Air bleeding valve, air compressor air bleeding control system adopting air bleeding valve and aircraft engine
阅读说明:本技术 放气活门及采用其的压气机放气控制系统、航空发动机 (Air bleeding valve, air compressor air bleeding control system adopting air bleeding valve and aircraft engine ) 是由 盛柏林 李琼 曾维 高吉新 余恺 关醒雯 吴学深 于 2020-06-30 设计创作,主要内容包括:本发明公开了一种放气活门及具有其的压气机放气控制系统、航空发动机。本发明的放气活门采用压气机集气室内的气体作为控制介质,取消了原来的放气结构的8根油压控制管路,有利于实现发动机的小型化设计,整体结构紧凑,其外形不会与飞机其余部件存在干涉,便于安装使用,并且,通过电子控制器控制电磁铁组件通断电即可控制活门打开或者关闭,实现了电子控制功能,使压气机放气更加灵活,可以很好地满足发动机的电子化控制要求。(The invention discloses an air bleeding valve, an air compressor air bleeding control system with the air bleeding valve and an aircraft engine with the air bleeding control system. The air bleeding valve of the invention adopts the gas in the air collecting chamber of the air compressor as a control medium, eliminates 8 oil pressure control pipelines of the original air bleeding structure, is beneficial to realizing the miniaturization design of the engine, has compact integral structure, does not interfere with other parts of the airplane in the shape, is convenient to install and use, can control the valve to open or close by controlling the electromagnet assembly to be powered on or off through an electronic controller, realizes the electronic control function, enables the air bleeding of the air compressor to be more flexible, and can well meet the electronic control requirement of the engine.)
1. An air bleed valve is used for air bleed on the air collecting chamber of any stage of air compressor, and is characterized in that,
comprises an electromagnet assembly (1), an upper shell (2), a base (3), a valve (4), a guide sleeve (6), a steel ball (7), a push rod (8), an iron core spring (9) and a valve spring (10), wherein the base (3) is fixedly arranged on a gas collection chamber of a gas compressor, the upper shell (2) is fixedly arranged on the base (3), the valve (4) is arranged between the base (3) and the upper shell (2) and can slide up and down, a gap between the valve (4) and the upper shell (2) forms a cavity (12), the guide sleeve (6), the steel ball (7), the push rod (8), the iron core spring (9) and the valve spring (10) are all positioned in the upper shell (2), one end of the iron core spring (9) is abutted against the shell of the electromagnet assembly (1), and the other end is abutted against an iron core (101) in the electromagnet assembly (1), one end of the valve spring (10) abuts against the upper shell (2), and the other end of the valve spring abuts against the valve (4);
the electromagnet assembly (1) is fixedly arranged on the upper shell (2), part of the electromagnet assembly (1) extends into the upper shell (2) and presses the guide sleeve (6) to be fixed, a gap exists between the electromagnet assembly (1) and the upper shell (2), one end of the ejector rod (8) is fixedly connected with the iron core (101), the other end of the ejector rod is fixedly connected with the steel ball (7), the upper shell (2) is provided with a first through hole (21) which penetrates in the radial direction, the guide sleeve (6) is provided with a second through hole (61) which penetrates in the axial direction and a third through hole (62) which penetrates in the radial direction, the second through hole and the third through hole are communicated with each other, the third through hole (62) is communicated with the first through hole (21), the ejector rod (8) is positioned in the second through hole (61) and can move up and down in the second through hole (61), the steel ball (7) is positioned in the third through hole (62) and is used for, when electromagnet assembly (1) circular telegram, ejector pin (8) and steel ball (7) are along with iron core (101) rebound together, the upper segment of second through-hole (61) is sealed in steel ball (7), when electromagnet assembly (1) outage, ejector pin (8) and steel ball (7) are along with iron core (101) rebound together, the hypomere of second through-hole (61) is sealed in steel ball (7), and electronic controller controls valve (4) through controlling electromagnet assembly (1) outage and opens or close.
2. Deflation valve according to claim 1,
in an initial state, the iron core spring (9) and the valve spring (10) are both in a compressed state, the valve spring (10) presses the valve (4) downwards to be completely opened, the iron core spring (9) presses the iron core (101) downwards, and the steel ball (7) moves downwards along with the iron core (101) and the ejector rod (8) to seal the lower section of the second through hole (61);
when the engine speed is less than 10%, the valve (4) is kept in a fully opened state under the action of the valve spring (10).
3. Deflation valve according to claim 1,
still include valve switch response subassembly (11), valve switch response subassembly (11) include movable rod (111) and micro-gap switch (112), micro-gap switch (112) fixed mounting on last casing (2) and with electronic controller electric connection, movable rod (111) are connected on valve (4), when valve (4) are opened, movable rod (111) move down and touch micro-gap switch (112) along with valve (4) together, and micro-gap switch (112) switch-on, when valve (4) were closed, thereby movable rod (111) upwards move along with valve (4) and break away from micro-gap switch (112), and micro-gap switch (112) disconnection, electronic controller obtain the position state of valve (4) through the break-make electrical signal that detects micro-gap switch (112) feedback.
4. Deflation valve according to claim 1,
the filter screen (5) is fixed on the guide sleeve (6) and used for preventing impurities from entering the second through hole (61) from the gas collection chamber of the compressor.
5. A bleeder valve as claimed in any of claims 1 to 4,
and the air bleeding valves are respectively arranged on the fifth stage and the eighth stage of the air compressor.
6. An air bleeding control system of a compressor using the air bleeding valve as claimed in claim 5,
the compressor bleed air control system comprises:
a rotational speed sensor for measuring an engine rotational speed;
and the electronic controller is used for controlling the on-off state of the electromagnet assemblies (1) in the fifth-stage air release valve and the eighth-stage air release valve on the air compressor according to the detection result of the rotating speed sensor so as to control the air release valves to be opened or closed.
7. Compressor bleed air control system as in claim 6,
during engine acceleration:
when the rotating speed sensor detects that the rotating speed of the engine rises to 10 percent of the rotating speed, the electronic controller controls the electromagnet assemblies (1) in the fifth-stage air release valve and the eighth-stage air release valve to be electrified, and the fifth-stage air release valve and the eighth-stage air release valve are kept in a fully opened state;
when the rotating speed sensor detects that the rotating speed of the engine is increased to 72.5 percent of the rotating speed, the electronic controller controls the electromagnet assembly (1) of the eighth-stage air release valve to be powered off, and the eighth-stage air release valve is closed;
when the rotating speed sensor detects that the rotating speed of the engine rises to 88 percent of the rotating speed, the electronic controller controls the electromagnet assembly (1) of the fifth-stage air release valve to be powered off, and the fifth-stage air release valve is closed.
8. Compressor bleed air control system as in claim 7,
during engine deceleration:
when the rotating speed sensor detects that the rotating speed of the engine is reduced to 86.1 percent of the rotating speed, the electronic controller controls the electromagnet assembly (1) of the fifth-stage air bleeding valve to be electrified, and the fifth-stage air bleeding valve is completely opened;
when the rotating speed sensor detects that the rotating speed of the engine is reduced to 70.6 percent of the rotating speed, the electronic controller controls the electromagnet assembly (1) of the eighth-stage air release valve to be electrified, and the eighth-stage air release valve is completely opened;
when the rotating speed sensor detects that the rotating speed of the engine is reduced to 8 percent of the rotating speed, the electromagnet assembly (1) of the fifth-stage air release valve and the eighth-stage air release valve is controlled by the electronic controller to be powered off, and the fifth-stage air release valve and the eighth-stage air release valve are still kept in a fully opened state.
9. Compressor bleed air control system as in claim 6,
the electronic controller is also used for acquiring the position state of the air bleeding valve by detecting the on-off electric signal of the microswitch (112).
10. An aircraft engine, characterized in that a compressor bleed air control system according to any one of claims 6 to 9 is employed.
Technical Field
The invention relates to the technical field of air bleeding of a compressor, in particular to an air bleeding valve, an air bleeding control system of the compressor adopting the air bleeding valve, and an aero-engine adopting the air bleeding control system of the compressor.
Background
The aircraft engine mainly comprises components such as a gas compressor, a combustion chamber, a turbine and the like, and when the air flow is reduced to a certain value under a certain rotating speed, the gas compressor can generate a surge phenomenon. Compressor surge is an unstable operating condition of the engine that can cause vibration of the blades and the entire engine and can cause compressor and engine damage. Therefore, surge is not allowed to occur while the engine is operating. Practice proves that for a multi-stage axial flow compressor with the pressure increase ratio of less than 10, air is discharged from the middle stage of the compressor, and the method is a simple and effective method for improving the characteristics of the compressor and expanding the stable working range.
The patent CN106089441A previously filed by the applicant discloses an engine bleed valve control device and an engine control system, which are provided with two bleed valves respectively at the fifth stage and the 8 th stage of the compressor in order to prevent compressor surge, and automatically operated by a fuel regulator. When the engine speed reaches 500-1000 r/min, the four air release valves are opened simultaneously, and the eighth air release valve is opened when the engine speed isIs closed, and the fifth stage air release valve is arranged
And closing the engine to ensure that the engine works stably in the process from starting to working rotating speed. As shown in fig. 1, the specific control principle is as follows: the fuel regulator is provided with a first and aHowever, the fuel regulator used therein is of a mechanical hydraulic type, and the rotation speed at which the purge valve is opened/closed is adjusted by an adjustment screw. When the engine is modified, a digital electronic control system is used, an air bleeding valve of the engine is not improved, oil pressure is still used as a control medium for controlling the air bleeding valve, the opening/closing rotating speed of the air bleeding valve still needs to be adjusted through an adjusting screw, and therefore the air bleeding valve cannot meet the electronic control requirement of the engine. In order to solve the above problems, the present application improves the air bleeding valve.
Disclosure of Invention
The invention provides an air bleeding valve, an air compressor air bleeding system adopting the air bleeding valve and an aero-engine, and aims to solve the technical problems that the existing air bleeding valve adopting oil pressure control cannot meet the electronic control requirement of the engine, an oil pressure control pipeline is too large in arrangement space, and the appearance of the air bleeding valve is interfered with other parts.
According to one aspect of the invention, the deflation valve is used for being installed on a gas collection chamber of any stage of a gas compressor for deflation and comprises an electromagnet assembly, an upper shell, a base, a valve, a guide sleeve, a steel ball, a mandril, an iron core spring and a valve spring, wherein the base is fixedly installed on the gas collection chamber of the gas compressor, the upper shell is fixedly installed on the base, the valve is installed between the base and the upper shell and can slide up and down, a cavity is formed in a gap between the valve and the upper shell, the guide sleeve, the steel ball, the mandril, the iron core spring and the valve spring are all positioned in the upper shell, one end of the iron core spring abuts against the shell of the electromagnet assembly, the other end of the iron core spring abuts against an iron core in the electromagnet assembly, one end of the valve spring abuts against the;
the electromagnet assembly is fixedly arranged on the upper shell, part of the electromagnet assembly extends into the upper shell and presses the guide sleeve to be fixed, a gap exists between the electromagnet assembly and the upper shell, one end of the ejector rod is fixedly connected with the iron core, the other end of the ejector rod is fixedly connected with the steel ball, the upper shell is provided with a first through hole which penetrates in the radial direction, the guide sleeve is provided with a second through hole which penetrates in the axial direction and a third through hole which penetrates in the radial direction, the second through hole and the third through hole are communicated with each other, the third through hole is communicated with the first through hole, the ejector rod is positioned in the second through hole and can move up and down in the second through hole, the steel ball is positioned in the third through hole and is used for sealing the second through hole, when the electromagnet assembly is electrified, the ejector rod and the steel ball move up along with the iron core, the steel ball seals the, the steel ball seals the lower section of the second through hole, and the electronic controller controls the valve to be opened or closed by controlling the electromagnet assembly to be powered on or off.
Further, in an initial state, the iron core spring and the valve spring are both in a compressed state, the valve spring presses the valve downwards to enable the valve to be opened completely, the iron core spring presses the iron core downwards, and the steel ball moves downwards along with the iron core and the ejector rod to seal the lower section of the second through hole;
when the engine speed is less than 10%, the valve is kept in a fully opened state under the action of the valve spring.
Further, still include valve switch response subassembly, valve switch response subassembly includes movable rod and micro-gap switch, micro-gap switch fixed mounting on last casing and with electronic controller electric connection, the movable rod is connected on the valve, when the valve was opened, the movable rod moves down and touches micro-gap switch along with the valve together, and the micro-gap switch-on, when the valve was closed, thereby the movable rod upwards moved along with the valve together breaks away from micro-gap switch, and the micro-gap switch disconnection, the electronic controller acquires the position state of valve through the break-make signal of telecommunication that detects the micro-gap switch feedback.
And the filter screen is fixed on the guide sleeve and used for preventing impurities from entering the second through hole from the gas collection chamber of the compressor.
Further, the bleed valves are respectively mounted on the fifth stage and the eighth stage of the compressor.
In addition, the invention also provides a bleed air control system of the compressor, which adopts the bleed air valve, and the bleed air control system of the compressor comprises:
a rotational speed sensor for measuring an engine rotational speed;
and the electronic controller is used for controlling the on-off state of the electromagnet assemblies in the fifth-stage air release valve and the eighth-stage air release valve on the air compressor according to the detection result of the rotating speed sensor so as to control the air release valves to be opened or closed.
Further, during engine acceleration:
when the rotating speed sensor detects that the rotating speed of the engine rises to 10 percent of the rotating speed, the electronic controller controls electromagnet assemblies in the fifth-stage air release valve and the eighth-stage air release valve to be electrified, and the fifth-stage air release valve and the eighth-stage air release valve are kept in a fully opened state;
when the rotating speed sensor detects that the rotating speed of the engine is increased to 72.5 percent of the rotating speed, the electronic controller controls the electromagnet assembly of the eighth-stage air release valve to be powered off, and the eighth-stage air release valve is closed;
when the rotating speed sensor detects that the rotating speed of the engine rises to 88 percent of the rotating speed, the electronic controller controls the electromagnet assembly of the fifth-stage air release valve to be powered off, and the fifth-stage air release valve is closed.
Further, during engine deceleration:
when the rotating speed sensor detects that the rotating speed of the engine is reduced to 86.1 percent of the rotating speed, the electronic controller controls the electromagnet assembly of the fifth-stage air bleeding valve to be electrified, and the fifth-stage air bleeding valve is completely opened;
when the rotating speed sensor detects that the rotating speed of the engine is reduced to 70.6 percent of the rotating speed, the electronic controller controls the electromagnet assembly of the eighth-stage air release valve to be electrified, and the eighth-stage air release valve is completely opened;
when the rotating speed sensor detects that the rotating speed of the engine is reduced to 8 percent of the rotating speed, the electronic controller controls the electromagnet assemblies of the fifth-stage air release valve and the eighth-stage air release valve to be powered off, and the fifth-stage air release valve and the eighth-stage air release valve are still kept in a fully opened state.
Further, the electronic controller is also used for acquiring the position state of the air bleeding valve by detecting the on-off electric signal of the micro switch.
In addition, the invention also provides an aircraft engine which adopts the air compressor bleed air control system.
The invention has the following effects:
the air bleeding valve of the invention adopts the gas in the air collecting chamber of the air compressor as a control medium, eliminates 8 oil pressure control pipelines of the original air bleeding structure, is beneficial to realizing the miniaturization design of the engine, has compact integral structure, does not interfere with other parts of the airplane in the shape, is convenient to install and use, can control the valve to open or close by controlling the electromagnet assembly to be powered on or off through the electronic controller, realizes the electronic control function, enables the air bleeding of the air compressor to be more flexible, and can well meet the electronic control requirement of the engine.
In addition, the compressor bleed air control system and the aircraft engine have the advantages.
In addition to the objects, features and advantages described above, other objects, features and advantages of the present invention are also provided. The present invention will be described in further detail below with reference to the drawings.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this application, illustrate embodiments of the invention and, together with the description, serve to explain the invention and not to limit the invention. In the drawings:
fig. 1 is a schematic structural view of a conventional engine bleed valve control apparatus.
Fig. 2 is a structural schematic view of a prior art deflation valve.
Fig. 3 is a sectional structural view of the deflation valve in accordance with the first embodiment of the present invention.
Fig. 4 is a schematic view of the gas flow when the deflation valve of the first embodiment of the present invention is in the open state.
Fig. 5 is a schematic view of the gas flow when the deflation valve of the first embodiment of the present invention is in the closed state.
Fig. 6 is a schematic view of a module connection structure of a compressor bleed air control system according to a second embodiment of the present invention.
Description of the reference numerals
1. An electromagnet assembly; 2. an upper housing; 3. a base; 4. a shutter; 5. filtering with a screen; 6. a guide sleeve; 7. a steel ball; 8. a top rod; 9. an iron core spring; 10. a shutter spring; 11. a valve switch sensing assembly; 12. a cavity; 101. an iron core; 21. a first through hole; 61. a second through hole; 62. a third through hole; 111. a movable rod; 112. a micro switch.
Detailed Description
The embodiments of the invention will be described in detail below with reference to the accompanying drawings, but the invention can be embodied in many different forms, which are defined and covered by the following description.
As shown in fig. 3 to 5, a first embodiment of the present invention provides an air bleeding valve for installing on an air collecting chamber of any stage of an air compressor to bleed air, the air bleeding valve includes an
One end of the ejector rod 8 is fixedly connected with the
It can be understood that, the bleed valve of this embodiment adopts the gas in the compressor gas collecting chamber as the control medium, has cancelled 8 oil pressure control pipelines of original bleed structure, is favorable to realizing the miniaturized design of engine, and overall structure is compact, and its appearance can not have the interference with other parts of aircraft, and the installation is convenient for use, and, can control
It can be understood that in the initial state, the engine is not running, the gas pressure of the fifth stage and the eighth stage of the compressor is as large as the atmospheric pressure, the core spring 9 and the
Preferably, the air release valve further comprises a valve switch sensing assembly 11, the valve switch sensing assembly 11 comprises a
It will be appreciated that the bleed valve preferably further comprises a filter screen 5 fixed to the guide sleeve 6 and adapted to prevent impurities from entering the second through
In addition, as shown in fig. 6, a second embodiment of the present invention further provides a compressor bleed air control system, which employs the bleed air valve according to the first embodiment, and includes:
a rotational speed sensor for measuring an engine rotational speed;
and the electronic controller is used for controlling the on-off state of the
Because the rotating speed of the engine is related to the air pressure in the fifth stage and the eighth stage of the air compressor, the air pressure in the fifth stage and the eighth stage of the air compressor can be indirectly reflected by detecting the rotating speed of the engine, so that the on-off state of the
When the engine is in a stop and static state, the air pressure of the fifth stage and the eighth stage of the air compressor is as high as the atmospheric pressure, and the fifth stage air release valve and the eighth stage air release valve are both in a fully open state.
During engine acceleration:
when the rotating speed sensor detects that the rotating speed of the engine rises to 10% of the rotating speed (1280r/min), the air pressure in the fifth stage and the eighth stage of the air compressor exceeds 20kPa, the air pressure at the bottom of the
When the rotating speed sensor detects that the rotating speed of the engine rises to 72.5 percent of the rotating speed (9340r/min), the electronic controller disconnects and outputs a 28V voltage signal to the
When the rotating speed sensor detects that the rotating speed of the engine rises to 88 percent of the rotating speed (11340r/min), the electronic controller cuts off and outputs a 28V voltage signal to the
And during engine deceleration:
when the rotating speed sensor detects that the rotating speed of the engine is reduced to 86.1 percent of the rotating speed (11100r/min), the electronic controller outputs a 28V voltage signal to the
when the rotating speed sensor detects that the rotating speed of the engine is reduced to 70.6 percent (9100r/min), the electronic controller outputs a 28V voltage signal to the
when the rotating speed sensor detects that the rotating speed of the engine is reduced to 8 percent (1030r/min), the electronic controller disconnects and outputs a 28V voltage signal to the
It can be understood that the rotating speeds corresponding to the opening valve and the closing valve in the processes of increasing and decreasing the rotating speed are different, so that the slight fluctuation of the rotating speed caused by the opening or closing of the air bleeding valve can be effectively avoided, and the working stability of the engine is ensured.
Preferably, the electronic controller is further electrically connected to the
In addition, the third embodiment of the invention also provides an aircraft engine which adopts the compressor bleed air control system.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
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