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Gas turbine unit and gas turbine driving equipment

A technology of gas turbines and gas turbines, which is applied in the direction of gas turbine devices, mechanical equipment, combustion air/combustion-air treatment, etc., and can solve problems such as affecting the output power of gas turbines and increasing energy loss

Pending Publication Date: 2022-03-25
YANTAI JEREH PETROLEUM EQUIP & TECH CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] The purpose of the embodiment of the present application is to provide a gas turbine unit, which can solve the problems of increasing energy loss or affecting the output power of the gas turbine in the current anti-icing treatment.

Method used

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  • Gas turbine unit and gas turbine driving equipment
  • Gas turbine unit and gas turbine driving equipment
  • Gas turbine unit and gas turbine driving equipment

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Embodiment Construction

[0036] The following will clearly and completely describe the technical solutions in the embodiments of the present application with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, not all of them. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of this application.

[0037] The terms "first", "second" and the like in the specification and claims of the present application are used to distinguish similar objects, and are not used to describe a specific sequence or sequence. It should be understood that the terms so used are interchangeable under appropriate circumstances such that the embodiments of the application can be practiced in sequences other than those illustrated or described herein, and that references to "first," "second," et...

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Abstract

The invention discloses a gas turbine unit and gas turbine driving equipment, and relates to the field of gas turbines. A gas turbine unit includes a first skid assembly and a second skid assembly; the first skid assembly comprises a ventilation module and an air inlet module; the ventilation module comprises a ventilation pipeline, a ventilation filter, an equipment cabin and a ventilation valve, the ventilation filter, the equipment cabin and the ventilation valve are sequentially arranged on the ventilation pipeline in the airflow direction, the ventilation valve is provided with a first ventilation opening and a second ventilation opening, and the first ventilation opening communicates with the outside atmosphere. The air inlet module comprises an air inlet pipeline and an air inlet filter; the first skid assembly comprises a connecting pipeline, one end of the connecting pipeline is connected with the second ventilation opening, the other end of the connecting pipeline is connected with the air inlet pipeline, and the joint of the connecting pipeline and the air inlet pipeline is located on the upstream of the air inlet filter. The second skid block assembly comprises a gas turbine, and the gas inlet pipeline is connected with the gas turbine. A gas turbine drive apparatus includes a gas turbine set. The problems of energy loss or influence on output power of the gas turbine and the like can be solved.

Description

technical field [0001] The application belongs to the technical field of gas turbines, and in particular relates to a gas turbine unit and a gas turbine driving device. Background technique [0002] Gas turbines have the advantages of large output power, high energy density, low noise, and low emissions, and are widely used in the fields of power generation or driving. When some gas turbines operate in a low-temperature environment, the air intake system is prone to freezing, which affects the air intake of the gas turbine, and then affects the normal operation of the gas turbine. [0003] At present, some gas turbine intake air anti-icing treatment methods include: using compressor to take gas, electric heating, gas turbine waste heat heating, etc. However, the above method will cause additional energy loss or affect the output power of the gas turbine. Contents of the invention [0004] The purpose of the embodiments of the present application is to provide a gas turbi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C6/00F02C7/047F02C7/05F02C7/18
CPCF02C6/00F02C7/047F02C7/05F02C7/18
Inventor 张亭冯宁查万春邹江磊张聪刘志杰吴琼
Owner YANTAI JEREH PETROLEUM EQUIP & TECH CO LTD
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