Electric fuel switch for starting and stopping gas turbine
By designing an electric fuel switch, using an electric mechanism to control the rotation of the switch valve, slowly open or close the fuel channel, and reduce the fuel supply of the fuel pump before closing, the shock wave problem caused by the inability to slowly close the existing fuel switch is solved, and the safe and stable operation of the gas turbine is achieved.
CN120120124APending Publication Date: 2025-06-10GUIZHOU HONGLIN MACHINERY
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Patent Information
- Application Number
- CN202510485361.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-04-17
- Publication Date
- 2025-06-10
AI Technical Summary
Technical Problem
The existing fuel switches cannot be closed slowly during the start and stop of the gas turbine, which can easily cause the fuel pump to be closed suddenly, cause shock waves, and cause damage to the pipelines and equipment.
Method used
An electric fuel switch is designed to control the rotation of the switch valve through an electric mechanism, slowly open or close the fuel channel, and reduce the fuel supply to the fuel pump before closing to prevent the generation of shock waves.
Benefits of technology
It realizes that the fuel switch is slowly turned off during the start and stop of the gas turbine, avoiding the shock wave caused by the sudden shutdown of the fuel pump, and ensuring the safe and stable operation of the gas turbine.
✦ Generated by Eureka AI based on patent content.
Smart Images

Figure CN120120124A_ABST
Abstract
The invention discloses an electric fuel oil switch for starting and stopping a gas turbine, which comprises a shell, a lining is arranged in the shell, a switch valve is arranged in the lining, and in the rotating process of the switch valve, a control oil inlet, a through hole A, an annular groove and a control oil outlet can form a communicated control oil channel. The fuel inlet, the through hole B, the penetrating hole and the fuel outlet can form a communicated fuel channel, when the opening degree of the fuel channel is maximum, only one of the through holes A is communicated with the annular groove, and an included angle exists between the other through hole of the through hole A and the adjacent end of the annular groove. The fuel switch can slowly turn on the electric fuel switch to supply fuel to a combustion chamber for a system according to a starting control instruction of the gas turbine, slowly turn off the electric fuel switch according to a stopping instruction, stop supplying fuel to the combustion chamber, reduce the fuel supply amount of the fuel pump before the fuel is turned off, prevent impact on a pipeline system when the fuel is turned off, and improve the safety of the system. And safe and stable operation of the gas turbine is ensured.
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