CN219890958U - Wing resistance to compression detection device is used in unmanned aerial vehicle production - Google Patents
Wing resistance to compression detection device is used in unmanned aerial vehicle production Download PDFInfo
- Publication number
- CN219890958U CN219890958U CN202321003202.2U CN202321003202U CN219890958U CN 219890958 U CN219890958 U CN 219890958U CN 202321003202 U CN202321003202 U CN 202321003202U CN 219890958 U CN219890958 U CN 219890958U
- Authority
- CN
- China
- Prior art keywords
- frame
- wing
- plate
- clamping plate
- tested
- 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
Links
- 238000001514 detection method Methods 0.000 title claims abstract description 24
- 230000006835 compression Effects 0.000 title claims abstract description 17
- 238000007906 compression Methods 0.000 title claims abstract description 17
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 16
- 244000309464 bull Species 0.000 claims description 10
- 238000001125 extrusion Methods 0.000 claims description 8
- 238000010030 laminating Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- TVEXGJYMHHTVKP-UHFFFAOYSA-N 6-oxabicyclo[3.2.1]oct-3-en-7-one Chemical compound C1C2C(=O)OC1C=CC2 TVEXGJYMHHTVKP-UHFFFAOYSA-N 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000000178 monomer Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Landscapes
- Investigation Of Foundation Soil And Reinforcement Of Foundation Soil By Compacting Or Drainage (AREA)
Abstract
The utility model discloses a wing compression-resistant detection device for unmanned aerial vehicle production, wherein a lower clamping plate is fixedly arranged on one side of the inner wall of a frame, a first rotating rod is connected with the inner wall of one side of the upper end of the frame in a threaded manner, the first rotating rod penetrates through one side of the frame to extend to be close to one side of the upper end of the lower clamping plate, an upper clamping plate is connected in a limiting rotation manner, and rubber pads are arranged on the opposite sides of the lower clamping plate and the upper clamping plate, so that the wing compression-resistant detection device has the following advantages: the wing to be tested is placed on the single plate, the root of the wing to be tested is located between the upper clamping plate and the lower clamping plate, a plurality of wings to be tested can be placed by the same operation, the first rotating rod moves downwards in the frame through the threads in the first rotating disc, the wings to be tested can be clamped and fixed simultaneously through the operation, and when the wing to be tested is tested, the position of the sliding block can be adjusted through the rotation of the second rotating disc, so that the wing to be tested can be tested at different positions conveniently.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle wing compression resistance detection, in particular to a wing compression resistance detection device for unmanned aerial vehicle production.
Background
The unmanned aerial vehicle is a common name of unmanned aerial vehicle in fact, can be divided into unmanned fixed wing aircraft, unmanned vertical take-off and landing aircraft and the like from technical angle definition, and compared with a manned aircraft, the unmanned aerial vehicle has the advantages of small size, low manufacturing cost and convenience in use.
The existing unmanned aerial vehicle wing production later, in order to ensure that the produced wing reaches the standard, the compressive detection is needed to be carried out on the wing, but when the wing is actually detected, the wing is not easy to fix due to the unique structure of the wing monomer, so that the wing is usually directly placed on a detection platform for detection, and therefore, the wing can move during detection, so that the detection effect is influenced.
Disclosure of Invention
The utility model aims to solve the technical problems that after the production of the unmanned aerial vehicle wing, the compression-resistant detection is needed for the wing to ensure that the produced wing meets the standards, but when the wing is actually detected, the wing is usually directly placed on a detection platform for detection because the wing single body structure is unique and is not easy to fix, and therefore, when the wing is detected, the wing moves to influence the detection effect, so that the compression-resistant detection device for the wing for the unmanned aerial vehicle production is provided, and the problems are solved.
The technical scheme adopted for solving the technical problems is as follows: an unmanned aerial vehicle production is with wing resistance to compression detection device, it includes: the frame, frame inner wall one side is fixed to be provided with the lower plate, frame upper end one side inner wall threaded connection has first bull stick, first bull stick screw thread runs through frame one side and extends to be close to lower plate upper end one side spacing rotation and be connected with the punch holder, lower plate and punch holder opposite side all are provided with the rubber pad, punch holder both ends upside is all fixed to be provided with the telescopic link, frame upper end one side inner wall spacing sliding connection has the slider, slider bottom one side is fixed to be provided with first hydraulic stem, first hydraulic stem output is fixed to be provided with the stripper plate, slider inner wall threaded connection has the second bull stick, second bull stick one end bearing is connected inside the frame, the frame corresponds slider one side inner wall laminating sliding connection has the guide block, guide block inner wall laminating sliding connection has the guide bar.
As a preferable technical scheme of the utility model, the first rotating rod extends to the outside of the frame and is fixedly provided with a first disc, and a handle structure is arranged on the side, opposite to the first rotating rod, of the first disc.
As a preferable technical scheme of the utility model, one side of the top end of the telescopic rod is fixedly connected with the frame, the bottom end of the guide rod is fixedly connected with the extrusion plate, and one side of the bottom end of the extrusion plate is arc-shaped.
As a preferable technical scheme of the utility model, the other end of the second rotating rod extends to the outside of the frame and is fixedly provided with a second disc, and one side of the second disc opposite to the second rotating rod is provided with a handle structure.
As a preferable technical scheme of the utility model, the wing to be tested is clamped between the upper clamping plate and the lower clamping plate, a single plate is rotationally connected to one side of the frame close to the lower end of the lower clamping plate, a second hydraulic rod is rotationally connected to one side of the bottom end of the single plate, and one end of the second hydraulic rod far away from the single plate is rotationally connected with the frame.
As a preferable technical scheme of the utility model, the single plate is L-shaped, and the upper surface of one end of the single plate and the rubber pad on the lower clamping plate are positioned on the same horizontal plane.
The utility model has the following advantages: the second hydraulic rod is controlled to push the single plate, the upper surface of the single plate is horizontal, the wings to be tested are placed on the single plate, the root of the wings to be tested is located between the upper clamping plate and the lower clamping plate, a plurality of wings to be tested can be placed in the same operation, after the wings to be tested are placed, the first rotating rod moves downwards in the internal threads of the frame through rotating the first disc, the wings to be tested can be clamped and fixed simultaneously through the operation, when the wings to be tested are tested, the position of the sliding block can be adjusted through rotating the second disc, so that the wings to be tested can be tested at different positions conveniently, the first hydraulic rod is controlled to drive the extrusion plate to descend, and the wings to be tested are pressed down simultaneously through the extrusion plate, so that the compression resistance of the wings to be tested can be detected.
Drawings
FIG. 1 is a schematic view of the construction of a preferred embodiment of the present utility model;
FIG. 2 is a schematic side elevational view of a preferred embodiment of the present utility model;
FIG. 3 is a schematic view of a connection structure between a slider and a second rotating rod according to a preferred embodiment of the present utility model.
Reference numerals illustrate: 1. a frame; 2. a lower clamping plate; 3. a first rotating lever; 4. an upper clamping plate; 5. a rubber pad; 6. a telescopic rod; 7. a slide block; 8. a first hydraulic lever; 9. an extrusion plate; 10. a second rotating rod; 11. a guide block; 12. a guide rod; 13. a first disc; 14. a second disc; 15. a wing to be tested; 16. a single board; 17. and a second hydraulic rod.
Detailed Description
The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings. In the description of the present utility model, it should be noted that the directions or positional relationships indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying positive importance.
In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
The utility model is further described below with reference to the accompanying drawings.
Referring to fig. 1-3 in combination, the present utility model provides a wing compression-resistant detection device for unmanned aerial vehicle production, comprising: the frame 1, frame 1 inner wall one side is fixed to be provided with lower plate 2, frame 1 upper end one side inner wall threaded connection has first dwang 3, first dwang 3 screw thread runs through frame 1 one side and extends to be close to lower plate 2 upper end one side spacing rotation and be connected with punch holder 4, lower plate 2 and punch holder 4 opposite side all are provided with rubber pad 5, punch holder 4 both ends upside is all fixed being provided with telescopic link 6, frame 1 upper end one side inner wall spacing sliding connection has slider 7, slider 7 bottom one side is fixed to be provided with first hydraulic stem 8, first hydraulic stem 8 output is fixed to be provided with stripper plate 9, slider 7 inner wall threaded connection has second bull stick 10, inside second bull stick 10 one end bearing connection frame 1, frame 1 corresponds slider 7 one side inner wall laminating sliding connection has guide block 11, guide block 11 inner wall laminating sliding connection has guide bar 12.
As shown in fig. 1, the first rotating rod 3 extends to the outside of the frame 1 and is fixedly provided with a first disc 13, the first rotating rod 3 can be driven to rotate by rotating the first disc 13, a handle structure is arranged on one side, opposite to the first rotating rod 3, of the first disc 13, the first rotating rod 3 can move in the up-and-down direction of threads inside the frame 1, one side of the top end of the telescopic rod 6 is fixedly connected with the frame 1, the bottom end of the guide rod 12 is fixedly connected with the extruding plate 9, the structure is kept stable when the extruding plate 9 moves up and down through the guide rod 12, one side of the bottom end of the extruding plate 9 is arc-shaped, the other end of the second rotating rod 10 extends to the outside of the frame 1 and is fixedly provided with a second disc 14, the second rotating rod 10 can be driven to rotate by rotating the second disc 14, and the opposite side of the second disc 14 and the second rotating rod 10 is provided with a handle structure.
As shown in fig. 2, a wing 15 to be tested is clamped between the upper clamping plate 4 and the lower clamping plate 2, one side of the frame 1, which is close to the lower end of the lower clamping plate 2, is rotatably connected with a single plate 16, one side of the bottom end of the single plate 16 is rotatably connected with a second hydraulic rod 17, one end, which is far away from the single plate 16, of the second hydraulic rod 17 is rotatably connected with the frame 1, the single plate 16 is L-shaped, the upper surface of one end of the single plate 16 and the rubber pad 5 on the lower clamping plate 2 are positioned on the same horizontal plane, and the single plate 16 can be supported or contracted by stretching and retracting the second hydraulic rod 17.
Specifically, when the utility model is used, firstly, the single plate 16 is pushed by controlling the second hydraulic rod 17, the single plate 16 is supported and the upper surface of the single plate 16 is horizontal, then, the to-be-tested wing 15 is placed on the single plate 16, the root of the to-be-tested wing 15 is positioned between the upper clamping plate 4 and the lower clamping plate 2, a plurality of to-be-tested wings 15 can be placed in the same operation, after the placement is finished, the first rotating rod 3 is driven to rotate by rotating the first disc 13, the first rotating rod 3 is enabled to move downwards in the internal thread of the frame 1, the upper clamping plate 4 is driven to move downwards by the first rotating rod 3, the root of the to-be-tested wing 15 is clamped and fixed by the lower clamping plate 2, the above operation can realize the simultaneous clamping and fixing of the plurality of to-be-tested wings 15, when the test is performed, the single plate 16 can be firstly retracted by controlling the second hydraulic rod 17, then, the second rotating disc 14 is driven to rotate, the sliding block 7 is driven to move by the threads of the second rotating rod 10, the position above the to-be-tested wing 15 corresponding to the to-be-tested wing 7 can be controlled, after the adjustment is finished, the extrusion plate 9 is driven to move by controlling the first hydraulic rod 8, the extruding plate 9 is driven to move downwards, the pressing plate 9, and the plurality of to be tested wings 15 are simultaneously pressed, and the to be tested.
The foregoing is merely a preferred embodiment of the present utility model and it should be noted that modifications and adaptations to those skilled in the art may be made without departing from the principles of the present utility model, which are intended to be comprehended within the scope of the present utility model.
Other parts of the present utility model not described in detail are all of the prior art, and are not described in detail herein.
Finally, it should be noted that: the above embodiments are only for illustrating the technical solution of the present utility model, and not for limiting the same; although the utility model has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some or all of the technical features thereof can be replaced by equivalents; such modifications and substitutions do not depart from the spirit of the utility model.
Claims (6)
1. Wing resistance to compression detection device is used in unmanned aerial vehicle production includes: frame (1), its characterized in that, frame (1) inner wall one side is fixed to be provided with lower plate (2), frame (1) upper end one side inner wall threaded connection has first bull stick (3), first bull stick (3) screw thread runs through frame (1) one side and extends to be close to lower plate (2) upper end one side spacing rotation and be connected with punch holder (4), lower plate (2) all are provided with rubber pad (5) with one side opposite to punch holder (4), punch holder (4) both ends upside is all fixed to be provided with telescopic link (6), frame (1) upper end one side inner wall spacing sliding connection has slider (7), slider (7) bottom one side is fixed to be provided with first hydraulic stem (8), slider (7) inner wall threaded connection has second bull stick (10), second bull stick (10) one end bearing connection frame (1) inside, frame (1) corresponds slider (7) one side inner wall sliding connection and has guide block (11), guide block (11) are connected with guide bar (12) sliding connection.
2. The wing compression-resistant detection device for unmanned aerial vehicle production according to claim 1, wherein the first rotating rod (3) extends to the outside of the frame (1) and is fixedly provided with a first disc (13), and a handle structure is arranged on one side of the first disc (13) opposite to the first rotating rod (3).
3. The wing compression-resistant detection device for unmanned aerial vehicle production according to claim 1, wherein one side of the top end of the telescopic rod (6) is fixedly connected with the frame (1), the bottom end of the guide rod (12) is fixedly connected with the extrusion plate (9), and one side of the bottom end of the extrusion plate (9) is arc-shaped.
4. The wing compression-resistant detection device for unmanned aerial vehicle production according to claim 1, wherein a second disc (14) is fixedly arranged at the other end of the second rotating rod (10) extending to the outside of the frame (1), and a handle structure is arranged on one side of the second disc (14) opposite to the second rotating rod (10).
5. The wing compression-resistant detection device for unmanned aerial vehicle production according to claim 1, wherein a wing (15) to be detected is clamped between the upper clamping plate (4) and the lower clamping plate (2), a single plate (16) is rotationally connected to one side of the frame (1) close to the lower end of the lower clamping plate (2), a second hydraulic rod (17) is rotationally connected to one side of the bottom end of the single plate (16), and one end of the second hydraulic rod (17) far away from the single plate (16) is rotationally connected with the frame (1).
6. The wing compression-resistant detection device for unmanned aerial vehicle production according to claim 5, wherein the single plate (16) is L-shaped, and the upper surface of one end of the single plate (16) and the rubber pad (5) on the lower clamping plate (2) are positioned on the same horizontal plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321003202.2U CN219890958U (en) | 2023-04-28 | 2023-04-28 | Wing resistance to compression detection device is used in unmanned aerial vehicle production |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321003202.2U CN219890958U (en) | 2023-04-28 | 2023-04-28 | Wing resistance to compression detection device is used in unmanned aerial vehicle production |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219890958U true CN219890958U (en) | 2023-10-24 |
Family
ID=88396115
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321003202.2U Active CN219890958U (en) | 2023-04-28 | 2023-04-28 | Wing resistance to compression detection device is used in unmanned aerial vehicle production |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219890958U (en) |
-
2023
- 2023-04-28 CN CN202321003202.2U patent/CN219890958U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2021109126A1 (en) | Probe module separation-distance quick-adjustment mechanism and forming needle bed | |
| CN219890958U (en) | Wing resistance to compression detection device is used in unmanned aerial vehicle production | |
| CN209784016U (en) | Blood smear preparation instrument | |
| CN110007116A (en) | A kind of TG antenna measurement rotation and lifting mobile station | |
| CN211121724U (en) | Thrust test equipment | |
| CN112326650A (en) | Quick detection device of pH value for bio-technology beer brewing | |
| CN209802940U (en) | Angle-adjustable combined regulator for flow cytometer | |
| CN204819334U (en) | Thermocouple plug instrument | |
| CN201819016U (en) | Searchlight with light source axial moving device | |
| CN207997094U (en) | A kind of aviation fasteners under head fillet rolling device | |
| CN202372187U (en) | Manual clamping self-locking device used for motormeter | |
| CN207935234U (en) | One kind is for Hopkinson pressure bar and strain gauge adhesion positioning device | |
| CN210109011U (en) | Auxiliary device of rubber sclerometer | |
| CN110763419A (en) | Drop test device | |
| CN221375011U (en) | Information acquisition equipment for inpatient standardized training and checking system | |
| CN219574198U (en) | Positioning equipment of motor detection device | |
| CN220626044U (en) | Comprehensive tester for electronic seat ring | |
| CN219152809U (en) | Fixing device is used in sensor production | |
| CN217156023U (en) | Convenient to use's smear device for medical science inspection | |
| CN215865053U (en) | Aircraft wing surface detection device for aerospace civil aircraft technology | |
| CN220039867U (en) | Soil sampling equipment | |
| CN220019178U (en) | Positioning assembly and pressure testing device | |
| CN110561513B (en) | Test paper cutting device for blood detection | |
| CN221377408U (en) | Device for detecting bending property of composite material | |
| CN218725742U (en) | Sampling device for dairy product detection |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |