A gas turbine energy recovery system

Abstract

The invention discloses a gas turbine energy recycling system which comprises a combustible source, a combustion system, a regulating valve, an energy accumulator, a one-way valve, a first electromagnetic valve, a second electromagnetic valve, a spray gun and a lifting valve; the lifting valve comprises 1, a first cleaning part, 2, a second cleaning part and 3, a third cleaning part. In the first cleaning part, by adopting a short column and a track groove that are matched, linear motion is tuned into rotation of a cleaning sleeve, then a hair brush on the inner wall of the cleaning sleeve is used for cleaning, and since the cleaning sleeve is located in a lower piston cavity, self-cleaning can be carried out during ventilation. In the second cleaning part, gas injection holes are obliquely formed towards the position of a valve plug, when the valve plug is lifted, all surfaces can be blown and cleaned. In the third cleaning part, a quick maintenance structure is adopted, a closing plate is opened, a stop block is pressed by a tool, then a left valve plug part and a right valve plug part can move along a slide rail, the discharge of sundries in the lower piston cavity is facilitated, and cleaning the valve plug manually by using a special tool can be facilitated.

Description

technical field [0001] The invention relates to the field of fluid control, in particular to a gas turbine energy reuse system. Background technique [0002] A gas turbine is a power machine that converts heat energy into mechanical work using continuously flowing gas as the medium. It roughly includes three parts: the compressor part, the combustion chamber, and the gas turbine (Turbine). The fluid system includes valves. [0003] In the process of use, the gas utilization rate of the gas turbine is prone to be insufficient, the gas residues such as coke residues need to be solved, and fuel pressure fluctuations and gas hammer phenomena often occur. Contents of the invention [0004] In order to overcome the above problems, the present invention proposes a gas turbine energy reuse system to solve the above problems. [0005] The technical solution adopted by the present invention to solve the technical problem is: a gas turbine energy reuse system, including a fuel sourc...

AI Technical Summary

Problems solved by technology

[0003] However, in the process of use, the gas utilization rate of the gas turbine is likely to be insufficient, and the gas residues such as coke residues need to be solved, and fuel pressure fluctuations and air hammer phenomena often occur

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