CN105606704A - Airplane wheel hub integrated nondestructive detection system - Google Patents
Airplane wheel hub integrated nondestructive detection system Download PDFInfo
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- CN105606704A CN105606704A CN201510757779.6A CN201510757779A CN105606704A CN 105606704 A CN105606704 A CN 105606704A CN 201510757779 A CN201510757779 A CN 201510757779A CN 105606704 A CN105606704 A CN 105606704A
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Abstract
The invention discloses an airplane wheel hub integrated nondestructive detection system. The airplane wheel hub integrated nondestructive detection system comprises a pedestal, two cleaning subassemblies, a plurality of cleaning nozzles, two heating subassemblies, two fans, four transverse slide rails, two first lead screws, two first servo motors, a fixing subassembly, two supporting pedestals, a driving supporting subassembly, a first stepping motor, a driving coupling device, a moving working platform, a second servo motor, a moving supporting arm, a first flange, a moving supporting arm connecting piece, a fixed supporting arm, a detecting arm fixing support, two detecting arm rotating parts, a second stepping motor, two third stepping motors, two rotating detecting arms, two probe fixing subassemblies, a linear motor, a second lead screw, a transverse slide rail, a distributed electrical control subassembly, and two direct current motors. The airplane wheel hub integrated nondestructive detection system is capable of increasing detection efficiency greatly, detecting internal damages of airplane wheel hubs via automatic nondestructive detection means, avoiding false detection or missing detection caused by man-made causes, reducing labor intensity of maintenance personnel, and increasing detection accuracy.
Description
Technical field
The invention belongs to civil aircraft automatic Nondestructive field, particularly relate to a kind of airplane wheelThe integrated nondestructive detection system of wheel hub.
Background technology
The examination and maintenance of airline carriers of passengers are being brought into play key effect at aspects such as keeping its security and punctuality rate,And Aircraft landing gear system and wheel parts are as the critical component weight of operational support especially of airline carriers of passengersIn heavy.
In recent years, aircraft wheel hub in take-off and landing process ruptures suddenly, and has while smashing the event of bodyOccur, thereby had a strong impact on the safe flight of airline carriers of passengers. For example, on May 8th, 1997, south boatAfter empty CZ3456 heavily lands, wheel hub explosion causes aviation accident; On September 12nd, 2006 East Airways's Boeing-747The aircraft wheel hub that passenger plane occurs in Guangzhou breaks cabin event. By analyzing, above accident is all by aircraft machineWheel wheel hub cracks caused.
In the line maintenance of airline carriers of passengers, nondestructive inspection is generally used for the detection of airplane wheel wheel hub, its orderBe the situation that regularly detects airplane wheel wheel hub, find in time wheel hub crackle, in case there is jeopardizing flight peaceFull accident. But domestic operator mainly adopts and first disassembles wheel, then manual detection wheel at presentThe mode of wheel hub is carried out, and so not only detection efficiency is low and easy appearance " undetected " and " flase drop ", also simultaneouslyCan cause aircraft to stop field time long, thereby directly increase the operation cost of airline.
Along with developing rapidly of automation Dynamic Non-Destruction Measurement, Chinese industrial progresses into " Non-Destructive Testing 4.0Epoch ". In multiple fields such as machine-building, automobile industry, Aero-Space, automation Dynamic Non-Destruction MeasurementBecome the supplementary means of internationally recognized advanced manufacturing technology and new-product development. Employing airplane wheel wheel hubIn-situ detection method, can greatly reduce time of dismounting aircraft wheel hub in aircraft maintenance process, improves and detects effectRate; Adopt automatic nondestructiving detecting means to detect the internal injury of aircraft wheel hub, can avoid artificial origin to causeFlase drop or undetected, can reduce maintenance personnel's labour intensity, improve accuracy of detection. But still lack at presentFew special device.
Summary of the invention
In order to address the above problem, the object of the present invention is to provide the integrated harmless inspection of a kind of airplane wheel wheel hubExamining system.
In order to achieve the above object, the integrated nondestructive detection system of airplane wheel wheel hub provided by the invention comprises:Base, two cleaning assemblies, multiple cleaning shower nozzle, two heating components, two fans, four laterally slidingRail, two the first leading screws, two the first servomotors, fixation kit, two supporting seats, drive support groupPart, the first stepper motor, driving hitch bar, mobile working platform, the second servomotor, movable supportArm, the first flange, movable support arm connector, fixed support arm, detection arm fixed support, two detectionsArm tumbler, the second stepper motor, two the 3rd stepper motors, two rotation detection arm, two probes are admittedlyLocking assembly, linear electric motors, the second leading screw, horizontal slide rail, distributed electric controling assembly and two direct currentsMachine; Wherein, base is horizontally disposed with; Article four, horizontal slide rail is divided into two groups, two horizontal slide rail edges in every groupThe fore-and-aft direction standoff distance of base is arranged on the front or rear portion in the left side surface of base; Article two, between horizontal slide railFirst leading screw that be arranged in parallel, one end relative on two the first leading screws is supported by a supporting seat respectively,The other end that is positioned at outside is connected with the output shaft of first servomotor respectively; Every group of horizontal slide rail and oneA cleaning assembly is installed on root the first leading screw, and therefore cleaning assembly can be under the driving of the first servomotorMove along horizontal slide rail by the first leading screw; The medial surface edge of each cleaning assembly is provided with multiple and cleansThe cleaning shower nozzle that hydraulic coupling liquid-supplying system is connected, is positioned at the position installation heating component that cleans shower nozzle inner side, addsProvided with fan between hot assembly and cleaning assembly medial surface, and fan is by the direct current being arranged on cleaning assemblyMachine drives; Linear electric motors and laterally slide rail are arranged in the surface of base along the left and right directions standoff distance of baseBetween position; Mobile working platform is arranged on linear electric motors and laterally on slide rail, therefore can be at linear electric motorsDrive the horizontal slide rail in lower edge to move, and the anterior face of mobile working platform is formed with along base fore-and-aft directionArticle two, chute; Article two, the second leading screw, the front end of the second leading screw and the second servomotor be arranged in parallel between chuteOutput shaft be connected, rear end connects movable support arm connector; The lower end of movable support arm is arranged on two cunningsIn groove, and the rear end of bottom and movable support arm connector joins, therefore can be at the second servomotorUnder driving, move along chute; The first flange is arranged on the upper end trailing flank of movable support arm; Fixed support armLower end be fixed on the surperficial rear portion of mobile working platform, and with movable support arm before and after be oppositely arranged; GuThe middle part of locking assembly is arranged on the upper end of fixed support arm, and front end is second flange relative with the first flange,Rear end is hitch bar; Drive the lower end of supporting component to be fixed on right side, susceptor surface rear portion; The first stepping electricityMachine is arranged on and drives the upper end of supporting component, and its output shaft arranges forward, and on output shaft, be connected with canThe driving hitch bar combining with hitch bar; The support bracket fastened lower end of detection arm is fixed in susceptor surfaceBe positioned at the position on linear electric motors and horizontal slide rail right side; The rear end of two detection arm tumblers is hinged on respectively inspectionOn the front and back sides of the support bracket fastened upper end of test arm; The second stepper motor is arranged on the support bracket fastened upper end of detection armMiddle part, and the rear end of its output shaft and two detection arm tumblers is hinged, and therefore can drive detection armThe front portion of tumbler swings up and down in vertical plane; The front end of each detection arm tumbler is installed the 3rd stepEnter motor; The rear end of two rotation detection arm is connected with the output shaft of two the 3rd stepper motors respectively, revolvesThe front portion that turns detection arm can swing under the driving of the 3rd stepper motor in horizontal plane; Each rotationThe front end of detection arm is installed a probe fixation kit; Distributed electric controling assembly simultaneously with heating component,Fan, direct current generator, the first servomotor, linear electric motors, the second servomotor, the first stepper motor,The second stepper motor, the 3rd stepper motor electrical connection.
The described integrated nondestructive detection system of airplane wheel wheel hub also comprises and is arranged on the 3rd stepper motor output shaftOn pressure sensor and be arranged on the wheel speed sensors on the first stepping motor output shaft, and pressure sensingDevice is all connected with distributed electrical control electrical component with wheel speed sensors.
The lateral edge position of facing mutually on two described probe fixation kits is provided with multiple for fixing harmlessThe threaded fastener of detection probe, is also provided with at least one coupling liquid spray hole on this side, end face is provided withA coupling liquid hand-hole being connected with coupling liquid spray hole, and coupling liquid hand-hole is by pipeline and couplingClosing hydraulic coupling liquid-supplying system is connected.
Described distributed electric controling assembly top is provided with graphic control panel, and bottom is for controlling regulator cubicle.
The described integrated nondestructive detection system of airplane wheel wheel hub also comprises that two are arranged on respectively two supporting seatsThe limit switch of medial surface edge, and limit switch is connected with distributed electrical control electrical component, usesIn the extreme position that limits cleaning assembly.
The integrated nondestructive detection system of airplane wheel wheel hub provided by the invention can improve detection efficiency greatly, adoptsAutomatically nondestructiving detecting means detects the internal injury of aircraft wheel hub, can avoid flase drop that artificial origin causes orUndetected, can reduce maintenance personnel's labour intensity, improve accuracy of detection; Native system can be preserved and rememberThe testing result of record wheel hub, can significantly reduce maintenance cost by analyzing, and promotes flight safety level.
Brief description of the drawings
Fig. 1 is that the integrated nondestructive detection system part-structure of airplane wheel wheel hub provided by the invention use state is verticalBody figure.
Fig. 2 is that the integrated nondestructive detection system part-structure of airplane wheel wheel hub provided by the invention axle is surveyed view.
Fig. 3 is distributed electrical control group in the integrated nondestructive detection system of airplane wheel wheel hub provided by the inventionPart structural representation.
Fig. 4 is the fixation kit structure of popping one's head in the integrated nondestructive detection system of airplane wheel wheel hub provided by the inventionSchematic diagram.
Fig. 5 be in the integrated nondestructive detection system of airplane wheel wheel hub provided by the invention mobile working platform andUpper-part structural representation.
Fig. 6 is cleaning assembly structural representation in the integrated nondestructive detection system of airplane wheel wheel hub provided by the inventionFigure.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, airplane wheel wheel hub original position provided by the invention be can't harm to inspection automaticallyExamining system is elaborated.
As shown in Fig. 1-Fig. 6, the automatic nondestructive detection system of airplane wheel wheel hub original position provided by the invention comprises:Base 1, two cleaning assemblies 2, multiple cleaning shower nozzle 3, two heating components 4, two fans 5, fourLaterally slide rail 6, two pieces the first leading screw 7, two the first servomotors 8, fixation kit 9, two supporting seats10, drive supporting component 12, the first stepper motor 13, drive hitch bar 15, mobile working platform 16,The second servomotor 17, movable support arm 18, the first flange 19, movable support arm connector 20, fixingSupport arm 21, detection arm fixed support 23, two detection arm tumblers 24, the second stepper motor 25, twoIndividual the 3rd stepper motor 26, two rotation detection arm 27, two probe fixation kits 28, linear electric motors 29,The second leading screw 30, horizontal slide rail 36, distributed electric controling assembly 40 and two direct current generators 43; Wherein,Base 1 is horizontally disposed with; Article four, horizontal slide rail 6 is divided into two groups, and two horizontal slide rails 6 in every group are along base 1Fore-and-aft direction standoff distance be arranged on portion surface before or after the left side of base 1; Article two, between horizontal slide rail 6Relative one end be arranged on 7, two the first leading screws 7 of first leading screw in parallel respectively by a supporting seat 10Support, the other end that is positioned at outside is connected with the output shaft of first servomotor 8 respectively; Every group horizontalOn slide rail 6 and first leading screw 7, a cleaning assembly 2 is installed, therefore cleaning assembly 2 can be watched firstTake under the driving of motor 8 by the first leading screw 7 and move along horizontal slide rails 6; The inner side of each cleaning assembly 2Face edge is provided with multiple cleaning shower nozzles 3 that are connected with cleaning fluid pressure liquid-supplying system, is positioned at and cleans shower nozzle 3Heating component 4 is installed at the position of side, provided with fan 5 between heating component 4 and cleaning assembly 2 medial surfaces, andFan 5 is driven by the direct current generator 43 being arranged on cleaning assembly 2; Linear electric motors 29 and laterally slide rail 36Be arranged on the surperficial middle part of base 1 along the left and right directions standoff distance of base 1; Mobile working platform 16Be arranged on linear electric motors 29 and horizontal slide rail 36, therefore can be along horizontal under the driving of linear electric motors 29Slide rail 36 moves, and the anterior face of mobile working platform 16 is formed with two along base 1 fore-and-aft directionChute 33; Article two, the front end and second of the second leading screw 30, the second leading screws 30 of be arrangeding in parallel between chute 33 is watchedThe output shaft that takes motor 17 is connected, and rear end connects movable support arm connector 20; Under movable support arm 18End is arranged in two chutes 33, and the rear end of bottom and movable support arm connector 20 joins, thereforeCan under the driving of the second servomotor 17, move along chute 33; The first flange 19 is arranged on movable supportOn the upper end trailing flank of arm 18; The lower end of fixed support arm 21 is fixed on behind the surface of mobile working platform 16Portion, and be oppositely arranged with movable support arm 18 front and back; The middle part of fixation kit 9 is arranged on fixed support arm21 upper end, front end is second flange 37 relative with the first flange 19, rear end is hitch bar 22; DriveThe lower end of moving supporting component 12 is fixed on right side, the surperficial rear portion of base 1; The first stepper motor 13 is arranged on and drivesThe upper end of moving supporting component 12, its output shaft 14 arranges forward, and on output shaft 14, be connected with can be withThe driving hitch bar 15 that hitch bar 22 combines; The lower end of detection arm fixed support 23 is fixed on baseOn 1 surface, be positioned at the position on linear electric motors 29 and horizontal slide rail 36 right sides; Two detection arm tumblers 24Rear end is hinged on respectively on the upper end front and back sides of detection arm fixed support 23; The second stepper motor 25 is installedIn the upper center of detection arm fixed support 23, and its output shaft and two detection arm tumblers 24 afterEnd is hinged, and therefore can drive the front portion of detection arm tumbler 24 to swing up and down in vertical plane; Each inspectionThe front end of test arm tumbler 24 is installed the 3rd stepper motor 26; The rear end of two rotation detection arm 27 is dividedBe not connected with the output shaft of two the 3rd stepper motors 26, the front portion of rotation detection arm 27 can be the 3rdUnder the driving of stepper motor 26, in horizontal plane, swing; The front end of each rotation detection arm 27 installs oneIndividual probe fixation kit 28; Distributed 40 whiles and heating component 4, fan 5, direct current of electric controling assemblyMotor 43, the first servomotor 8, linear electric motors 29, the second servomotor 17, the first stepper motor 13,The second stepper motor 25, the 3rd stepper motor 26 are electrically connected.
The described integrated nondestructive detection system of airplane wheel wheel hub also comprises that being arranged on the 3rd stepper motor 26 exportsPressure sensor on axle 46 and be arranged on the wheel speed sensors 47 on the first stepper motor 13 output shafts 14,And pressure sensor 46 and wheel speed sensors 47 are all electrically connected with distributed electric controling assembly 40.
The lateral edge position of facing mutually on two described probe fixation kits 28 is provided with multiple for fixing nothingThe threaded fastener 43 that damages detection probe, is also provided with at least one coupling liquid spray hole 44, end face on this sideBe provided with a coupling liquid hand-hole 45 being connected with coupling liquid spray hole 44, and coupling liquid hand-hole45 are connected with coupling liquid pressure liquid-supplying system by pipeline. In addition, non-destructive control probe can select such asThe ultrasonic probe of Olympus company or GE company.
Described distributed electric controling assembly 40 tops are provided with graphic control panel 42, and bottom is electric for controllingCabinet. Graphic control panel 42 can be selected according to demand, the NB10W of for example Omron Corp.
The described integrated nondestructive detection system of airplane wheel wheel hub also comprises that two are arranged on respectively two supporting seatsThe limit switch 11 of 10 medial surface edges, and limit switch 11 and distributed electric controling assembly 40Electrical connection, for limiting the extreme position of cleaning assembly 2.
Now automatic airplane wheel wheel hub original position provided by the invention nondestructive detection system using method is set forth asUnder:
First, start and operate distributed electric controling assembly 40 by testing staff, in distributed electrical controlUnder the control of assembly 40, utilize linear electric motors 29 that mobile working platform 16 is moved to base 1 left side, itAfter airplane wheel wheel hub 31 1 sides to be detected are arranged on the second flange 37; Then utilize second servoIt is fixing that motor 17 drives movable support arm 18 to shift to by the second leading screw 30 and movable support arm connector 20Support arm 21, until utilize the first flange 19 that airplane wheel wheel hub 31 is clamped;
The second, under the control of distributed electric controling assembly 40, utilize linear electric motors 29 by mobile workingPlatform 16 moves between two cleaning assemblies 2 and stops; Then control two the first servomotors 8 respectivelyDrive two cleaning assemblies to base 1 third side to movement, until two limit switches 11 provide signal, stopOnly mobile;
The 3rd, under the control of distributed electric controling assembly 40, make from cleaning fluid pressure liquid-supplying systemCleaning fluid outwards sprays from multiple cleaning shower nozzles 3, airplane wheel wheel hub 31 is cleaned starting; CleanAfter completing, heating component 4 is heated up, utilize direct current generator 43 drive fan 5 to work simultaneously, with by aircraftWheel hub 31 surfaces dry up;
The 4th, under the control of distributed electric controling assembly 40, utilize two the first servomotors 8 respectivelyDrive two cleaning assemblies 2 mobile in the other direction, then utilize linear electric motors 29 that mobile working platform 16 is movedMove the region to be detected at horizontal slide rail 36 right-hand member positions, until hitch bar 22 and driving hitch bar 15Alignment, is linked together hitch bar 22 and driving hitch bar 15 by testing staff afterwards;
The 5th, under the control of distributed electric controling assembly 40, utilize the second stepper motor 25 by twoThe front end of detection arm tumbler 24 rotates to the axis height of airplane wheel wheel hub 31; Utilize afterwards twoTwo rotation detection arm 27 are turned to the position that is applicable to detection by three stepper motors 26, in this process, needsThe signal of monitor force sensor 46, to ensure the stable of Non-Destructive Testing measuring process;
Six,, under the control of distributed electric controling assembly 40, utilize the first stepper motor 13 by connectionShaft device 22 and driving hitch bar 15 drive airplane wheel wheel hub 31 to rotate, and utilize wheel speed sensingDevice 47 is monitored the rotary speed of airplane wheel wheel hub 31, to ensure the effective of Non-Destructive Testing measurement result; SoAfter will offer coupling liquid spray hole through coupling liquid hand-hole 45 from the coupling liquid of coupling hydraulic coupling liquid-supplying system44 are also outwards ejected on the side of airplane wheel wheel hub 31;
Seven, spray evenly until coupling liquid after, stop the first stepping electricity on the side of airplane wheel wheel hub 31The rotation of machine 13, then utilizes threaded fastener 43 that non-destructive control probe is fixed on to probe fixation kit 28,Again start the first stepper motor 13, utilize non-destructive control probe to detect airplane wheel wheel hub 31 simultaneously,And sending detected image to distributed electric controling assembly 40, distributed electric controling assembly 40 is through processingAfter above-mentioned image is shown on graphic control panel 42; When testing staff sends out on graphic control panel 42When crackle appears in existing airplane wheel wheel hub 31 somewheres, suspend the first stepper motor 13, and mark in cracksPosition, then proceeds to detect.
Eight,, when completing after detection, need to first disconnect hitch bar 22 and drive between hitch bar 15Connect, then move laterally rotation detection arm 27, determine whether once clean again according to civil aviaton's regulationProgram, finally moves to mobile working platform 16 left side of base 1, finally takes off aircraft by testing staffWheel hub 31.
It is emphasized that embodiment of the present invention is illustrative, instead of determinate, thereforeThe present invention is not limited to the embodiment described in detailed description of the invention. Situation about not departing from the scope of the present inventionUnder, can carry out various improvement or replacement to it. Especially, only otherwise have structural conflict, each realityThe feature of executing in example all can mutually combine, or by those skilled in the art according to technical scheme of the present inventionAnd other embodiments of drawing of other these similar principles, belong to equally the scope of protection of the invention.
Claims (5)
1. the integrated nondestructive detection system of airplane wheel wheel hub, is characterized in that: described airplane wheel wheelThe integrated nondestructive detection system of hub comprises: base (1), two cleaning assemblies (2), multiple cleaning shower nozzle (3),Two heating components (4), two fans (5), four horizontal slide rails (6), two the first leading screws (7),Two the first servomotors (8), fixation kit (9), two supporting seats (10), drive supporting component (12),The first stepper motor (13), driving hitch bar (15), mobile working platform (16), the second servomotor(17), movable support arm (18), the first flange (19), movable support arm connector (20), fixing propping upBrace (21), detection arm fixed support (23), two detection arm tumblers (24), the second stepper motor (25),Two the 3rd stepper motors (26), two rotation detection arm (27), two probe fixation kits (28), straightLine motor (29), the second leading screw (30), laterally slide rail (36), distributed electric controling assembly (40) andTwo direct current generators (43); Wherein, base (1) is horizontally disposed with; Article four, horizontal slide rail (6) is divided into two groups,Two horizontal slide rails (6) in every group are arranged on base (1) along the fore-and-aft direction standoff distance of base (1)Left side before or after portion surface; Article two, first leading screw (7) that be arranged in parallel between horizontal slide rail (6), twoThe upper relative one end of root the first leading screw (7) is supported by a supporting seat (10) respectively, is positioned at another of outsideEnd is connected with the output shaft of first servomotor (8) respectively; Every group of horizontal slide rail (6) and oneThe upper cleaning assembly (2) of installing of one leading screw (7), therefore cleaning assembly (2) can be at the first servo electricityMobile along horizontal slide rail (6) by the first leading screw (7) under the driving of machine (8); Each cleaning assembly (2)Medial surface edge multiple cleaning shower nozzles (3) that are connected with cleaning fluid pressure liquid-supplying system are installed, be positioned at clearlyWash the position of shower nozzle (3) inner side heating component (4) is installed, in heating component (4) and cleaning assembly (2)Provided with fan between side (5), and fan (5) is by the direct current generator (43) being arranged on cleaning assembly (2)Drive; Linear electric motors (29) and laterally slide rail (36) arrange along the left and right directions standoff distance of base (1)In the surperficial middle part of base (1); Mobile working platform (16) is arranged on linear electric motors (29) and horizontal strokeUpper to slide rail (36), therefore can be mobile along horizontal slide rail (36) under the driving of linear electric motors (29),And the anterior face of mobile working platform (16) is formed with two chutes (33) along base (1) fore-and-aft direction;Article two, the second leading screw (30) that be arranged in parallel between chute (33), the front end of the second leading screw (30) and second is watchedThe output shaft that takes motor (17) is connected, and rear end connects movable support arm connector (20); Movable support arm (18)Lower end be arranged in two chutes (33), and the rear end of bottom and movable support arm connector (20)Join, therefore can be mobile along chute (33) under the driving of the second servomotor (17); The first flange(19) be arranged on the upper end trailing flank of movable support arm (18); The lower end of fixed support arm (21) is solidFix on the surperficial rear portion of mobile working platform (16), and be oppositely arranged with movable support arm (18) front and back;The middle part of fixation kit (9) is arranged on the upper end of fixed support arm (21), and front end is and the first flange (19)Relative the second flange (37), rear end is hitch bar (22); Drive the lower end of supporting component (12) solidFix on right side, the surperficial rear portion of base (1); The first stepper motor (13) is arranged on and drives supporting component (12)Upper end, its output shaft (14) arranges forward, and is connected with and can fills with shaft coupling on output shaft (14)Put the driving hitch bar (15) that (22) combine; The lower end of detection arm fixed support (23) is fixed on the endOn seat (1) surface, be positioned at the position on linear electric motors (29) and horizontal slide rail (36) right side; Two detection armThe rear end of tumbler (24) is hinged on respectively on the upper end front and back sides of detection arm fixed support (23); TheTwo stepping motor (25) is arranged on the upper center of detection arm fixed support (23), and its output shaft withThe rear end of two detection arm tumblers (24) is hinged, and therefore can drive detection arm tumbler (24)Front portion swings up and down in vertical plane; The front end of each detection arm tumbler (24) is installed the 3rd steppingMotor (26); The rear end of two rotation detection arm (27) defeated with two the 3rd stepper motors (26) respectivelyShaft is connected, the front portion of rotation detection arm (27) can be under the driving of the 3rd stepper motor (26)In horizontal plane, swing; The front end of each rotation detection arm (27) is installed a probe fixation kit (28);Distributed electric controling assembly (40) simultaneously with heating component (4), fan (5), direct current generator (43),The first servomotor (8), linear electric motors (29), the second servomotor (17), the first stepper motor (13),The second stepper motor (25), the 3rd stepper motor (26) electrical connection.
2. the integrated nondestructive detection system of airplane wheel wheel hub according to claim 1, is characterized in that:The described integrated nondestructive detection system of airplane wheel wheel hub also comprises that being arranged on the 3rd stepper motor (26) exportsPressure sensor (46) on axle and be arranged on the wheel speed on the first stepper motor (13) output shaft (14)Sensor (47), and pressure sensor (46) and wheel speed sensors (47) all with distributed electrical controlAssembly (40) electrical connection.
3. the integrated nondestructive detection system of airplane wheel wheel hub according to claim 1, is characterized in that:The lateral edge position of facing mutually on described two probe fixation kits (28) is provided with multiple for fixing nothingThe threaded fastener (43) that damages detection probe, is also provided with at least one coupling liquid spray hole (44) on this side,End face is provided with a coupling liquid hand-hole (45) being connected with coupling liquid spray hole (44), and couplingLiquid hand-hole (45) is connected with coupling liquid pressure liquid-supplying system by pipeline.
4. the integrated nondestructive detection system of airplane wheel wheel hub according to claim 1, is characterized in that:Described distributed electric controling assembly (40) top is provided with graphic control panel (42), and bottom is for controlling electricityGas holder.
5. the integrated nondestructive detection system of airplane wheel wheel hub according to claim 1, is characterized in that:The described integrated nondestructive detection system of airplane wheel wheel hub also comprises that two are arranged on respectively two supporting seats (10)The limit switch (11) of medial surface edge, and limit switch (11) and distributed electric controling assembly(40) electrical connection, for limiting the extreme position of cleaning assembly (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510757779.6A CN105606704B (en) | 2015-11-09 | 2015-11-09 | A kind of airplane wheel wheel hub integrates nondestructive detection system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510757779.6A CN105606704B (en) | 2015-11-09 | 2015-11-09 | A kind of airplane wheel wheel hub integrates nondestructive detection system |
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| CN105606704A true CN105606704A (en) | 2016-05-25 |
| CN105606704B CN105606704B (en) | 2018-03-20 |
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| CN201510757779.6A Expired - Fee Related CN105606704B (en) | 2015-11-09 | 2015-11-09 | A kind of airplane wheel wheel hub integrates nondestructive detection system |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108956771A (en) * | 2018-07-07 | 2018-12-07 | 南京理工大学 | Special vehicle transmission shaft damage detection system based on supersonic guide-wave |
| CN109253915A (en) * | 2018-09-25 | 2019-01-22 | 南京通用化工设备技术研究院 | A kind of pressure vessel detection device |
| CN112034042A (en) * | 2020-08-25 | 2020-12-04 | 武汉理工大学 | Mooring chain working state detection device and detection method |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012173117A (en) * | 2011-02-21 | 2012-09-10 | Nsk Ltd | Defect inspection method and defect inspection device |
| CN102768028A (en) * | 2012-06-04 | 2012-11-07 | 天津大学 | Method and device for online in-situ measurement with single joint arm |
| CN103389207A (en) * | 2012-05-09 | 2013-11-13 | 株式会社捷太格特 | Method of inspecting wheel hub unit |
| CN104535341A (en) * | 2015-01-23 | 2015-04-22 | 山东交通学院 | Multifunctional wheel tester |
| CN205103213U (en) * | 2015-11-09 | 2016-03-23 | 中国民航大学 | Integrated nondestructive test device of aircraft wheel wheel hub |
-
2015
- 2015-11-09 CN CN201510757779.6A patent/CN105606704B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012173117A (en) * | 2011-02-21 | 2012-09-10 | Nsk Ltd | Defect inspection method and defect inspection device |
| CN103389207A (en) * | 2012-05-09 | 2013-11-13 | 株式会社捷太格特 | Method of inspecting wheel hub unit |
| CN102768028A (en) * | 2012-06-04 | 2012-11-07 | 天津大学 | Method and device for online in-situ measurement with single joint arm |
| CN104535341A (en) * | 2015-01-23 | 2015-04-22 | 山东交通学院 | Multifunctional wheel tester |
| CN205103213U (en) * | 2015-11-09 | 2016-03-23 | 中国民航大学 | Integrated nondestructive test device of aircraft wheel wheel hub |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108956771A (en) * | 2018-07-07 | 2018-12-07 | 南京理工大学 | Special vehicle transmission shaft damage detection system based on supersonic guide-wave |
| CN109253915A (en) * | 2018-09-25 | 2019-01-22 | 南京通用化工设备技术研究院 | A kind of pressure vessel detection device |
| CN109253915B (en) * | 2018-09-25 | 2023-08-11 | 嘉兴市安得特种设备科技有限公司 | Detection device for pressure vessel |
| CN112034042A (en) * | 2020-08-25 | 2020-12-04 | 武汉理工大学 | Mooring chain working state detection device and detection method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105606704B (en) | 2018-03-20 |
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