CN104267238A - Testing device for pneumatic actuator - Google Patents

Testing device for pneumatic actuator Download PDF

Info

Publication number
CN104267238A
CN104267238A CN201410507491.9A CN201410507491A CN104267238A CN 104267238 A CN104267238 A CN 104267238A CN 201410507491 A CN201410507491 A CN 201410507491A CN 104267238 A CN104267238 A CN 104267238A
Authority
CN
China
Prior art keywords
stand
torque stand
rigid rod
pneumatic actuator
fixed
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.)
Granted
Application number
CN201410507491.9A
Other languages
Chinese (zh)
Other versions
CN104267238B (en
Inventor
姜航
王小春
王刚
林明辉
周欣欢
周鹏
萧剑平
邹永
雷燕
梅记敏
曹白玉
朱莲香
雷媛萍
吴俊演
马洪成
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.)
Jiangnan Industries Group Co Ltd
Original Assignee
Jiangnan Industries Group Co Ltd
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 Jiangnan Industries Group Co Ltd filed Critical Jiangnan Industries Group Co Ltd
Priority to CN201410507491.9A priority Critical patent/CN104267238B/en
Publication of CN104267238A publication Critical patent/CN104267238A/en
Application granted granted Critical
Publication of CN104267238B publication Critical patent/CN104267238B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The invention relates to a testing device for a pneumatic actuator, and belongs to the technical field of technological equipment. The testing device is mainly and technically characterized by comprising a base, an auxiliary torsion frame, a potentiometer, a fixing screw, bearings, a left clamp, a fixing frame foundation, a fixing frame, a right clamp, a rigid rod, a support, a pointer, a moment calibration disc, a main torsion frame, an adjusting sliding block, an adjusting screw and fastening bolts; the auxiliary torsion frame, the main torsion frame and the fixing frame foundation are fixed to the base through the bolts, the left clamp and the right clamp are fixed into the two horizontal and coaxial bearings, can horizontally swing on the auxiliary torsion frame and the main torsion frame by the angle within the range from -15 degrees to 15 degrees respectively and drive the potentiometer and the rigid rod to move respectively, the potentiometer outputs the swing angle of a rudder of the pneumatic actuator in an electric signal mode, and the rigid rod provides simulation load moment for the pneumatic actuator. The testing device has the advantages that the structure is simple and reasonable, testing and operation are convenient and quick, and reliability is high.

Description

A kind of pneumatic actuator proving installation
Technical field
The present invention relates to a kind of pneumatic actuator proving installation, belong to equipment Technology field, it is mainly used in carrying out accurately, in real time, comprehensively testing to the performance of each parameter of pulse-width modulation type pneumatic actuator.
Background technology
Pneumatic actuator is a kind of precision, responsive electronic devices and components, and carrying out accurately each parameter of pneumatic actuator, in real time, comprehensively testing is the basic guarantee grasping its performance.In background technology, the method for domestic existing test pneumatic actuator parameter has multiple, and device and equipment accordingly for testing pneumatic actuator is also complicated and simple differs, and these devices and equipment are all not enough below ubiquity:
1) proving installation structure is too complicated, and precision precision is higher, manufactures maintenance cost high, is unfavorable for processing and assembling simultaneously.
2) loading moment calculating and regulate more loaded down with trivial details, directly affect work efficiency.
3) performance parameter of testing is less, can not once obtain test result comprehensively and accurately, simultaneously because test process is more complicated, affects the consistance of test result.
In order to overcome above-mentioned deficiency, we develop pneumatic actuator proving installation.
Summary of the invention
Technical matters to be solved by this invention to provide a kind of pneumatic actuator proving installation, it is by being loaded on fixed mount and a left side by tested pneumatic actuator, in right two fixtures, left, right fixture drives pot and rigid rod action respectively, the pendulum angle of pneumatic actuator rudder sheet exports by pot as electronic signals, rigid rod provides fictitious load moment for pneumatic actuator, simultaneously by the time delay of external test circuitry to pneumatic actuator, pick-up current, steady operation electric current, the parameter indexs such as maximum operation frequency carry out accurately, in real time, comprehensive test.
The technical scheme that the present invention solves the employing of its technical matters is: it comprises base, secondary torque stand, pot, gib screw, bearing, left fixture, fixing stand, fixed mount, right fixture, rigid rod, support, pointer, moment demarcation dish, main torque stand, adjusting slider, adjusting screw(rod), fastening bolt
Multiple fastening bolt is loaded on the mounting hole bottom secondary torque stand, main torque stand, secondary torque stand, main torque stand is symmetrically fixed on respectively the both sides of base,
Fixing stand equidistantly in secondary torque stand, main torque stand be fixed on the side in the middle part of base by multiple fastening bolt,
Fixed mount bolt is fixed on fixing stand,
2 bearings are loaded in the bearing mounting hole of secondary torque stand, main torque stand upper end respectively,
2 bearing levels on secondary torque stand and main torque stand are coaxial,
The open slot subtend of left fixture, right fixture is installed and is individually fixed in 2 bearings of secondary torque stand, main torque stand,
Left fixture and right fixture can make the horizontal hunting that maximum angle is ± 15 ° respectively on secondary torque stand, main torque stand,
Tested pneumatic actuator can be placed on fixed mount, and the rudder sheet that the pneumatic actuator left and right sides is launched can be installed in the open slot of left fixture, right fixture respectively,
Pot is loaded on the rear portion of left fixture and is fixed on secondary torque stand by gib screw, and drive pot to rotate during left fixture horizontal hunting, the pendulum angle of pneumatic actuator rudder sheet exports by pot as electronic signals,
Adjusting slider is loaded in the bar-shaped trough of main torque stand inside,
Rigid rod is threaded onto in the center pit of adjusting slider, and the lower end of rigid rod is vertically plugged in the jack bottom main torque stand, and the bulb of rigid rod upper end is loaded on the connecting hole of right fixture lower end,
Stir rigid rod by the bulb of rigid rod upper end during right fixture horizontal hunting, rigid rod provides fictitious load moment for pneumatic actuator,
Adjusting screw(rod) spinning in the rear end of adjusting slider,
Adjusting slider can slide up and down along rigid rod in the bar-shaped trough of main torque stand inside, and the height adjusting adjusting slider up and down regulates rigid rod to be supplied to the fictitious load moment of pneumatic actuator, screws adjusting screw(rod) and is fixed on rigid rod by adjusting slider side direction,
Moment demarcation dish is loaded on the rear portion of right fixture and is fixed on main torque stand, and moment demarcation dish posts angle indicating graduation,
Support is fixed on the top of main torque stand by screw, and pointer vertically adheres on the cantilever that support protracts, when moment demarcation dish does not stress square, and the zero graduation on pointed moment demarcation dish.
Before test, tested pneumatic actuator is fixed on fixed mount, the rudder sheet that the pneumatic actuator left and right sides is launched is installed in the open slot of left fixture, right fixture respectively, pneumatic actuator connects external test circuitry, according to the height of the fictitious load moment adjustment adjusting slider of setting.
During test, the rudder sheet that left fixture, right fixture launch with the pneumatic actuator left and right sides swings, wherein left fixture swings and drives pot to rotate, pot reads time delay by contrast standard signal and potentiometric voltage curve, and judges whether pneumatic actuator rudder sheet swings according to the pendulum angle of rudder sheet and put in place; Right fixture swings and stirs rigid rod, and rigid rod provides fictitious load moment for pneumatic actuator.In the rudder sheet swing process of the pneumatic actuator left and right sides, the parameter index such as pick-up current, steady operation electric current, maximum operation frequency of external test circuitry to pneumatic actuator is tested.
The beneficial effect that the present invention is compared with the existing technology produced
1, because this device adopts rigid rod simply and effectively to provide fictitious load moment, simultaneously by adjusting slider adjustment fictitious load moment size, the requirement that rigid rod parameter is calculated is greatly reduced, and the process and assemble accuracy requirement of correlated parts.
2, because pot rotates with the swing of fixture, the pendulum angle of pneumatic actuator rudder sheet is exported as electronic signals, the performance of pneumatic actuator can be reflected accurately, in real time.
3, it have simple and reasonable, test operation is convenient and swift, high reliability.
Accompanying drawing explanation
Fig. 1 is the structural representation of pneumatic actuator proving installation of the present invention.
Fig. 2 is the perspective view of Fig. 1.
Embodiment
Below in conjunction with accompanying drawing, most preferred embodiment of the present invention is further described.
Referring to Fig. 1,2, a kind of pneumatic actuator proving installation, it comprises base 1, secondary torque stand 2, pot 3, gib screw 4, bearing 5, left fixture 6, fixing stand 7, fixed mount 8, right fixture 9, rigid rod 10, support 11, pointer 12, moment demarcation dish 13, main torque stand 14, adjusting slider 15, adjusting screw(rod) 16, fastening bolt 17.
Multiple fastening bolt 17 is loaded on the mounting hole bottom secondary torque stand 2, main torque stand 14, regulates the position of mounting hole and fastening bolt 17, secondary torque stand 2, main torque stand 14 is symmetrically fixed on respectively the both sides of base 1.
Fixing stand 7 is equidistantly in secondary torque stand 2, main torque stand 14 be fixed on the side in the middle part of base 1 by multiple fastening bolt 17.
Fixed mount 8 bolt is fixed on fixing stand 7.
2 bearings 5 are loaded in the bearing mounting hole of secondary torque stand 2, main torque stand 14 upper end respectively.
2 bearing 5 levels on secondary torque stand 2 and main torque stand 14 are coaxial.
The open slot subtend of left fixture 6, right fixture 9 is installed and is individually fixed in 2 bearings 5 of secondary torque stand 2, main torque stand 14.
Left fixture 6 and right fixture 9 can make the horizontal hunting that maximum angle is ± 15 ° respectively on secondary torque stand 2, main torque stand 14.
Tested pneumatic actuator can be placed on fixed mount 8, and the rudder sheet that the pneumatic actuator left and right sides is launched can be installed in the open slot of left fixture 6, right fixture 9 respectively.
Pot 3 is loaded on the rear portion of left fixture 6 and is fixed on secondary torque stand 2 by gib screw 4, pot 3 is driven to rotate during left fixture 6 horizontal hunting, the pendulum angle of pneumatic actuator rudder sheet exports by pot 3 as electronic signals, pot 3 reads time delay by contrast standard signal and potentiometric voltage curve, and judges whether pneumatic actuator rudder sheet swings according to the pendulum angle of rudder sheet and put in place.
Adjusting slider 15 is loaded in the bar-shaped trough of main torque stand 14 inside.
Rigid rod 10 is threaded onto in the center pit of adjusting slider 15, and the lower end of rigid rod 10 is vertically plugged in the jack bottom main torque stand 14, and the bulb of rigid rod 10 upper end is loaded on the connecting hole of right fixture 9 lower end.
Stir rigid rod 10 by the bulb of rigid rod 10 upper end during right fixture 9 horizontal hunting, rigid rod 10 provides fictitious load moment for pneumatic actuator.
Adjusting screw(rod) 16 spinning is in the rear end of adjusting slider 15.
Adjusting slider 15 can slide up and down along rigid rod 10 in the bar-shaped trough of main torque stand 14 inside, screw adjusting screw(rod) 16 and adjusting slider 15 side direction can be fixed on rigid rod 10, the Height Adjustable rigid rod 10 adjusting adjusting slider 15 is up and down supplied to the fictitious load moment of pneumatic actuator.
Moment demarcation dish 13 is loaded on the rear portion of right fixture 9 and is fixed on main torque stand 14, and moment demarcation dish 13 posts angle indicating graduation.
Support 11 is fixed on the top of main torque stand 14 by screw.
Pointer 12 vertically adheres on the cantilever that support 11 protracts, when moment demarcation dish 13 does not stress square, and the zero graduation on pointer 12 meridian seeking moment demarcation dish 13.
Before test, tested pneumatic actuator is fixed on fixed mount 8, the rudder sheet that the pneumatic actuator left and right sides is launched is installed in the open slot of left fixture 6, right fixture 9 respectively, pneumatic actuator connects external test circuitry, according to the height of the fictitious load moment adjustment adjusting slider 15 of setting.
During test, the rudder sheet that left fixture 6, right fixture 9 launch with the pneumatic actuator left and right sides swings, wherein left fixture 6 swings and drives pot 3 to rotate, pot 3 reads time delay by contrast standard signal and potentiometric voltage curve, and judges whether pneumatic actuator rudder sheet swings according to the pendulum angle of rudder sheet and put in place; Right fixture 9 swings and stirs rigid rod 10, and rigid rod 10 provides fictitious load moment for pneumatic actuator.In the rudder sheet swing process of the pneumatic actuator left and right sides, the parameter index such as pick-up current, steady operation electric current, maximum operation frequency of external test circuitry to pneumatic actuator is tested.

Claims (2)

1. a pneumatic actuator proving installation, is characterized in that it comprises base (1), secondary torque stand (2), pot (3), gib screw (4), bearing (5), left fixture (6), fixing stand (7), fixed mount (8), right fixture (9), rigid rod (10), support (11), pointer (12), moment demarcation dish (13), main torque stand (14), adjusting slider (15), adjusting screw(rod) (16), fastening bolt (17);
Multiple fastening bolt (17) is loaded on the mounting hole of secondary torque stand (2), main torque stand (14) bottom, secondary torque stand (2), main torque stand (14) is symmetrically fixed on respectively the both sides of base (1);
Fixing stand (7) is equidistantly in secondary torque stand (2), main torque stand (14) be fixed on the side at base (1) middle part by multiple fastening bolt (17);
Fixed mount (8) bolt is fixed on fixing stand (7);
2 bearings (5) are loaded in the bearing mounting hole of secondary torque stand (2), main torque stand (14) upper end respectively;
2 bearing (5) levels on secondary torque stand (2) and main torque stand (14) are coaxial;
The open slot subtend of left fixture (6), right fixture (9) is installed and is individually fixed in 2 bearings (5) of secondary torque stand (2), main torque stand (14);
Left fixture (6) and right fixture (9) at secondary torque stand (2), main torque stand, (14) can make horizontal hunting respectively;
Pot (3) is loaded on the rear portion of left fixture (6) and is fixed on secondary torque stand (2) by gib screw (4), drive pot (3) to rotate during left fixture (6) horizontal hunting, the pendulum angle of pneumatic actuator rudder sheet exports by pot (3) as electronic signals;
Adjusting slider (15) is loaded in the inner bar-shaped trough of main torque stand (14);
Rigid rod (10) is threaded onto in the center pit of adjusting slider (15), and the lower end of rigid rod (10) is vertically plugged in the jack of main torque stand (14) bottom, and the bulb of rigid rod (10) upper end is loaded on the connecting hole of right fixture (9) lower end;
Stir rigid rod (10) by the bulb of rigid rod (10) upper end during right fixture (9) horizontal hunting, rigid rod (10) provides fictitious load moment for pneumatic actuator;
Adjusting screw(rod) (16) spinning is in the rear end of adjusting slider (15);
Adjusting slider (15) can slide up and down along rigid rod (10) in the bar-shaped trough that main torque stand (14) is inner, the height adjusting adjusting slider (15) up and down regulates rigid rod (10) to be supplied to the fictitious load moment of pneumatic actuator, screws adjusting screw(rod) (16) and is fixed on rigid rod (10) by adjusting slider (15) side direction;
Moment demarcation dish (13) is loaded on the rear portion of right fixture (9) and is fixed on main torque stand (14), and moment demarcation dish (13) posts angle indicating graduation;
Support (11) is fixed on the top of main torque stand (14) by screw, pointer (12) vertically adheres on the cantilever that support (11) protracts, when moment demarcation dish (13) does not stress square, and the zero graduation in pointer (12) meridian seeking moment demarcation dish (13).
2. pneumatic actuator proving installation according to claim 1, is characterized in that: described left fixture (6) and right fixture (9) are ± 15 ° at the maximum angle of secondary torque stand (2), the upper horizontal hunting of main torque stand (14) respectively.
CN201410507491.9A 2014-09-28 2014-09-28 Testing device for pneumatic actuator Active CN104267238B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410507491.9A CN104267238B (en) 2014-09-28 2014-09-28 Testing device for pneumatic actuator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410507491.9A CN104267238B (en) 2014-09-28 2014-09-28 Testing device for pneumatic actuator

Publications (2)

Publication Number Publication Date
CN104267238A true CN104267238A (en) 2015-01-07
CN104267238B CN104267238B (en) 2017-02-08

Family

ID=52158778

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410507491.9A Active CN104267238B (en) 2014-09-28 2014-09-28 Testing device for pneumatic actuator

Country Status (1)

Country Link
CN (1) CN104267238B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111982008A (en) * 2020-08-28 2020-11-24 四川三联新材料有限公司 Cigarette filter stick cutting depth detection device
CN113466058A (en) * 2021-07-02 2021-10-01 王永雪 Fixing performance detection device for steel structure engineering and use method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050120785A1 (en) * 2003-12-09 2005-06-09 Hyundai Motor Company Variable intake system monitoring apparatus
CN201935665U (en) * 2010-12-22 2011-08-17 郑州大学 Tabletop fixed type torsional angle measuring apparatus
CN103899830A (en) * 2014-04-04 2014-07-02 徐州阿卡控制阀门有限公司 Intelligent-type pneumatic actuating mechanism with fault diagnosis function
CN203770808U (en) * 2014-04-04 2014-08-13 徐州阿卡控制阀门有限公司 Intelligent pneumatic actuator with fault diagnosis function
CN204154788U (en) * 2014-09-28 2015-02-11 江南工业集团有限公司 A kind of pneumatic actuator proving installation

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050120785A1 (en) * 2003-12-09 2005-06-09 Hyundai Motor Company Variable intake system monitoring apparatus
CN201935665U (en) * 2010-12-22 2011-08-17 郑州大学 Tabletop fixed type torsional angle measuring apparatus
CN103899830A (en) * 2014-04-04 2014-07-02 徐州阿卡控制阀门有限公司 Intelligent-type pneumatic actuating mechanism with fault diagnosis function
CN203770808U (en) * 2014-04-04 2014-08-13 徐州阿卡控制阀门有限公司 Intelligent pneumatic actuator with fault diagnosis function
CN204154788U (en) * 2014-09-28 2015-02-11 江南工业集团有限公司 A kind of pneumatic actuator proving installation

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111982008A (en) * 2020-08-28 2020-11-24 四川三联新材料有限公司 Cigarette filter stick cutting depth detection device
CN113466058A (en) * 2021-07-02 2021-10-01 王永雪 Fixing performance detection device for steel structure engineering and use method

Also Published As

Publication number Publication date
CN104267238B (en) 2017-02-08

Similar Documents

Publication Publication Date Title
CN204154788U (en) A kind of pneumatic actuator proving installation
CN103197147A (en) Solar cell multifunctional contact resistance automatic measuring instrument and measuring system thereof
CN103364755A (en) Full-automatic scanning testing device, full-automatic scanning testing system and full-automatic scanning testing method for electric energy meter power frequency magnetic field
CN102736054A (en) Multi-meter-position automatic connection device and connection method for electric energy meter checking device
CN104267238A (en) Testing device for pneumatic actuator
CN204009028U (en) Magnet mgnetic observations device
CN202956481U (en) Detection device for non-contact power transmission line high-voltage electroscope
CN208588502U (en) A kind of bullet arrow quality center of mass rotary inertia testboard
CN106767239B (en) A kind of turbine disk assembling assembly blade installation site measuring device
CN201765051U (en) Weighing sensor corner load error tester
CN201859100U (en) Engine flywheel detecting device
CN103592466A (en) Automatic lot sizing static rolling testing device for MEMS acceleration sensor
CN105115707A (en) Testing device and testing method for dynamic characteristic of joint curved surface faying surface
CN206209063U (en) A kind of novel test circuit board robot
CN209417246U (en) Three position mechanism motor braking test equipment
CN202701755U (en) Arc plate adjusting device of solar trough collector
CN108981904A (en) A kind of Portable mounting base of vibration sensor
CN205139301U (en) Tracking tester
CN106645314B (en) Fault diagnosis device and detection method for FDR tubular soil moisture sensor
CN108106833A (en) Disconnecting link folding force tester
CN203224512U (en) Device capable of adjusting height of AFM sample
CN102331373A (en) Mobile temperature control constant stress loading testing device
CN105467175A (en) An angle-adjustable test machine
CN204649371U (en) A kind of low-frequency vibration calibrating installation with humiture impact
CN205691704U (en) A kind of resistance to electricity trace tester

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant