CN105333207B - A kind of bleed valve based on flow-rate adjustment - Google Patents

A kind of bleed valve based on flow-rate adjustment Download PDF

Info

Publication number
CN105333207B
CN105333207B CN201510922489.2A CN201510922489A CN105333207B CN 105333207 B CN105333207 B CN 105333207B CN 201510922489 A CN201510922489 A CN 201510922489A CN 105333207 B CN105333207 B CN 105333207B
Authority
CN
China
Prior art keywords
bleed
butterfly valve
sensor
flow
exhaust manifolds
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.)
Active
Application number
CN201510922489.2A
Other languages
Chinese (zh)
Other versions
CN105333207A (en
Inventor
周景锋
张欣荣
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.)
Xian Aircraft Design and Research Institute of AVIC
Original Assignee
Xian Aircraft Design and Research Institute of AVIC
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 Xian Aircraft Design and Research Institute of AVIC filed Critical Xian Aircraft Design and Research Institute of AVIC
Priority to CN201510922489.2A priority Critical patent/CN105333207B/en
Publication of CN105333207A publication Critical patent/CN105333207A/en
Application granted granted Critical
Publication of CN105333207B publication Critical patent/CN105333207B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00Actuating devices; Operating means; Releasing devices
    • F16K31/12Actuating devices; Operating means; Releasing devices actuated by fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K37/00Special means in or on valves or other cut-off apparatus for indicating or recording operation thereof, or for enabling an alarm to be given
    • F16K37/0075For recording or indicating the functioning of a valve in combination with test equipment
    • F16K37/0083For recording or indicating the functioning of a valve in combination with test equipment by measuring valve parameters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K37/00Special means in or on valves or other cut-off apparatus for indicating or recording operation thereof, or for enabling an alarm to be given
    • F16K37/0075For recording or indicating the functioning of a valve in combination with test equipment
    • F16K37/0091For recording or indicating the functioning of a valve in combination with test equipment by measuring fluid parameters

Abstract

The invention discloses a kind of bleed valve based on flow-rate adjustment.The bleed valve based on flow-rate adjustment includes bleed conduit;Exhaust manifolds;The inlet end of butterfly valve, butterfly valve is connect with bleed conduit, and exhaust end is connect with exhaust manifolds;Temperature sensor for detecting gas temperature in exhaust manifolds;Pressure sensor for detecting gas pressure in exhaust manifolds;Position sensor, position sensor are used to detect the position of butterfly valve;Command device;Control device, control device receive the signal of temperature sensor, pressure sensor, position sensor, and are transferred to command device;Driving device;Command device will feed back to driving device from the inlet end bleed of butterfly valve by pneumatic signal, and driving device is used to control the aperture of butterfly valve.Beneficial effects of the present invention:The bleed valve of the present invention can adjust bleed flow according to actual demand, reduce unnecessary bleed waste, improve the bleed efficiency of anti-icing system, saved the energy of engine.

Description

A kind of bleed valve based on flow-rate adjustment
Technical field
The present invention relates to aircraft air supply system or hot gas anti-deicing systems technology fields, and in particular to one kind being based on flow tune The bleed valve of section.
Background technology
Flow-rate adjustment, this hair can not be carried out currently used for aircraft air supply system or the bleed valve of the anti-deicing system of hot gas The parameters such as bright bleed flow by valve upstream, the bleed temperature and pressure in downstream, external environment information are analyzed, right Valve opening is adjusted, and controls bleed flow, solves the problems, such as that bleed flow can be adjusted according to actual demand.
Invention content
The object of the present invention is to provide a kind of bleed valve based on flow-rate adjustment, to solve or at least mitigate background technology In required bleed flow the problem of being adjusted according to actual demand.
The technical scheme is that:A kind of bleed valve based on flow-rate adjustment is provided, including bleed conduit;Exhaust is led Pipe;The inlet end of butterfly valve, the butterfly valve is connect with bleed conduit, and the exhaust end of the butterfly valve is connect with exhaust manifolds;Temperature passes Sensor and pressure sensor;The temperature sensor is used to detect the temperature of gas in exhaust manifolds, and the pressure sensor is used In the pressure of gas in detection exhaust manifolds;Position sensor, the position sensor are used to detect the position of butterfly valve;Instruction dress It sets;Control device, the control device receive the signal of temperature sensor, pressure sensor, position sensor, and are transferred to finger Enable device;Driving device;Described instruction device will feed back to driving dress from the inlet end bleed of butterfly valve by pneumatic signal It sets, the driving device is used to control the aperture of butterfly valve.
Preferably, the bleed valve based on flow-rate adjustment also includes external environmental signal incoming line, the control Device receives external environmental signals by external environmental signal incoming line.
Preferably, the external environmental signals include temperature signal.
Preferably, the temperature sensor is dual channel sensor.
Preferably, there are two the pressure sensor settings, two pressure sensors are arranged in parallel.
Beneficial effects of the present invention:The control device of the present invention is by receiving temperature sensor, pressure sensor and position The feedback information of sensor, and it is transferred to command device, butterfly valve is realized in the position that refrigerating plant controls butterfly valve according to feedback information The adjusting of aperture, bleed valve of the invention can adjust bleed flow according to actual demand, reduce unnecessary bleed waste, The bleed efficiency for improving anti-icing system, has saved the energy of engine.
Description of the drawings
Fig. 1 is the schematic diagram of an embodiment of the bleed valve based on flow-rate adjustment of the present invention.
Wherein, 1- bleeds conduit, 3- command devices, 5- control devices, 6- external environmental signals incoming lines, 7- temperature pass Sensor, 8- pressure sensors, 10- driving devices, 11- exhaust manifolds, 12- butterfly valves, 13- position sensors.
Specific implementation mode
To keep the purpose, technical scheme and advantage that the present invention is implemented clearer, below in conjunction in the embodiment of the present invention Attached drawing, technical solution in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from beginning to end or class As label indicate same or similar element or element with the same or similar functions.Described embodiment is the present invention A part of the embodiment, instead of all the embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to use It is of the invention in explaining, and be not considered as limiting the invention.Based on the embodiments of the present invention, ordinary skill people The every other embodiment that member is obtained without creative efforts, shall fall within the protection scope of the present invention.Under Face is described in detail the embodiment of the present invention in conjunction with attached drawing.
In the description of the present invention, it is to be understood that, term "center", " longitudinal direction ", " transverse direction ", "front", "rear", The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom" "inner", "outside" is based on attached drawing institute The orientation or positional relationship shown, is merely for convenience of description of the present invention and simplification of the description, and does not indicate or imply the indicated dress It sets or element must have a particular orientation, with specific azimuth configuration and operation, therefore should not be understood as protecting the present invention The limitation of range.
As shown in Figure 1, a kind of bleed valve based on flow-rate adjustment, including bleed conduit 1 and exhaust manifolds 11, also include The inlet end of butterfly valve 12, butterfly valve 12 is connect with bleed conduit 1, and the exhaust end of butterfly valve 12 is connect with exhaust manifolds 11;Temperature sensing Device 7 and pressure sensor 8;The temperature sensor 7 is used to detect the temperature of gas in exhaust manifolds 11, the pressure sensor 8 pressure for detecting gas in exhaust manifolds 11;Position sensor 13, the position sensor 13 is for detecting butterfly valve 12 Position;Command device 3;Control device 5, the control device 5 receive temperature sensor 7, pressure sensor 8, position sensor 13 signal, and it is transferred to command device 3;Driving device 10;Command device 3 will pass through from the inlet end bleed of butterfly valve 12 Pneumatic signal feeds back to driving device 10, and driving device 10 is used to control the aperture of butterfly valve 12.
In the present embodiment, the bleed valve based on flow-rate adjustment also includes external environmental signal incoming line 6, control Device 5 processed receives external environmental signals by external environmental signal incoming line 6.
In the present embodiment, the external environmental signals include temperature signal.
In the present embodiment, temperature sensor 7 is dual channel sensor.Temperature sensor 7 includes that a temperature measures master Channel and an alternate channel, after main channel is broken down, alternate channel can substitute main channel and complete temperature detecting function.
In the present embodiment, the temperature-measuring element in temperature sensor uses thermocouple, the advantage is that, thermocouple is surveyed Amount temperature range is wider, and anti shock and vibration is good, is more suitable for dangerous rugged environment.Response is fast, because they are small, heat Capacity is low, and thermocouple responds soon temperature change, can be in hundreds of milliseconds to temperature change especially when induced junction chalaza is exposed It responds.Since thermocouple does not need excitation power supply, it is not easy spontaneous heating, use is safer.
In the present embodiment, there are two the settings of pressure sensor 8, two pressure sensors 8 are arranged in parallel.Two pressure pass 8 relatively independent work of sensor, and detection signal is passed into control device 5, when two pressure sensings that control device 5 receives When the signal difference of device 8 is more than setting value, illustrate that one of pressure sensor breaks down, two pressure sensors can phase It mutually checks, improves the accuracy in detection of system.In the present embodiment, two pressure sensors 8 are identical two sensors, The signal difference of described two pressure sensors 8 is the precision set according to pressure sensor.
In the present embodiment, control device 5 has binary channels, one of them is set as main channel, another is as spare Channel, main channel and alternate channel are 5 independent control channels, and after main channel is broken down, alternate channel can substitute Main channel complete independently control task improves the reliability of system control.
The specific implementation process of the present embodiment is:High temperature and pressure air from engine enters butterfly by bleed conduit 1 The inlet end of valve 12 supplies for anti-icing system from the exhaust end of butterfly valve 12 by exhaust manifolds 11, is arranged on exhaust manifolds 11 There are temperature sensor 7 and two pressure sensors 8 in parallel, temperature sensor 7 to detect the gas temperature on exhaust manifolds 11, and The temperature signal detected is fed back into control device 5, pressure sensor 8 detects the gas pressure on exhaust manifolds 11, and will The pressure signal detected feeds back to control device 5, meanwhile, control device 5 also receives defeated by external environmental signals incoming line 6 The ambient temperature signal entered, the ambient temperature signal are the temperature signal of aircraft exterior.Exhaust of the control device 5 to receiving After the temperature signal of temperature signal, pressure signal and aircraft exterior on conduit 11 is handled it, by treated, information is transmitted To command device 3.
It is understood that control device 5 is to temperature signal, pressure signal and the aircraft on the exhaust manifolds 11 that receive The processing that external temperature signal is made is determined according to the course line of aircraft.
In the entire course line track of aircraft, for its freezing environment of different ice fields difference, 5 basis of control device The corresponding control air pressure for the different freezing environments setting passed through and the control algolithm of temperature are also different.It is more tight for freezing The segment of weight, the air pressure and temperature of setting are higher, for the lighter segment of freezing, the air pressure and temperature of setting compared with It is low, to realize the personalized gas supply for being directed to different ice-formation conditions, compared with prior art in the segment the most serious that freezes Air pressure and temperature are set, and The present invention reduces the wastes more than bleed, have saved the energy of engine.
The inlet end in the compressed air source and butterfly valve 12 of command device 3, command device 3 are filled control by pneumatic signal It sets 5 transmission information and is sent to driving device 10, driving device 10 drives butterfly valve 12 to move, and realizes the change of 12 position of butterfly valve, with The aperture of regulating butterfly valve 12.
It is an advantage of the invention that the bleed flow for solving air supply system or anti-icing system can be adjusted according to actual demand The problem of section, and then the bleed from engine is reduced, energy consumption is reduced, the bleed efficiency of air supply system or anti-icing system is improved, is increased Add the economy and reliability of airplane operation.
It is last it is to be noted that:The above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations.To the greatest extent Present invention has been described in detail with reference to the aforementioned embodiments for pipe, it will be understood by those of ordinary skill in the art that:It is still Can be with technical scheme described in the above embodiments is modified, or which part technical characteristic is equally replaced It changes;And these modifications or replacements, the essence for various embodiments of the present invention technical solution that it does not separate the essence of the corresponding technical solution God and range.

Claims (5)

1. a kind of bleed valve based on flow-rate adjustment, including bleed conduit (1) and exhaust manifolds (11), it is characterised in that:Also Including
The inlet end of butterfly valve (12), the butterfly valve (12) is connect with bleed conduit (1), the exhaust end and exhaust manifolds of butterfly valve (12) (11) it connects;
Temperature sensor (7) and pressure sensor (8), the temperature sensor (7) and pressure sensor (8) are arranged in parallel and connect Exhaust manifolds (12) and control device (5) are connected to, the temperature sensor (7) is used to detect the temperature of exhaust manifolds (11) interior gas Degree, the pressure sensor (8) are used to detect the pressure of exhaust manifolds (11) interior gas;
Position sensor (13), the position sensor (13) are connected to butterfly valve (12), the position for detecting butterfly valve (12);
Command device (3);
Control device (5), the control device (5) receive temperature sensor (7), pressure sensor (8), position sensor (13) Signal, and be transferred to command device (3);
Driving device (10), the driving device (10) are connected to butterfly valve (12);
Described instruction device (3) will feed back to driving device (10) from the inlet end bleed of butterfly valve (12) by pneumatic signal, The driving device (10) is used to control the aperture of butterfly valve (12).
2. the bleed valve based on flow-rate adjustment as described in claim 1, it is characterised in that:Also include that external environmental signal is defeated Enter circuit (6), the control device (5) receives external environmental signals by external environmental signal incoming line (6).
3. the bleed valve based on flow-rate adjustment as claimed in claim 2, it is characterised in that:The external environmental signals include Temperature signal.
4. the bleed valve based on flow-rate adjustment as described in claim 1, it is characterised in that:The temperature sensor (7) is Dual channel sensor.
5. the bleed valve based on flow-rate adjustment as described in claim 1, it is characterised in that:The pressure sensor (8) sets There are two setting, two pressure sensors (8) are arranged in parallel.
CN201510922489.2A 2015-12-11 2015-12-11 A kind of bleed valve based on flow-rate adjustment Active CN105333207B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510922489.2A CN105333207B (en) 2015-12-11 2015-12-11 A kind of bleed valve based on flow-rate adjustment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510922489.2A CN105333207B (en) 2015-12-11 2015-12-11 A kind of bleed valve based on flow-rate adjustment

Publications (2)

Publication Number Publication Date
CN105333207A CN105333207A (en) 2016-02-17
CN105333207B true CN105333207B (en) 2018-08-24

Family

ID=55283906

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510922489.2A Active CN105333207B (en) 2015-12-11 2015-12-11 A kind of bleed valve based on flow-rate adjustment

Country Status (1)

Country Link
CN (1) CN105333207B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109224332A (en) * 2018-09-14 2019-01-18 南京耀泽电子科技有限公司 Integral intelligent respirator back board device and collecting method
JP7320473B2 (en) * 2020-03-27 2023-08-03 Ckd株式会社 butterfly valve

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1461429A (en) * 2000-09-20 2003-12-10 富加西提公司 Fluid flow controller and method of operation
CN1751176A (en) * 2003-02-20 2006-03-22 株式会社三国 Sensor module unit and throttle device with the same
CN201310667Y (en) * 2008-12-09 2009-09-16 杭州展德软件技术有限公司 Electronic dynamic balancing electric adjustable valve capable of realizing remote monitor and control
JP2010117330A (en) * 2008-11-14 2010-05-27 Kanto Chem Co Inc Method of diagnosing air operation valve, air operation valve diagnosis device, and air operation valve
CN201773324U (en) * 2010-06-29 2011-03-23 张家港市沃斯汀新材料研究所有限公司 Flow control device
GB201103306D0 (en) * 2011-02-28 2011-04-13 Smartap A Y Ltd Household electronic mixing-valve device
CN102687087A (en) * 2009-10-15 2012-09-19 关键***公司 Method and apparatus for gas flow control
CN102927343A (en) * 2012-11-07 2013-02-13 昆山北极光电子科技有限公司 Dynamic flow on-line detecting system
CN203363380U (en) * 2013-07-12 2013-12-25 上海市通用机械技术研究所有限公司 Fluid stop valve
CN103982695A (en) * 2014-05-19 2014-08-13 东正科技有限公司 Intelligent controller for pneumatic valve

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9727062B2 (en) * 2011-07-14 2017-08-08 Onesubsea Ip Uk Limited Shape memory alloy thermostat for subsea equipment

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1461429A (en) * 2000-09-20 2003-12-10 富加西提公司 Fluid flow controller and method of operation
CN1751176A (en) * 2003-02-20 2006-03-22 株式会社三国 Sensor module unit and throttle device with the same
JP2010117330A (en) * 2008-11-14 2010-05-27 Kanto Chem Co Inc Method of diagnosing air operation valve, air operation valve diagnosis device, and air operation valve
CN201310667Y (en) * 2008-12-09 2009-09-16 杭州展德软件技术有限公司 Electronic dynamic balancing electric adjustable valve capable of realizing remote monitor and control
CN102687087A (en) * 2009-10-15 2012-09-19 关键***公司 Method and apparatus for gas flow control
CN201773324U (en) * 2010-06-29 2011-03-23 张家港市沃斯汀新材料研究所有限公司 Flow control device
GB201103306D0 (en) * 2011-02-28 2011-04-13 Smartap A Y Ltd Household electronic mixing-valve device
CN102927343A (en) * 2012-11-07 2013-02-13 昆山北极光电子科技有限公司 Dynamic flow on-line detecting system
CN203363380U (en) * 2013-07-12 2013-12-25 上海市通用机械技术研究所有限公司 Fluid stop valve
CN103982695A (en) * 2014-05-19 2014-08-13 东正科技有限公司 Intelligent controller for pneumatic valve

Also Published As

Publication number Publication date
CN105333207A (en) 2016-02-17

Similar Documents

Publication Publication Date Title
US10071807B2 (en) Method and device for controlling an aircraft air conditioning system
WO2012056228A3 (en) Burner control systems and methods of operating a burner
CN105333207B (en) A kind of bleed valve based on flow-rate adjustment
CN203657295U (en) Multi-source adjusting and controlling ultra-low temperature heat pump
JP2014529709A5 (en)
GB2528549A (en) Method for detecting a fluid leak in a turbomachine and system for distributing a fluid
US10144521B2 (en) Electric compressor for use with a wing anti-ice system
US10974835B2 (en) Bleed air temperature and flow control system
CN101952171A (en) Aircraft propulsion assembly comprising hot air bleed systems
RU2016136162A (en) EVAPORATOR SAMPLING SYSTEM WITH GAS-CONDENSATE LIQUID PRESSURE ADJUSTMENT
CN105443246B (en) A kind of engine inlets anti-icing system
CN110595558A (en) Natural gas flow measurement system self-adaptive to ambient temperature
CN101352814A (en) Temperature control system for machine tool
US20120137712A1 (en) Method for operating an aircraft cooling system and aircraft cooling system
CN103727305A (en) Intelligent valve positioner
CN202582786U (en) Test device of aircraft engine bleed air system temperature sensor
CN105007766B (en) Pneumatic conveying equipment
CN103674522A (en) Valve test system
MX2021004317A (en) Water distillation apparatus, method and system.
CN109458701A (en) A kind of air-conditioning with defrosting function
CN107505957A (en) A kind of refrigeration system ground experiment temperature control equipment
CN203858871U (en) Control device of nuclear power plant air emission system
CN204203204U (en) A kind of ultralow temperature temperature control test platform
CN101788278A (en) Displacement sensing device for soft-pressing process control system of continuous casting machine
CN104235466B (en) A kind of its anti-noise pneumatic control valve

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant