CN203248817U - Servo fuel gas adjusting valve - Google Patents

Servo fuel gas adjusting valve Download PDF

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Publication number
CN203248817U
CN203248817U CN 201320194741 CN201320194741U CN203248817U CN 203248817 U CN203248817 U CN 203248817U CN 201320194741 CN201320194741 CN 201320194741 CN 201320194741 U CN201320194741 U CN 201320194741U CN 203248817 U CN203248817 U CN 203248817U
Authority
CN
China
Prior art keywords
valve
servo
end cover
shell body
end cap
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN 201320194741
Other languages
Chinese (zh)
Inventor
孙晓军
杨柳
左伟
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AVIC Shenyang Engine Design and Research Institute
Original Assignee
AVIC Shenyang Engine Design and Research Institute
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by AVIC Shenyang Engine Design and Research Institute filed Critical AVIC Shenyang Engine Design and Research Institute
Priority to CN 201320194741 priority Critical patent/CN203248817U/en
Application granted granted Critical
Publication of CN203248817U publication Critical patent/CN203248817U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

A servo fuel gas adjusting valve comprises a displacement sensor, a servo oil cylinder, a servo valve, a supporting frame, an upper end cover, a spring, an upper valve element, an upper valve seat, a flange disc, a valve shell body, a lower end cover, a lower valve element and a lower valve seat, wherein the displacement sensor is installed on the servo oil cylinder, the servo valve is installed on the lateral face of the servo oil cylinder, the servo oil cylinder is installed on the supporting frame, the upper end cover is installed on the upper portion outside the valve shell body, the supporting frame is installed at the upper portion of the upper end cover, the upper valve seat is installed at the upper portion inside the valve shell body, the upper valve element is installed on the upper valve seat, the spring is installed between the upper end cover and the upper valve element, the lower valve seat is installed at the lower portion inside the valve shell body, the lower valve element is installed on the lower valve seat, the flange disc is installed on the lateral face of the valve shell body, and the lower end cover is installed at the bottom of the valve shell body. The servo fuel gas adjusting valve has the advantages of being small in friction, quick in response, good in flow characteristic repeatability, high in accuracy, high in starting ignition success rate, and particularly suitable for long-term operation of gas turbines.

Description

A kind of servo gas control valve
Technical field
The utility model relates to gas turbine controlling device field, particularly a kind of servo gas control valve.
Background technique
At present, servo gas control valve is regulated metering for the gas discharge toward the firing chamber, can't accurately satisfy the needs of the various working staties of combustion machine, under the long-time running, and unstable properties.
The model utility content
The purpose of this utility model is in order to satisfy long-time running, improves reliability, and the spy provides a kind of servo gas control valve.
The utility model provides a kind of servo gas control valve, it is characterized in that: described servo gas control valve comprises displacement transducer 1, servo-cylinder 2, servovalve 3, support 4, upper end cap 5, spring 6, upper valve core 7, upper valve base 8, flange plate 9, valve chest 10, lower end cap 11, lower valve core 12, lower valve base 13;
Wherein: displacement transducer 1 is installed on the servo-cylinder 2, and servovalve 3 is installed in the side of servo-cylinder 2, and servo-cylinder 2 is installed on the support 4, and upper end cap 5 is installed in the exterior upper of valve chest 10, and support 4 is installed in upper end cap 5 tops;
Upper valve base 8 is installed in valve chest 10 inner upper, and upper valve core 7 is installed on the upper valve base 8, and spring 6 is installed between upper end cap 5 and the upper valve core 7; Lower valve base 13 is installed in valve chest 10 inner lower, and lower valve core 12 is installed on the lower valve base 13, and flange plate 9 is installed in the side of valve chest 10, and lower end cap 11 is installed in the bottom of valve chest 10.
Described flange plate 9 is two.
Advantage of the present utility model:
Servo gas control valve described in the utility model in the automatic control system of aero-derived gas turbine, is the final controlling element of commonly using.Frictional force is little, response is fast, and Flow characteristics good reproducibility, precision are high, is particularly conducive to the process that starts to work before the adjusted open loop, and the starting ignition success rate is high.Open loop control performance is stable, and degree of regulation is high, and the characteristics such as have that the control quality is good, reliability is high and line using is easy to maintenance are particularly suitable for the long-time running of gas turbine.
Description of drawings
Below in conjunction with drawings and the embodiments the utility model is described in further detail:
Fig. 1 is servo gas control valve theory structure schematic diagram.
Embodiment
Embodiment 1
The present embodiment provides a kind of servo gas control valve, it is characterized in that: described servo gas control valve comprises displacement transducer 1, servo-cylinder 2, servovalve 3, support 4, upper end cap 5, spring 6, upper valve core 7, upper valve base 8, flange plate 9, valve chest 10, lower end cap 11, lower valve core 12, lower valve base 13;
Wherein: displacement transducer 1 is installed on the servo-cylinder 2, and servovalve 3 is installed in the side of servo-cylinder 2, and servo-cylinder 2 is installed on the support 4, and upper end cap 5 is installed in the exterior upper of valve chest 10, and support 4 is installed in upper end cap 5 tops;
Upper valve base 8 is installed in valve chest 10 inner upper, and upper valve core 7 is installed on the upper valve base 8, and spring 6 is installed between upper end cap 5 and the upper valve core 7; Lower valve base 13 is installed in valve chest 10 inner lower, and lower valve core 12 is installed on the lower valve base 13, and flange plate 9 is installed in the side of valve chest 10, and lower end cap 11 is installed in the bottom of valve chest 10.
Described flange plate 9 is two.

Claims (2)

1. servo gas control valve, it is characterized in that: described servo gas control valve comprises displacement transducer (1), servo-cylinder (2), servovalve (3), support (4), upper end cap (5), spring (6), upper valve core (7), upper valve base (8), flange plate (9), valve chest (10), lower end cap (11), lower valve core (12), lower valve base (13);
Wherein: displacement transducer (1) is installed on the servo-cylinder (2), servovalve (3) is installed in the side of servo-cylinder (2), servo-cylinder (2) is installed on the support (4), upper end cap (5) is installed in the exterior upper of valve chest (10), and support (4) is installed in upper end cap (5) top;
Upper valve base (8) is installed in valve chest (10) inner upper, and upper valve core (7) is installed on the upper valve base (8), and spring (6) is installed between upper end cap (5) and the upper valve core (7); Lower valve base (13) is installed in valve chest (10) inner lower, and lower valve core (12) is installed on the lower valve base (13), and flange plate (9) is installed in the side of valve chest (10), and lower end cap (11) is installed in the bottom of valve chest (10).
2. according to servo gas control valve claimed in claim 1, it is characterized in that: described flange plate (9) is two.
CN 201320194741 2013-04-18 2013-04-18 Servo fuel gas adjusting valve Expired - Fee Related CN203248817U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201320194741 CN203248817U (en) 2013-04-18 2013-04-18 Servo fuel gas adjusting valve

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201320194741 CN203248817U (en) 2013-04-18 2013-04-18 Servo fuel gas adjusting valve

Publications (1)

Publication Number Publication Date
CN203248817U true CN203248817U (en) 2013-10-23

Family

ID=49375256

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201320194741 Expired - Fee Related CN203248817U (en) 2013-04-18 2013-04-18 Servo fuel gas adjusting valve

Country Status (1)

Country Link
CN (1) CN203248817U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103527546A (en) * 2013-11-01 2014-01-22 中国航天科技集团公司烽火机械厂 Gas adjuster

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103527546A (en) * 2013-11-01 2014-01-22 中国航天科技集团公司烽火机械厂 Gas adjuster
CN103527546B (en) * 2013-11-01 2016-04-20 中国航天科技集团公司烽火机械厂 A kind of gas regulator

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20131023

Termination date: 20160418

CF01 Termination of patent right due to non-payment of annual fee