CN205193021U - Aircraft leading edge detection device - Google Patents
Aircraft leading edge detection device Download PDFInfo
- Publication number
- CN205193021U CN205193021U CN201520999419.2U CN201520999419U CN205193021U CN 205193021 U CN205193021 U CN 205193021U CN 201520999419 U CN201520999419 U CN 201520999419U CN 205193021 U CN205193021 U CN 205193021U
- Authority
- CN
- China
- Prior art keywords
- slide
- leading edge
- aircraft leading
- slide rail
- underframe
- 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.)
- Withdrawn - After Issue
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Abstract
The utility model discloses an aircraft leading edge detection device, including laying at two subaerial slide rails, sliding fit detects the car on the slide rail, corresponds the centre gripping car that sliding fit is used for centre gripping aircraft leading edge on the slide rail of detection car both sides, detect the car and include the chassis, chassis bottom four corners be equipped with with slide rail complex track gyro wheel, the chassis top surface sets up Y to the slide, Y is equipped with the grudging post on to the slide, the grudging post top is equipped with X to the slide, X is equipped with Z on to the slide to the cursor slide, Z be equipped with on to the cursor slide can along Y to gliding slider, install the carousel on the slider, connect fixed probe on the carousel and put up. The utility model discloses the centre gripping and the detection achievement of the aircraft leading edge of different length, opening size, course width and leading edge shape can be satisfied, the centre gripping height of aircraft leading edge can be adjusted wantonly, the shift position, turned angle has solved the narrow unable comprehensive problem that detects in aircraft leading edge circular arc district space, realizes detecting the comprehensive, accurate of aircraft leading edge, is favorable to ensureing safety.
Description
Technical field
The utility model relates to a kind of checkout equipment, particularly relates to a kind of pick-up unit for aircraft leading edge ultrasound examination.
Background technology
At present, the ultrasound examination of aircraft leading edge generally all adopts correlation method, in testing process, must ensure that two relative positions of popping one's head in are correct, ensure the stable of coupling water layer.Simultaneously in order to meet the detection of each position of aircraft leading edge, need to design a kind of aircraft leading edge pick-up unit to adapt to the ultrasound examination of the aircraft leading edge of shape and structure complexity, solve aircraft leading edge circular arc district because of narrow space cannot the problem of complete detection.
Utility model content
The purpose of this utility model is just to provide a kind of aircraft leading edge pick-up unit, can solve above-mentioned the deficiencies in the prior art part completely.
The purpose of this utility model is realized by following technical proposals:
A kind of aircraft leading edge pick-up unit, comprise and be laid on ground two slide rails, slide rail is slidably matched inspection vehicle, the corresponding clamping trolley be slidably matched for clamping aircraft leading edge on the slide rail of inspection vehicle both sides; Described inspection vehicle comprises underframe, bottom underframe, corner is provided with the track roller coordinated with slide rail, underframe end face arranges Y-direction slide, Y-direction slide is provided with stand, stand top is provided with X to slide plate, and X is provided with Z-direction cursor slide to slide plate, and Z-direction cursor slide is provided with the slide block that can slide along Y-direction, slide block installs rotating disk, rotating disk is connected and fixed probe holder.
Further, described underframe end face is provided with Y-direction slide rail, Y-direction slide is slidably fitted on Y-direction slide rail, the ball-screw of band handwheel is utilized to control the movement of Y-direction slide on Y-direction slide rail, X to slide plate by X-axis motor drive realize X to slip, Z-direction cursor slide is driven the slip realizing Z-direction by Z axis motor, slide block is driven by sliding motor and realizes sliding.
Further, described clamping trolley comprises underframe, bottom underframe, corner is provided with the track roller coordinated with slide rail, underframe end face arranges the base that energy Y-direction is slided, base connects top board by vertical lifting mechanism, by rotating mechanism connecting cross arm on top board, transverse arm is slidably matched 2 clamping limbs, and transverse arm and clamping limb are mutually vertical.Clamping limb is scalable to be regulated.
Further, described vertical lifting mechanism comprises the column be vertically connected on base, and worm-and-wheel gear installed by column, and worm gear is connected with control hand wheel, and worm screw top is connected and fixed top board.
Further, described rotating mechanism is worm type of reduction gearing, and worm gear is connected with control hand wheel, worm screw overhanging end connecting cross arm.Index dial is installed at worm gear center, instruction angle.
Further, described two slide rails, wherein a slide rail end face is provided with tapered protrusion, and another slide rail end face is surface level.
Further, be equipped with the ground rollers be fastened on underframe outside the track roller bottom described inspection vehicle and clamping trolley, the external diameter of ground rollers is greater than track roller.
Further, the underframe between track roller and ground rollers is provided with lifting body.
Further, described probe holder is plane domain probe holder, and this plane domain probe holder comprises U-shaped support body, and the bottom of U-shaped support body is fastened on rotating disk, and openend correspondence is installed, lower probe and water injector.
Further, described probe holder is upper probe holder, and in stand, corresponding Z-direction cursor slide is provided with and can carries out to Y-direction the lower probe holder that regulates at X, and the end correspondence of upper and lower probe holder is installed, lower probe, and upper probe is rotatably mounted on probe holder end, lower probe is rotatably mounted on lower probe end.
The beneficial effects of the utility model are: structure is simple, reasonable in design, clamping and the testing of the aircraft leading edge of different length, openings of sizes, course width and leading edge shape can be met, and its clamped height of aircraft leading edge can be adjusted arbitrarily, rotational angle, solving aircraft leading edge circular arc district narrow space cannot the problem of complete detection, thus realize to aircraft leading edge comprehensive, accurately detect, be conducive to guaranteeing safety.
Accompanying drawing explanation
Fig. 1 is front elevation of the present utility model;
Fig. 2 is vertical view of the present utility model;
Fig. 3 is the perspective view of inspection vehicle in the utility model embodiment one;
Fig. 4 is the front elevation of inspection vehicle in the utility model embodiment one;
Fig. 5 is the side view of inspection vehicle in the utility model embodiment one;
Fig. 6 is the vertical view of inspection vehicle in the utility model embodiment one;
Fig. 7 is the using state figure of inspection vehicle in the utility model embodiment one;
Fig. 8 is the perspective view of clamping trolley in the utility model embodiment one;
Fig. 9 is the front elevation of clamping trolley in the utility model embodiment one;
Figure 10 is the side view of clamping trolley in the utility model embodiment one;
Figure 11 is the vertical view of clamping trolley in the utility model embodiment one;
Figure 12 is the track roller of clamping trolley and the fit structure schematic diagram of slide rail;
Figure 13 is the perspective view of inspection vehicle in the utility model embodiment two;
Figure 14 is the partial enlarged drawing at A place in Figure 13;
Figure 15 is the using state figure of inspection vehicle in the utility model embodiment two;
Figure 16 is the syndeton schematic diagram of popping one's head in up and down;
Figure 17 is B-B cross-sectional view in Figure 16.
Embodiment
Below in conjunction with specific embodiments and the drawings, the utility model is further described.
Embodiment one
As shown in Figures 1 to 12, a kind of aircraft leading edge pick-up unit, comprise and be laid on ground two slide rails 1, slide rail 1 is slidably matched inspection vehicle 2, the corresponding clamping trolley 3 be slidably matched for clamping aircraft leading edge on the slide rail 1 of inspection vehicle 2 both sides.
See Fig. 3 to Fig. 7, described inspection vehicle 2 comprises underframe 2-1, bottom underframe 2-1, corner is provided with the track roller 2-2 coordinated with slide rail 1, underframe 2-1 end face arranges Y-direction slide 2-3, and Y-direction slide 2-3 is provided with stand 2-4, and stand 2-4 top is provided with X to slide plate 2-5, X is provided with Z-direction cursor slide 2-6 to slide plate 2-5, Z-direction cursor slide 2-6 is provided with the slide block 2-7 that can slide along Y-direction, slide block 2-7 installs rotating disk 2-8, rotating disk 2-8 is connected and fixed probe holder.Described probe holder is plane domain probe holder, this plane domain probe holder comprises U-shaped support body 2-9, the bottom of U-shaped support body 2-9 is fastened on rotating disk 2-8, this rotating disk 2-8 can within the scope of 0-60 ° any rotational positioning, the openend correspondence of U-shaped support body 2-9 is installed, lower probe 2-10,2-11.
Described underframe 2-1 end face is provided with Y-direction slide rail 2-12, Y-direction slide 2-3 is slidably fitted on Y-direction slide rail 2-12, the ball-screw 2-13 of band handwheel is utilized to control the movement of Y-direction slide 2-3 on Y-direction slide rail 2-12, X to slide plate 2-5 by X-axis motor 2-14 drive realize X to slip, Z-direction cursor slide 2-6 is driven the slip realizing Z-direction by Z axis motor 2-15, slide block 2-7 is driven by sliding motor 2-16 and realizes sliding.
See Fig. 8 to Figure 12, described clamping trolley 3 comprises underframe 3-1, bottom underframe 3-1, corner is provided with the track roller 3-2 coordinated with slide rail 1, described underframe 3-1 end face arranges Y-direction slide rail 3-5 and the ball-screw 3-6 parallel with Y-direction slide rail 3-5, Y-direction slide rail 3-5 is slidably matched base 3-7, base 7 bottom surface is connected with the nut of ball-screw 3-6, and the screw rod end of ball-screw 3-6 arranges control hand wheel 3-8.
Base 3-7 vertically arranges column 3-9, column 3-9 installs worm-and-wheel gear 3-10, worm gear is connected with control hand wheel, worm screw top is connected and fixed top board 3-11, by worm type of reduction gearing 3-12 connecting cross arm 3-13 on top board 3-11, concretely, worm gear is connected with control hand wheel, worm screw overhanging end connecting cross arm 3-13, thus realize transverse arm 3-13 can free adjustment within the scope of 0 ~ 360 °.Transverse arm 3-13 is slidably matched 2 clamping limb 3-14, and transverse arm 3-13 is mutually vertical with clamping limb 3-14.
In order to ensure the accuracy that top board 3-11 is elevated vertically, vertically-guided post 3-15 is set bottom described top board 3-11, on column 3-15, correspondence is provided with guide pin bushing 3-16, and vertically-guided post 3-15 and guide pin bushing 3-16 is slidably matched, and guide pin bushing 3-16 is fixedly mounted on column 3-9.
Described two slide rails 1, wherein slide rail 1 end face is provided with tapered protrusion 1-1, and another slide rail 1 end face is surface level 1-2.Four track rollers 2-2,3-2 of described inspection vehicle 2 and clamping trolley 3 are symmetricly set in its underframe 2-1,3-1 both sides respectively, and wherein the idler wheel surface of track roller 2-2,3-2 of side is provided with V-shaped groove 17 and coordinates with the tapered protrusion 1-1 of slide rail end face, the idler wheel surface of track roller 2-2,3-2 of opposite side is that the level and smooth face of cylinder coordinates with the end face of another slide rail.This structure makes inspection vehicle 2 and clamping trolley 3 have self-locating function, ensures that the center line of inspection vehicle 2 and clamping trolley 3 overlaps with slide rail 1 center line.
Be equipped with ground rollers 2-17,3-3 of being fastened on underframe 2-1,3-1 outside track roller 2-2,3-2 bottom described inspection vehicle 2 and clamping trolley 3, the external diameter of ground rollers 2-17,3-3 is greater than track roller 2-2,3-2.This structure makes inspection vehicle 2 and clamping trolley 3 after pushing slide rail 1, and ground rollers can be utilized to continue to move to and need position, and now, track roller is unsettled, plays the effect of protection track roller.Underframe between track roller and ground rollers is provided with lifting body 4.
In use, according to the length of aircraft leading edge, adjust the distance of 2 clamping trolleys 3 on slide rail 1, utilize lifting body 4 by clamping trolley 3 jack-up, thus latched position, prevent clamping trolley 3 from sliding arbitrarily.Rotating control hand wheel regulates top board 3-11 to suitable height, control hand wheel is utilized to regulate worm type of reduction gearing 3-12, transverse arm 3-13 is made to turn to the angle of needs, regulate the distance between 2 clamping limb 3-14 according to the openings of sizes of aircraft leading edge, aircraft leading edge two ends are gripped by clamping limb 3-14.Then, promote inspection vehicle 2 and move to assigned address on slide rail 1, utilize lifting body 4 by inspection vehicle 2 jack-up latched position.Pop one's head in up and down 2-10,2-11 to the slide block 2-7 on slide plate 2-5, Z-direction cursor slide 2-6 and Z-direction cursor slide 2-6, thus are adjusted to the position of needs by adjustment rotating disk 2-8, Y-direction slide 2-3, X, and pop one's head in up and down 2-10,2-11 carry out ultrasound examination to aircraft leading edge.
The pick-up unit of the present embodiment is adapted to the ultrasound examination of the straight length portion to aircraft leading edge both sides, and working range is large, and efficiency is high.
Embodiment two
See Figure 13 to Figure 15, the difference of the present embodiment and embodiment one is, on the stand 2-4 of inspection vehicle 2, corresponding Z-direction cursor slide 2-6 is provided with and can carries out to Y-direction the lower probe holder 5 that regulates at X.Described rotating disk 2-8 installs probe holder 6.The end correspondence of upper and lower probe holder 6,5 is installed, lower probe 7,8.Described upper and lower probe holder 6,5 is long straight-bar, and the relative position of upper and lower probe holder 6,5 is adjustable, thus adjusts the distance between upper and lower probe 7,8.
See Figure 16 and Figure 17, the probe rotating shaft synchronizing wheel 21 that on described upper probe holder 6, corresponding installation is connected by Timing Belt 20 and synchronous pulley 22, probe rotating shaft synchronizing wheel 21 level is arranged on probe holder 6 bottom, upper probe 7 is arranged in the rotating shaft of probe rotating shaft synchronizing wheel 21, synchronous pulley 22 is driven to rotate by upper probe adjusting screw(rod) 23 by worm gear, and then drive upper probe 7 to rotate, realize the angular setting in the intrados small space of aircraft leading edge arc section.Install worm gear 24 on lower probe holder 5 top, lower probe 8 is arranged on the output revolving shaft of worm gear, is rotated and then drives lower probe 8 to rotate, make upper and lower probe 7,8 relative position correct by lower probe adjusting screw(rod) 25.
The pick-up unit of the present embodiment is adapted to the ultrasound examination to the circular arc segment section in the middle of aircraft leading edge.
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (10)
1. an aircraft leading edge pick-up unit, is characterized in that: comprise and be laid on ground two slide rails, slide rail is slidably matched inspection vehicle, the corresponding clamping trolley be slidably matched for clamping aircraft leading edge on the slide rail of inspection vehicle both sides; Described inspection vehicle comprises underframe, bottom underframe, corner is provided with the track roller coordinated with slide rail, underframe end face arranges Y-direction slide, Y-direction slide is provided with stand, stand top is provided with X to slide plate, and X is provided with Z-direction cursor slide to slide plate, and Z-direction cursor slide is provided with the slide block that can slide along Y-direction, slide block installs rotating disk, rotating disk is connected and fixed probe holder.
2. aircraft leading edge pick-up unit according to claim 1, it is characterized in that: described underframe end face is provided with Y-direction slide rail, Y-direction slide is slidably fitted on Y-direction slide rail, the ball-screw of band handwheel is utilized to control the movement of Y-direction slide on Y-direction slide rail, X to slide plate by X-axis motor drive realize X to slip, Z-direction cursor slide is driven the slip realizing Z-direction by Z axis motor, slide block is driven by sliding motor and realizes sliding.
3. aircraft leading edge pick-up unit according to claim 2, it is characterized in that: described clamping trolley comprises underframe, bottom underframe, corner is provided with the track roller coordinated with slide rail, underframe end face arranges the base that energy Y-direction is slided, base connects top board by vertical lifting mechanism, by rotating mechanism connecting cross arm on top board, transverse arm is slidably matched 2 clamping limbs, and transverse arm and clamping limb are mutually vertical.
4. aircraft leading edge pick-up unit according to claim 3, it is characterized in that: described vertical lifting mechanism comprises the column be vertically connected on base, and worm-and-wheel gear installed by column, and worm gear is connected with control hand wheel, worm screw top is connected and fixed top board.
5. aircraft leading edge pick-up unit according to claim 4, is characterized in that: described rotating mechanism is worm type of reduction gearing, and worm gear is connected with control hand wheel, worm screw overhanging end connecting cross arm.
6. aircraft leading edge pick-up unit according to claim 1, is characterized in that: described two slide rails, and wherein a slide rail end face is provided with tapered protrusion, and another slide rail end face is surface level.
7. aircraft leading edge pick-up unit according to claim 3, is characterized in that: be equipped with the ground rollers be fastened on underframe outside the track roller bottom described inspection vehicle and clamping trolley, the external diameter of ground rollers is greater than track roller.
8. aircraft leading edge pick-up unit according to claim 7, is characterized in that: the underframe between track roller and ground rollers is provided with lifting body.
9. the aircraft leading edge pick-up unit according to any one of claim 1-8, it is characterized in that: described probe holder is plane domain probe holder, this plane domain probe holder comprises U-shaped support body, and the bottom of U-shaped support body is fastened on rotating disk, and openend correspondence is installed, lower probe and water injector.
10. the aircraft leading edge pick-up unit according to any one of claim 1-8, it is characterized in that: described probe holder is upper probe holder, in stand, corresponding Z-direction cursor slide is provided with and can carries out to Y-direction the lower probe holder that regulates at X, the end correspondence of upper and lower probe holder is installed, lower probe, and upper probe is rotatably mounted on probe holder end, lower probe is rotatably mounted on lower probe end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520999419.2U CN205193021U (en) | 2015-12-04 | 2015-12-04 | Aircraft leading edge detection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520999419.2U CN205193021U (en) | 2015-12-04 | 2015-12-04 | Aircraft leading edge detection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205193021U true CN205193021U (en) | 2016-04-27 |
Family
ID=55786000
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520999419.2U Withdrawn - After Issue CN205193021U (en) | 2015-12-04 | 2015-12-04 | Aircraft leading edge detection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205193021U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105467007A (en) * | 2015-12-04 | 2016-04-06 | 四川兴天源材料检测技术有限公司 | Airplane leading edge detection device |
-
2015
- 2015-12-04 CN CN201520999419.2U patent/CN205193021U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105467007A (en) * | 2015-12-04 | 2016-04-06 | 四川兴天源材料检测技术有限公司 | Airplane leading edge detection device |
| CN105467007B (en) * | 2015-12-04 | 2017-11-21 | 四川曜诚无损检测技术有限公司 | Aircraft leading edge detection means |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160704 Address after: 620860 Meishan province Sichuan city Pengshan District No. 209 South Street Patentee after: Sichuan Yao Cheng Nondestructive Testing Technology Co., Ltd. Address before: 620860, No. 31, New South Street, Pengshan County, Meishan, Sichuan Patentee before: Sichuan Xingtianyuan Material Inspection Technology Co.,Ltd. |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20160427 Effective date of abandoning: 20171121 |
|
| AV01 | Patent right actively abandoned |