A Lean Multipoint Direct Injection Head for Low Pollution Combustion Chambers of Gas Turbines

A gas turbine and combustion chamber technology, which is applied in the directions of combustion chamber, continuous combustion chamber, combustion method, etc., can solve the problems of low-polluting combustion of gas turbines.

Active Publication Date: 2020-02-14
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

Gaseous fuel can be directly and quickly mixed with air, but liquid fuel must be well atomized and mixed with air to form a combustible mixture, so this burner is not suitable for liquid fuel, and cannot solve the problem of low-pollution combustion using liquid fuel gas turbines

Method used

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  • A Lean Multipoint Direct Injection Head for Low Pollution Combustion Chambers of Gas Turbines
  • A Lean Multipoint Direct Injection Head for Low Pollution Combustion Chambers of Gas Turbines
  • A Lean Multipoint Direct Injection Head for Low Pollution Combustion Chambers of Gas Turbines

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Embodiment Construction

[0027] This embodiment is a lean multi-point direct injection head used in a low-pollution combustion chamber of a gas turbine.

[0028] See Figure 1 ~ Figure 4 This embodiment is used in a lean multi-point direct injection head for a low-pollution combustion chamber of a gas turbine. It is composed of a plurality of swirl nozzle molds of the same structure. The secondary combustion stage swirl nozzle mold 3 consists of the swirl nozzle mold 3a and The swirl nozzle mould 3b, the swirl nozzle mould 3c and the swirl nozzle mould 3d which are evenly spaced in the circumferential direction according to the central swirl nozzle mould are composed of three swirl nozzle moulds 3b, 3c and 3d; The swirl nozzle die 4a, the swirl nozzle die 4c, and the swirl nozzle die 4h are composed of the swirl nozzle die 4a, the swirl nozzle die 4c, and the swirl nozzle die 4h. The main fuel stage swirl nozzle die 4 and the secondary fuel level swirl nozzle die 3 can be independently controlled to ensu...

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Abstract

The invention discloses a lean oil multipoint direct injection head for a low-pollution combustion chamber of a gas turbine. The lean oil multipoint direct injection head is composed of multiple swirl nozzle molds of the same structure. A secondary combustion stage is composed of a swirl nozzle mold located in the center and three swirl nozzle molds circumferentially and evenly distributed along the center swirl nozzle mold at equal distance. A primary combustion stage is composed of swirl nozzle molds alternate with the three swirl nozzle molds of the secondary combustion stage. The primary combustion stage and the secondary combustion stage can be independently controlled, and it is guaranteed that the combustion chamber can stably work in a wide working state. A lean oil direct injection combustion technology is adopted, a nozzle outlet is flushed with a swirl flow air outlet, the nozzle molds work in a non-premixed combustion manner, the phenomena of spontaneous combustion and tempering can be avoided, and the risk of oscillating combustion is reduced. The working equivalence ratio of the nozzle molds ranges from 0.6 to 0.8, it is guaranteed that the temperature of a combustion area is low and combustion is stable, and generated thermal nitric oxide is effectively reduced. Pollutant emissions are few, and the lean oil multipoint direct injection head is simple in structure and suitable for the low-pollution combustion chamber of the gas turbine.

Description

Technical field [0001] The invention relates to the technical field of gas turbine combustion chambers, in particular to a lean oil multi-point direct injection head for low pollution combustion chambers of gas turbines. Background technique [0002] The source of gas turbine pollutant emissions comes from the combustion chamber, so the development of low-pollution combustion technology is the key to reducing gas turbine emissions. The main pollutants in the combustion chamber include nitrogen oxides, carbon monoxide and unburned hydrocarbons, the most important of which is to reduce the production of nitrogen oxides. In the combustion chamber, the thermal nitrogen oxide generation mechanism plays a leading role, so reducing the combustion temperature in the combustion zone is one of the effective means to reduce the nitrogen oxide generation. Lean fuel combustion technology can effectively reduce the combustion temperature in the combustion zone, thereby reducing the amount of ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F23R3/34F23R3/38F23R3/14
CPCF23R3/14F23R3/346F23R3/38
Inventor 于涵索建秦梁红侠孙付军李乐黎明
Owner NORTHWESTERN POLYTECHNICAL UNIV
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