CN203023139U - Stationary blade adjusting system for axial flow compressor - Google Patents
Stationary blade adjusting system for axial flow compressor Download PDFInfo
- Publication number
- CN203023139U CN203023139U CN 201220713292 CN201220713292U CN203023139U CN 203023139 U CN203023139 U CN 203023139U CN 201220713292 CN201220713292 CN 201220713292 CN 201220713292 U CN201220713292 U CN 201220713292U CN 203023139 U CN203023139 U CN 203023139U
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- China
- Prior art keywords
- cylinder
- axial flow
- flow compressor
- stator blade
- servo
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- Expired - Lifetime
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Abstract
The utility model provides a stationary blade adjusting system for an axial flow compressor. The stationary blade adjusting system comprises an adjusting cylinder, guide rings, a first servo oil cylinder and a second servo oil cylinder, wherein the guide rings are connected with a stationary blade crank; the guide rings are as much as stationary blades; each guide ring is respectively arranged on the adjusting cylinder and is arranged in one-to-one correspondence with the stationary blades; two servo oil cylinders are arranged on two sides of the axial flow compressor in an axial symmetry way based on the symmetry axis of a center line of the adjusting cylinder; and piston rods of the two servo oil cylinders are respectively connected with two side surfaces of the adjusting cylinder through a first connecting plate and a second connecting plate.
Description
Technical field
The utility model relates to Axial Flow Compressor, particularly a kind of stator blade regulating system of full stator blade adjustable axial-flow formula compressor.
Background technique
Axial Flow Compressor is a kind of turbomachinery equipment that pressurized gas is provided, and it utilizes the interaction of blade and gas, improves pressure and the kinetic energy of gas, and utilizes flow passage component in succession that air-flow is slowed down, and kinetic energy is changed into the raising of pressure.The important motivity equipment of the large-scale air feeds such as oil, chemical industry, metallurgy, environmental protection, pharmacy, ammonia processed, gas compression.The operation stability of axial flow compressor and operating mode using scope will directly determine production capacity and the quality of product of these industries that involve the interests of the state and the people.The complete adjustable axial flow compressor of stator blade is by the adjustment to static blade angle, the adjusting of realization to operating mode, make it have that efficient is high, flow is large, the advantage such as flow, pressure regulation range broadness, even flow field, surge margin are large, thereby whether the structure of stator blade regulating system is rationally most important, but the problem such as existing stator blade regulating system exists that governing speed is slow, poor accuracy, life-span are low.
Summary of the invention
The purpose of this utility model is to overcome the deficiencies in the prior art, and a kind of stator blade regulating system of regulating quick, stable, accurate, safe Axial Flow Compressor is provided.
The stator blade regulating system of Axial Flow Compressor described in the utility model, comprise and regulate cylinder, be used for the guide ring, the first servo-cylinder and the second servo-cylinder that are connected with the stator blade crank, the quantity of described guide ring is identical with the quantity of stator blade, each guide ring is arranged on respectively to be regulated on cylinder, and with stator blade corresponding installation one by one, two servo-cylinders are take the center line of regulating cylinder as symmetry axis, be arranged on axisymmetricly Axial Flow Compressor both sides, the piston rod of two servo-cylinders is connected with the bi-side of adjusting cylinder by the first joining plate, the second joining plate respectively.
the working principle of the stator blade regulating system of Axial Flow Compressor described in the utility model: after the control system of Axial Flow Compressor is sent static blade angle change signal, its hydraulic oil system provides satisfactory pressure oil to the first servo-cylinder and the second servo-cylinder, drive the piston synchronous motion of two servo-cylinders, the piston of two servo-cylinders is respectively by the first joining plate, the second joining plate drives the adjusting cylinder and moves along its axis, can drive each stator blade crank that is connected with each guide ring respectively in the process that the adjusting cylinder moves rotates, thereby each stator blade is rotated, change angle.
The utlity model has following beneficial effect:
1, the stator blade regulating system of Axial Flow Compressor described in the utility model adopts two servo-cylinders that axisymmetric is installed to drive the adjusting cylinders to move, thus can be fast, stable, accurate, the safe adjusting that realizes static blade angle.
2, the stator blade regulating system of Axial Flow Compressor described in the utility model is simple and reasonable for structure, is convenient to maintaining, is conducive to improve working life.
Description of drawings
Fig. 1 is the structural representation of the stator blade regulating system of Axial Flow Compressor described in the utility model;
Fig. 2 is the Placement figure of guide ring and stator blade crank in the stator blade regulating system of Axial Flow Compressor described in the utility model.
In figure, the 1-the first servo-cylinder, the 2-the second servo-cylinder, 3-adjusting cylinder, 4-guide ring, 5-stator blade crank, 6-stator blade, the 7-the first joining plate, the 8-the second joining plate.
Embodiment
Below by embodiment and by reference to the accompanying drawings the structure of the stator blade regulating system of Axial Flow Compressor described in the utility model is described further.
In the present embodiment, the stator blade regulating system of Axial Flow Compressor comprises and regulates cylinder 3, is used for the guide ring 4, the first servo-cylinder 1, the second servo-cylinder 2, the first joining plate 7 and the second joining plate 8 that are connected with the stator blade crank as shown in Figure 1.The quantity of described guide ring 4 is identical with the quantity of stator blade 6, and each guide ring is arranged on respectively to be regulated on cylinder 3, and with stator blade corresponding installation one by one, each stator blade crank 5 is embedded in respectively (see figure 2) in the guide ring of correspondence; Described the first servo-cylinder 1 and the second servo-cylinder 2 be take the center line of regulating cylinder 3 as symmetry axis, is arranged on axisymmetricly Axial Flow Compressor both sides; One end of the first joining plate 7 is connected with the piston rod of the first servo-cylinder 1, and its other end is connected with the right flank of regulating cylinder 3, and an end of the second joining plate 8 is connected with the piston rod of the second servo-cylinder 2, and its other end is connected with the left surface of regulating cylinder 3.
Claims (1)
1. the stator blade regulating system of an Axial Flow Compressor, comprise and regulate cylinder (3), for the guide ring (4) that is connected with the stator blade crank, the quantity of described guide ring is identical with the quantity of stator blade, each guide ring is arranged on respectively to be regulated on cylinder, and with stator blade corresponding installation one by one, characterized by further comprising the first servo-cylinder (1) and the second servo-cylinder (2), two servo-cylinders are take the center line of regulating cylinder (3) as symmetry axis, be arranged on axisymmetricly Axial Flow Compressor both sides, the piston rod of two servo-cylinders is respectively by the first joining plate (7), the second joining plate (8) is connected with the bi-side of regulating cylinder (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220713292 CN203023139U (en) | 2012-12-21 | 2012-12-21 | Stationary blade adjusting system for axial flow compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220713292 CN203023139U (en) | 2012-12-21 | 2012-12-21 | Stationary blade adjusting system for axial flow compressor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203023139U true CN203023139U (en) | 2013-06-26 |
Family
ID=48647128
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220713292 Expired - Lifetime CN203023139U (en) | 2012-12-21 | 2012-12-21 | Stationary blade adjusting system for axial flow compressor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203023139U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104533544A (en) * | 2015-01-26 | 2015-04-22 | 成都成发科能动力工程有限公司 | Stationary blade adjustment device for TRT (blast furnace top gas recovery turbine unit) |
| CN109707671A (en) * | 2019-02-02 | 2019-05-03 | 沈阳透平机械股份有限公司 | A kind of built-in Silence Process mechanism of Axial Flow Compressor |
| CN112360817A (en) * | 2020-12-08 | 2021-02-12 | 成都成发科能动力工程有限公司 | Static blade adjusting mechanism of axial flow compressor and axial flow compressor using same |
-
2012
- 2012-12-21 CN CN 201220713292 patent/CN203023139U/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104533544A (en) * | 2015-01-26 | 2015-04-22 | 成都成发科能动力工程有限公司 | Stationary blade adjustment device for TRT (blast furnace top gas recovery turbine unit) |
| CN104533544B (en) * | 2015-01-26 | 2016-01-06 | 成都成发科能动力工程有限公司 | For the stator blade controlling device of TRT |
| CN109707671A (en) * | 2019-02-02 | 2019-05-03 | 沈阳透平机械股份有限公司 | A kind of built-in Silence Process mechanism of Axial Flow Compressor |
| CN112360817A (en) * | 2020-12-08 | 2021-02-12 | 成都成发科能动力工程有限公司 | Static blade adjusting mechanism of axial flow compressor and axial flow compressor using same |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130626 |