CN112557191A - A part equipment check out test set for intelligent unmanned aerial vehicle research and development design - Google Patents
A part equipment check out test set for intelligent unmanned aerial vehicle research and development design Download PDFInfo
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- CN112557191A CN112557191A CN202011370209.9A CN202011370209A CN112557191A CN 112557191 A CN112557191 A CN 112557191A CN 202011370209 A CN202011370209 A CN 202011370209A CN 112557191 A CN112557191 A CN 112557191A
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/08—Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces
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Abstract
The invention relates to the technical field of part strength detection, in particular to part assembly detection equipment for research and development design of an intelligent unmanned aerial vehicle, which enables a worker to use defective goods during assembly and improves the practicability; still include the workstation, the bottom of workstation is provided with the support frame, the bottom of workstation is connected with the top of support frame, the top of workstation is provided with removes the frame, the top of workstation is connected with the top of removing the frame, be provided with the shifting chute on removing the frame, can remove to be provided with the mobile device on the shifting chute of frame, the top of mobile device is provided with the connecting rod, the top of mobile device is connected with the bottom of connecting rod, the top of connecting rod is provided with the connecting plate, the top of connecting rod is connected with the bottom of connecting plate, the top of connecting plate is provided with the pole setting, the top of connecting plate is connected with the bottom of pole setting, the front end of pole setting is provided with the crossbeam, the front end of pole setting is connected with the rear.
Description
Technical Field
The invention relates to the technical field of part strength detection, in particular to part assembly detection equipment for research and development design of an intelligent unmanned aerial vehicle.
Background
As is well known, an unmanned plane is abbreviated as "unmanned plane", and abbreviated as "UAV", and is an unmanned plane operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, when a worker assembles parts using a tool, defective parts are easily damaged as a whole, and the practicability is poor.
Disclosure of Invention
In order to solve the technical problems, the invention provides the part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle, which enables the worker to use the defective products during assembly and improves the practicability.
The invention relates to part assembly detection equipment for intelligent unmanned aerial vehicle research and development design, which further comprises a workbench, wherein a support frame is arranged at the bottom end of the workbench, the bottom end of the workbench is connected with the top end of the support frame, a movable frame is arranged at the top end of the workbench, the top end of the workbench is connected with the top end of the movable frame, a movable groove is formed in the movable frame, a movable device is movably arranged on the movable groove of the movable frame, a connecting rod is arranged at the top end of the movable device, the top end of the movable device is connected with the bottom end of the connecting rod, a connecting plate is arranged at the top end of the connecting rod, the top end of the connecting rod is connected with the bottom end of the connecting plate, a vertical rod is arranged at the top end of the connecting plate, the top end of the connecting plate is connected with the bottom end of the vertical rod, a cross, the bottom of riser is provided with the lifter, and the bottom of riser is connected with the top of lifter, and the bottom of lifter is provided with presses the clamp plate, and the bottom of lifter is connected with the top of pressing the clamp plate, and the top of workstation is provided with examines test table, and the top of workstation is connected with the bottom of examining test table, examines test table's top and is provided with and places the platform, examines test table's top and is connected with the bottom of placing the platform, examines test table and is connected with external equipment electricity.
According to the part assembly detection device for the research and development design of the intelligent unmanned aerial vehicle, two groups of triangular support plates are arranged at the bottom end of the cross beam, the bottom end of the cross beam is connected with the top ends of the two groups of triangular support plates, and the rear ends of the two groups of triangular support plates are connected with the front ends of the vertical rods.
According to the part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle, the top end of the workbench is detachably provided with the storage box, the top end of the workbench is connected with the bottom end of the storage box, the storage box is internally provided with the inner cavity, and the top end of the storage box is provided with the upper opening.
According to the part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle, a plurality of groups of fixing frames are arranged at the top end of the workbench, the top end of the workbench is connected with the bottom ends of the plurality of groups of fixing frames, and the plurality of groups of fixing frames are connected with the bottom of the storage box.
The part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle is characterized in that a plurality of groups of buffer rods are arranged at the bottom end of a support frame, the bottom end of the support frame is connected with the top ends of the plurality of groups of buffer rods, buffer sleeves are arranged at the bottom ends of the plurality of groups of buffer rods, the bottom ends of the plurality of groups of buffer rods penetrate through the top ends of the plurality of groups of buffer sleeves, inner cavities are formed in the plurality of groups of buffer sleeves, buffer springs are arranged at the bottom ends of the inner cavities of the plurality of groups of buffer sleeves, the bottom ends of the plurality of groups of buffer rods respectively abut against the top ends of the.
According to the part assembly detection device for the research and development design of the intelligent unmanned aerial vehicle, the bottom end of the support frame is provided with the plurality of groups of first fixing plates, the bottom end of the support frame is connected with the top ends of the plurality of groups of first fixing plates, and the bottom ends of the plurality of groups of first fixing plates are respectively connected with the top ends of the plurality of groups of buffer rods.
The invention relates to part assembly detection equipment for research and development design of an intelligent unmanned aerial vehicle.
According to the part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle, the second fixing plate is arranged at the top end of the pressing plate, the top end of the pressing plate is connected with the bottom end of the second fixing plate, and the top end of the second fixing plate is connected with the bottom end of the lifting rod.
Compared with the prior art, the invention has the beneficial effects that: place the spare part that will detect intensity earlier on examining test table, later start mobile device, mobile device passes through connecting rod and connecting plate and drives pole setting lateral shifting, move the spare part directly over according to the pressure board after, start the riser, the riser makes through the lifter press down the pressure board and press down the detection to the spare part, later examine test table and detect the intensity of pressing that the spare part received, and examine test table and with data display on external equipment, make the staff use the condition of wastrel when the equipment, improve the practicality.
Drawings
FIG. 1 is a front view of the present invention;
FIG. 2 is a schematic top view of the present invention;
FIG. 3 is a schematic cross-sectional view of the present invention;
FIG. 4 is a schematic axial side view of the present invention;
in the drawings, the reference numbers: 1. a work table; 2. a support frame; 3. a movable frame; 4. a mobile device; 5. a connecting rod; 6. a connecting plate; 7. erecting a rod; 8. a cross beam; 9. a lifter; 10. a lifting rod; 11. a pressing plate; 12. a detection table; 13. a placing table; 14. a triangular support plate; 15. a storage box; 16. a fixed mount; 17. a buffer rod; 18. a buffer sleeve; 19. a base plate; 20. a first fixing plate; 21. a warning light; 22. and a second fixing plate.
Detailed Description
The following detailed description of embodiments of the present invention is provided in connection with the accompanying drawings and examples. The following examples are intended to illustrate the invention but are not intended to limit the scope of the invention.
As shown in fig. 1 to 4, the part assembly detection apparatus for intelligent unmanned aerial vehicle research and development design of the present invention further includes a workbench 1, a support frame 2 is disposed at a bottom end of the workbench 1, a bottom end of the workbench 1 is connected to a top end of the support frame 2, a moving frame 3 is disposed at a top end of the workbench 1, a top end of the workbench 1 is connected to a top end of the moving frame 3, a moving slot is disposed on the moving frame 3, a moving device 4 is movably disposed on the moving slot of the moving frame 3, a connecting rod 5 is disposed at a top end of the moving device 4, a top end of the moving device 4 is connected to a bottom end of the connecting rod 5, a top end of the connecting rod 5 is provided with a connecting plate 6, a top end of the connecting rod 5 is connected to a bottom end of the connecting plate 6, a top end of the connecting plate 6 is provided with an upright post 7, a top end of the connecting plate 6 is connected, the top end of the beam 8 is provided with a lifter 9, the top end of the beam 8 is connected with the bottom end of the lifter 9, the bottom end of the lifter 9 is provided with a lifting rod 10, the bottom end of the lifter 9 is connected with the top end of the lifting rod 10, the bottom end of the lifting rod 10 is provided with a pressing plate 11, the bottom end of the lifting rod 10 is connected with the top end of the pressing plate 11, the top end of the workbench 1 is provided with a detection table 12, the top end of the workbench 1 is connected with the bottom end of the detection table 12, the top end of the detection table 12 is provided with a placing table 13, the top end of the detection table 12 is connected with the bottom end of the placing table 13; place the spare part that will detect intensity earlier on examining test table 12, later start mobile device 4, mobile device 4 drives pole setting 7 lateral shifting through connecting rod 5 and connecting plate 6, after removing to the spare part directly over according to pressure board 11, start riser 9, riser 9 makes through lifter 10 and presses down the detection to the spare part according to board 11, later examine test table 12 and detect the intensity of pressing that the spare part received, and examine test table 12 and with data display on external equipment, the condition that makes the staff use the wastrel when the equipment, improve the practicality.
According to the part assembly detection device for the research and development design of the intelligent unmanned aerial vehicle, two groups of triangular support plates 14 are arranged at the bottom end of the cross beam 8, the bottom end of the cross beam 8 is connected with the top ends of the two groups of triangular support plates 14, and the rear ends of the two groups of triangular support plates 14 are connected with the front ends of the upright rods 7; through the above, the triangular support plate 14 can provide a good support effect for the cross beam 8, and the stability is improved.
According to the part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle, the top end of the workbench 1 is detachably provided with the storage box 15, the top end of the workbench 1 is connected with the bottom end of the storage box 15, an inner cavity is formed in the storage box 15, and the top end of the storage box 15 is provided with an upper opening; through the aforesaid, the staff can deposit spare part temporarily through storage box 15, improves the convenience.
According to the part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle, a plurality of groups of fixing frames 16 are arranged at the top end of the workbench 1, the top end of the workbench 1 is connected with the bottom ends of the plurality of groups of fixing frames 16, and the plurality of groups of fixing frames 16 are connected with the bottom of the storage box 15; through the above, the fixing frame 16 can reduce the falling-off of the storage box 15, and the fixing frame 16 can play a good role in fixing the storage box 15, so that the practicability is improved.
The part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle is characterized in that a plurality of groups of buffer rods 17 are arranged at the bottom end of a support frame 2, the bottom end of the support frame 2 is connected with the top ends of the plurality of groups of buffer rods 17, buffer sleeves 18 are arranged at the bottom ends of the plurality of groups of buffer rods 17, the bottom ends of the plurality of groups of buffer rods 17 penetrate through the top ends of the plurality of groups of buffer sleeves 18, an inner cavity is arranged inside the plurality of groups of buffer sleeves 18, buffer springs are arranged at the bottom ends of the inner cavities of the plurality of groups of buffer sleeves 18, the bottom ends of the plurality of groups of buffer rods 17 respectively abut against the top ends of the plurality of groups; through the above, the buffer rod 17, the buffer sleeve 18 and the bottom plate 19 can reduce the influence of the vibration factor generated from the outside on the whole workbench 1, and improve the stability.
According to the part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle, the bottom end of the support frame 2 is provided with the multiple groups of first fixing plates 20, the bottom end of the support frame 2 is connected with the top ends of the multiple groups of first fixing plates 20, and the bottom ends of the multiple groups of first fixing plates 20 are respectively connected with the top ends of the multiple groups of buffer rods 17; through the above, the first fixing plate 20 can reduce the falling of the plurality of groups of buffer rods 17, and the firmness is improved.
The invention relates to part assembly detection equipment for intelligent unmanned aerial vehicle research and development design.A prompt lamp 21 is arranged at the top end of a lifter 9, the top end of the lifter 9 is connected with the bottom end of the prompt lamp 21, and the lifter 9 is electrically connected with the prompt lamp 21; through the above, the indicator light 21 is turned on when the lifter 9 works, so that the indicator light has an indication effect on workers and improves safety.
According to the part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle, a second fixing plate 22 is arranged at the top end of a pressing plate 11, the top end of the pressing plate 11 is connected with the bottom end of the second fixing plate 22, and the top end of the second fixing plate 22 is connected with the bottom end of a lifting rod 10; as described above, the second fixing plate 22 can reduce the possibility of the pressing plate 11 falling off, and can improve the firmness.
When the part assembly detection device for the research and development design of the intelligent unmanned aerial vehicle works, firstly, parts needing strength detection are placed on the detection table 12, then the moving device 4 is started, the moving device 4 drives the upright rod 7 to transversely move through the connecting rod 5 and the connecting plate 6, after the pressing plate 11 moves right above the parts, the lifter 9 is started, the lifter 9 enables the pressing plate 11 to press and detect the parts through the lifting rod 10, then the detection table 12 detects the pressing strength of the parts, and the detection table 12 displays data on external equipment.
The part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle is common in installation mode, connection mode or setting mode, and can be implemented as long as the beneficial effects of the part assembly detection equipment are achieved.
The above description is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, several modifications and variations can be made without departing from the technical principle of the present invention, and these modifications and variations should also be regarded as the protection scope of the present invention.
Claims (8)
1. The part assembly detection equipment for the research and development design of the intelligent unmanned aerial vehicle is characterized by further comprising a workbench (1), a support frame (2) is arranged at the bottom end of the workbench (1), the bottom end of the workbench (1) is connected with the top end of the support frame (2), a movable frame (3) is arranged at the top end of the workbench (1), the top end of the workbench (1) is connected with the top end of the movable frame (3), a movable groove is formed in the movable frame (3), a movable device (4) is movably arranged on the movable groove of the movable frame (3), a connecting rod (5) is arranged at the top end of the movable device (4), the top end of the movable device (4) is connected with the bottom end of the connecting rod (5), a connecting plate (6) is arranged at the top end of the connecting rod (5), the top end of the connecting rod (5) is connected with the bottom end of the connecting plate (6), a vertical, the top end of the connecting plate (6) is connected with the bottom end of the upright rod (7), the front end of the upright rod (7) is provided with a crossbeam (8), the front end of the upright rod (7) is connected with the rear end of the crossbeam (8), the top end of the crossbeam (8) is provided with a lifter (9), the top end of the crossbeam (8) is connected with the bottom end of the lifter (9), the bottom end of the lifter (9) is provided with a lifting rod (10), the bottom end of the lifter (9) is connected with the top end of the lifting rod (10), the bottom end of the lifting rod (10) is provided with a pressing plate (11), the bottom end of the lifting rod (10) is connected with the top end of the pressing plate (11), the top end of the workbench (1) is provided with a detection table (12), the top end of the workbench (1) is connected with the bottom end of the detection table (12), the top end of the detection table (12) is provided with a placing table (13), and, the detection table (12) is electrically connected with external equipment.
2. The part assembly detection apparatus for intelligent unmanned aerial vehicle development and design according to claim 1, wherein the bottom end of the cross beam (8) is provided with two sets of triangular support plates (14), the bottom end of the cross beam (8) is connected with the top ends of the two sets of triangular support plates (14), and the rear ends of the two sets of triangular support plates (14) are connected with the front ends of the vertical rods (7).
3. The part assembly detection device for intelligent unmanned aerial vehicle research and development design according to claim 2, characterized in that a storage box (15) is detachably arranged at the top end of the workbench (1), the top end of the workbench (1) is connected with the bottom end of the storage box (15), an inner cavity is arranged inside the storage box (15), and an upper opening is arranged at the top end of the storage box (15).
4. The part assembly detection apparatus for intelligent unmanned aerial vehicle research and development design of claim 3, characterized in that, the top of workstation (1) is provided with multiunit mount (16), and the top of workstation (1) is connected with the bottom of multiunit mount (16), and multiunit mount (16) are connected with the bottom of storage box (15).
5. The part assembly detection apparatus for intelligent unmanned aerial vehicle research and development design according to claim 4, wherein the bottom end of the support frame (2) is provided with a plurality of groups of buffer rods (17), the bottom end of the support frame (2) is connected with the top ends of the plurality of groups of buffer rods (17), the bottom ends of the plurality of groups of buffer rods (17) are provided with buffer sleeves (18), the bottom ends of the plurality of groups of buffer rods (17) pass through the top ends of the plurality of groups of buffer sleeves (18), the inside of the plurality of groups of buffer sleeves (18) is provided with an inner cavity, the bottom ends of the inner cavities of the plurality of groups of buffer sleeves (18) are provided with buffer springs, the bottom ends of the plurality of groups of buffer rods (17) respectively abut against the top ends of the plurality of groups of buffer springs, the bottom ends of the plurality of groups.
6. The part assembly detection apparatus for intelligent unmanned aerial vehicle research and development design of claim 5, characterized in that, the bottom of support frame (2) is provided with multiunit first fixed plate (20), and the bottom of support frame (2) is connected with the top of multiunit first fixed plate (20), and the bottom of multiunit first fixed plate (20) is connected with the top of multiunit buffer beam (17) respectively.
7. The part assembly detection device for intelligent unmanned aerial vehicle development and design according to claim 6, characterized in that a tip of the lifter (9) is provided with a warning light (21), the tip of the lifter (9) is connected with the bottom end of the warning light (21), and the lifter (9) is electrically connected with the warning light (21).
8. The part assembly detection apparatus for intelligent unmanned aerial vehicle development and design according to claim 7, wherein a second fixing plate (22) is disposed at a top end of the pressing plate (11), the top end of the pressing plate (11) is connected with a bottom end of the second fixing plate (22), and a top end of the second fixing plate (22) is connected with a bottom end of the lifting rod (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011370209.9A CN112557191A (en) | 2020-11-30 | 2020-11-30 | A part equipment check out test set for intelligent unmanned aerial vehicle research and development design |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011370209.9A CN112557191A (en) | 2020-11-30 | 2020-11-30 | A part equipment check out test set for intelligent unmanned aerial vehicle research and development design |
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| Publication Number | Publication Date |
|---|---|
| CN112557191A true CN112557191A (en) | 2021-03-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011370209.9A Withdrawn CN112557191A (en) | 2020-11-30 | 2020-11-30 | A part equipment check out test set for intelligent unmanned aerial vehicle research and development design |
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| CN (1) | CN112557191A (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205656086U (en) * | 2015-12-31 | 2016-10-19 | 上海天地涂料有限公司 | A check out test set for detecting aircraft dope's shock resistance |
| CN207742029U (en) * | 2017-12-08 | 2018-08-17 | 东莞鸿德检测设备有限公司 | A kind of furniture detection dining deck plate pressure test equipment |
| CN108593437A (en) * | 2018-05-16 | 2018-09-28 | 孟飞 | A kind of resistance to compression of plastic products and tension method and application method |
| CN109484669A (en) * | 2018-11-16 | 2019-03-19 | 黎庆佳 | A kind of agricultural unmanned plane assembling wing strength test mechanism |
| CN210719990U (en) * | 2019-10-14 | 2020-06-09 | 东源广工大现代产业协同创新研究院 | Unmanned aerial vehicle paddle detection device |
| CN211707596U (en) * | 2019-12-31 | 2020-10-20 | 苏州世扬自动化科技有限公司 | Circumferential bearing pressure detection device |
-
2020
- 2020-11-30 CN CN202011370209.9A patent/CN112557191A/en not_active Withdrawn
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205656086U (en) * | 2015-12-31 | 2016-10-19 | 上海天地涂料有限公司 | A check out test set for detecting aircraft dope's shock resistance |
| CN207742029U (en) * | 2017-12-08 | 2018-08-17 | 东莞鸿德检测设备有限公司 | A kind of furniture detection dining deck plate pressure test equipment |
| CN108593437A (en) * | 2018-05-16 | 2018-09-28 | 孟飞 | A kind of resistance to compression of plastic products and tension method and application method |
| CN109484669A (en) * | 2018-11-16 | 2019-03-19 | 黎庆佳 | A kind of agricultural unmanned plane assembling wing strength test mechanism |
| CN210719990U (en) * | 2019-10-14 | 2020-06-09 | 东源广工大现代产业协同创新研究院 | Unmanned aerial vehicle paddle detection device |
| CN211707596U (en) * | 2019-12-31 | 2020-10-20 | 苏州世扬自动化科技有限公司 | Circumferential bearing pressure detection device |
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Application publication date: 20210326 |
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