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Nozzle, combustion chamber and gas turbine

A nozzle and fuel outlet technology, applied in the field of gas turbines, can solve the problem of high cost

Pending Publication Date: 2020-04-21
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 actual operation of gas turbines, sometimes different injection velocities are required to meet the actual needs. The usual method is to replace a new nozzle. Therefore, the gas turbine needs to be configured with a large number of nozzles (especially for test debugging), and the cost is high.

Method used

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  • Nozzle, combustion chamber and gas turbine
  • Nozzle, combustion chamber and gas turbine
  • Nozzle, combustion chamber and gas turbine

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Embodiment Construction

[0025] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0026] First aspect, such as figure 1 and figure 2 As shown, the embodiment of the present invention provides a nozzle, including:

[0027] The housing 1 is provided with a fuel inlet and a fuel outlet;

[0028] The guide body 2 is at least partly arranged in the fuel outlet, and cooperates with the fuel outlet to form the injection opening 3, and the guide body 2 can move along the axis o of the fuel outlet; along with the guide body 2 As the position alo...

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Abstract

The invention relates to the technical field of display, and discloses a nozzle, a combustion chamber and a gas turbine. The nozzle comprises a shell which is provided with a fuel inlet and a fuel outlet; and a flow guide body, wherein at least part of the flow guide body is arranged in the fuel outlet and the flow guide body is matched with the fuel outlet to form an injection opening, the flow guide body can move in the axis direction of the fuel outlet, and the flow area of the injection opening changes along with the change of the position of the flow guide body in the axis direction. According to the nozzle, the flow guide body and the fuel outlet of the shell are matched to define the injection opening, and the flow guide body can move in the axis direction of the fuel outlet so thatthe flow cross section area of the injection opening changes, that is, the flow area of the outlet of the nozzle can be changed by adjusting the axial position of the flow guide body and then the jetspeed of the nozzle is changed; in conclusion, the outlet jet velocity of the nozzle can be changed and thus the requirements of the gas turbine for different fuel injection speeds can be met.

Description

technical field [0001] The invention relates to the technical field of gas turbines, in particular to a nozzle, a combustion chamber and a gas turbine. Background technique [0002] With the continuous improvement of pollution prevention and control standards, gas turbines are getting more and more attention. The combustion products of gas turbines mainly include NOx (nitrogen oxides), CO (carbon monoxide) and UHC (unburned hydrocarbons), and their emissions are much lower than those of traditional coal. and fuel burn. According to the power range, gas turbines can be divided into: micro gas turbines, small gas turbines, light gas turbines and heavy gas turbines. [0003] Taking micro gas turbine as an example, its core components include combustor, compressor and turbine. The combustion chamber is the power source of the gas turbine, and its performance directly affects the overall performance of the entire gas turbine. The nozzle is a key component of the combustion cha...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F23R3/28
CPCF23R3/283
Inventor 张金琦苏国振屠晓青阮建斌许庆李翔梁勇翔
Owner 新奥能源动力科技(上海)有限公司