047] like Figure 1a , Figure 1b , Figure 2 to Figure 5 As shown, the head device 1 of the combustion chamber provided by the embodiment of the present invention includes a flange 10 coaxially arranged from near to far, a gas collection box 11 and a head air inlet 12, as well as a main stage fuel pipe 13, an auxiliary Support rod 14, duty-level fuel pipe 15 and a plurality of main-stage fuel nozzles 16, wherein: the head air intake 12 includes a mixing cylinder 121 and...

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PUM

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Abstract

The invention discloses a head device of a combustion chamber, the combustion chamber and the gas turbine. The head device can be subjected to matching adjustment according to the axial dimensions ofa casing and a flame cylinder, the assembling needs are met, and the range of application is expanded. According to the head device of the combustion chamber, a first through hole is formed in the center of an end plate of a mixing cylinder of a head inlet piece; a second through hole and a third through hole which are symmetrical in the radial direction are formed in the near side cavity wall ofa gas collecting casing; a threaded hole is formed in the position, corresponding to the first through hole, of a flange, a fourth through hole is formed in the position, corresponding to the second through hole, of the flange, and a fifth through hole is formed in the position, corresponding to the third through hole, of the flange; and outer threads are arranged on a duty level fuel pipe, a mainlevel fuel pipe and an auxiliary support rod, the duty level fuel pipe is fixed to the flange by being connected with a thread of the threaded hole in a locking mode, the main level fuel pipe is fixed to the flange through a pair of first nuts located on two sides of the fourth through hole, and the auxiliary support rod is fixed to the flange through a pair of second nuts located on two sides ofthe fifth through hole.

Description

technical field [0001] The invention relates to the technical field of gas turbines, in particular to a head device of a combustion chamber, a combustion chamber and a gas turbine. Background technique [0002] Gas turbine is a high-power, high-performance power machine that uses air as the medium and relies on high-temperature gas to drive the turbine machine to continuously perform work. It is mainly composed of three major components: compressor, combustion chamber and turbine, together with intake, exhaust, control, transmission and other auxiliary systems. The thermodynamic cycle process of a gas turbine is as follows: [0003] The compressor continuously inhales air from the outside atmosphere and pressurizes it. The temperature rise of the compressed air is conducive to a more violent chemical reaction with the fuel, and a larger expansion ratio is also conducive to the release of a larger gas after the compressed air is burned. energy; [0004] After the compresse...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F23R3/28F23R3/60
CPCF23R3/286F23R3/60
Inventor 汪秋笑李雷秦高雄宋萌刘德玉周涛苏洋
Owner 新奥能源动力科技(上海)有限公司