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Adjusting device for electric control valve of gas turbine combustion chamber nozzle

A gas turbine and valve adjustment technology, which is applied to gas turbine devices, jet propulsion devices, and fuel valves of turbine/propulsion devices, etc., can solve the problem of wear of special-shaped holes, high scrap rate, and the machining accuracy of special-shaped holes and springs cannot meet the requirements of control accuracy, etc. problems, to achieve the effect of reducing the difficulty of processing and reducing the debugging time

Active Publication Date: 2020-03-17
AECC COMML AIRCRAFT ENGINE CO LTD
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  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

[0003] However, the inventor found that the processing accuracy of the special-shaped holes and springs obtained under the existing mechanical processing capabilities cannot meet the control accuracy requirements, and each set of valves must be manually selected and a large number of flow adjustments are performed, which leads to the current production of valves. The scrap rate is high in the process and the processing cycle is long. These problems cause the cost of the valve to be high and cannot be mass-produced and processed.
At the same time, after long-term use, the special-shaped hole is worn out, causing the flow characteristic curve of the valve to deviate from the original design value

Method used

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  • Adjusting device for electric control valve of gas turbine combustion chamber nozzle
  • Adjusting device for electric control valve of gas turbine combustion chamber nozzle
  • Adjusting device for electric control valve of gas turbine combustion chamber nozzle

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Embodiment Construction

[0029] A variety of different implementations or examples for implementing the described subject technical solutions are disclosed below. In order to simplify the disclosure, the following describes the specific examples of each component and arrangement, of course, these are only examples, not limiting the protection scope of the present invention. For example, the description that the first feature described later in the description is formed on or above the second feature may include an embodiment in which the first and second features are formed through direct contact, and may also include an embodiment in which the first and second features are formed between the first and second features. Embodiments of additional features such that there may be no direct relationship between the first and second features. Additionally, reference numerals and / or letters may be repeated in different instances in these disclosures. This repetition is for brevity and clarity and does not i...

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Abstract

The invention provides a fuel flow adjusting device for an electric control valve of a gas turbine combustion chamber nozzle. The fuel flow adjusting device for the electric control valve of the gas turbine combustion chamber nozzle simplifies the processing and debugging process of the valve by adding an electric control technology, and the fuel flow adjusting device for the electric control valve of the gas turbine combustion chamber nozzle comprises a valve shell, a valve mechanical assembly and a valve electric control assembly; the valve electric control assembly comprises an oil inlet joint used for supplying fuel to a first cavity, a flowmeter used for feeding back fuel flow information and outputting a signal, and a microprocessor and a motor used for receiving the output signal ofthe precision flowmeter; the microprocessor controls the motor according to the output signal of the flowmeter, so that the valve mechanical assembly can adjust the fuel flow under the driving of themotor.

Description

technical field [0001] The invention relates to the technical field of gas turbines, in particular to a fuel flow regulating device for an electric control valve of a nozzle of a combustion chamber of a gas turbine. Background technique [0002] The existing gas turbine combustor uses a nozzle with a valve to control the fuel flow into the combustor to increase the flow adjustment range and further increase the working envelope of the combustor. The current valves are all mechanical valves. The hole and the precision spring matched with the valve plug jointly control the effective opening under different pressures, so as to achieve the purpose of flow regulation. [0003] However, the inventors found that the processing accuracy of the special-shaped holes and springs obtained under the existing mechanical processing capabilities cannot meet the control accuracy requirements, and each set of valves must be manually selected and a large number of flow adjustments are performe...

Claims

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Application Information

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IPC IPC(8): F02C9/26F02C9/32F02C7/232
CPCF02C7/232F02C9/263F02C9/32
Inventor 于博文陈景阳罗昌金
Owner AECC COMML AIRCRAFT ENGINE CO LTD
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