CN219657121U - Impact force test device - Google Patents
Impact force test device Download PDFInfo
- Publication number
- CN219657121U CN219657121U CN202320780181.9U CN202320780181U CN219657121U CN 219657121 U CN219657121 U CN 219657121U CN 202320780181 U CN202320780181 U CN 202320780181U CN 219657121 U CN219657121 U CN 219657121U
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- test
- fixed
- box
- unmanned aerial
- aerial vehicle
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- 238000012360 testing method Methods 0.000 title claims abstract description 63
- 230000007246 mechanism Effects 0.000 claims abstract description 22
- 238000004804 winding Methods 0.000 claims abstract description 16
- 238000004140 cleaning Methods 0.000 claims description 20
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000011521 glass Substances 0.000 claims description 3
- 229910000617 Mangalloy Inorganic materials 0.000 claims description 2
- 208000012260 Accidental injury Diseases 0.000 abstract description 4
- 230000005484 gravity Effects 0.000 abstract description 4
- 230000009471 action Effects 0.000 abstract description 3
- 208000014674 injury Diseases 0.000 abstract description 3
- 210000000078 claw Anatomy 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 239000012535 impurity Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
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- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
The utility model discloses an impact force test device which comprises a supporting seat and a supporting plate, wherein the supporting plate is welded above the supporting seat. According to the utility model, the test mechanism is arranged, when the device is used, the box door is opened, the unmanned aerial vehicle is placed on the pneumatic clamping jaw, the pneumatic clamping jaw clamps and fixes the unmanned aerial vehicle, the box door is closed, the motor is started, the motor drives the winding wheel to rotate through the rotating shaft, the winding wheel rotates to wind the traction rope, the traction rope drives the unmanned aerial vehicle to ascend, the motor stops running when the unmanned aerial vehicle ascends to a corresponding height, the pneumatic clamping jaw releases the fixation of the unmanned aerial vehicle, the unmanned aerial vehicle rapidly descends under the action of gravity, so that the impact resistance of the unmanned aerial vehicle is tested, a worker can observe the test condition through the observation window, and the test box and the box door cooperate together to enable the test to be performed in a closed environment, so that accidental injury can be effectively avoided.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle manufacturing, in particular to an impact force test device.
Background
Unmanned aerial vehicles, for short, "unmanned aerial vehicles," are unmanned aerial vehicles that are operated by a radio remote control device and a self-contained programming device, or are operated autonomously, either entirely or intermittently, by an on-board computer.
The unmanned aerial vehicle needs to be tested for impact resistance during production, but most of the current tests are carried out in natural environments, and accidental injuries are easily caused in the test process, so that improvement is needed.
Disclosure of Invention
The present utility model has been made to solve the above-described problems, and an object of the present utility model is to provide an impact force test apparatus.
The utility model realizes the above purpose through the following technical scheme:
the impact force testing device comprises a supporting seat, a supporting plate and a testing mechanism, wherein the supporting plate is welded above the supporting seat, the testing mechanism is used for testing the impact force of the unmanned aerial vehicle, and the testing mechanism is fixed above the supporting plate;
the test mechanism comprises a test box, a box door, a vertical plate, a fixed box, a motor, a rotating shaft, a winding wheel, a traction rope, a lifting plate, lifting rods, pneumatic clamping jaws, a fixed plate and an observation window, wherein the box door is installed on the side face of the test box, the vertical plate is welded on the upper portion of the test box, the fixed box is welded on the upper portion of the vertical plate, the motor is installed on the side face of the fixed box, the rotating shaft is fixed at the output end of the motor, the winding wheel is fixed on the outer side of the rotating shaft, the traction rope is installed on the winding wheel, the lifting plate is fixed at one end of the traction rope, the lifting rods are welded on two sides of the lifting plate, the pneumatic clamping jaws are fixed below the lifting plate through bolts, and the fixed plate is arranged on the front portion and the rear portion of the pneumatic clamping jaws, and the observation window is installed on the front portion of the test box.
Preferably, the cleaning mechanism is mounted on the test mechanism and comprises a mounting plate, a first magic tape, a second magic tape and a cleaning wiper, wherein the first magic tape is adhered to the front portion of the mounting plate, the second magic tape is mounted on the front portion of the first magic tape, and the cleaning wiper is fixed on the front portion of the second magic tape.
Preferably, the motor is connected with the fixing box through bolts, and the fixing box is made of aluminum alloy.
Preferably, the number of the lifting rods is four, and the lifting rods are made of high manganese steel.
Preferably, the fixing plate is welded with the lifting plate, and the observation window is made of explosion-proof glass.
Preferably, the cleaning wiper is adhered to the second magic tape, and the cleaning wiper is made of sponge.
Compared with the prior art, the utility model has the following beneficial effects:
through setting up test mechanism, when using device, open the chamber door, place unmanned vehicles on pneumatic clamping jaw, pneumatic clamping jaw carries out the centre gripping to unmanned vehicles and fixes, closed chamber door and start motor, the motor drives the rolling wheel through the pivot and rotates, the rolling wheel rotates and carries out the rolling to the haulage rope, the haulage rope drives unmanned vehicles and rises, motor stop operation when unmanned vehicles rises to corresponding height, pneumatic clamping jaw is removed and is fixed unmanned vehicles, unmanned vehicles drops fast under the effect of gravity, so to test unmanned vehicles's impact resistance, the staff can observe experimental condition through the observation window, experimental box and chamber door cooperate jointly and make the experiment can be in closed environment, so can effectively avoid taking place the accidental injury.
Drawings
In order to more clearly illustrate the embodiments of the utility model or the technical solutions of the prior art, the drawings that are necessary for the description of the embodiments or the prior art will be briefly described, it being obvious that the drawings in the following description are only some embodiments of the utility model and that other drawings can be obtained according to these drawings without inventive faculty for a person skilled in the art.
FIG. 1 is a schematic view of an impact force testing apparatus according to the present utility model;
FIG. 2 is a front view of an impact force testing apparatus according to the present utility model;
FIG. 3 is a schematic diagram showing the internal structure of an impact force testing apparatus according to the present utility model;
FIG. 4 is a left side view of a lifter plate in an impact force testing apparatus of the present utility model;
FIG. 5 is an enlarged view of the impact force test apparatus according to the present utility model at A.
The reference numerals are explained as follows:
1. a support base; 2. a support plate; 3. a testing mechanism; 301. a test chamber; 302. a door; 303. a vertical plate; 304. a fixed box; 305. a motor; 306. a rotating shaft; 307. a winding wheel; 308. a traction rope; 309. a lifting plate; 310. a lifting rod; 311. pneumatic clamping jaws; 312. a fixing plate; 313. an observation window; 4. a cleaning mechanism; 401. a mounting plate; 402. a first magic tape; 403. the second magic tape; 404. cleaning the wiper.
Detailed Description
In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in 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 the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first", "a second", etc. may explicitly or implicitly include one or more such feature. In the description of the present utility model, unless otherwise indicated, the meaning of "a plurality" is two or more.
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 can be understood by those of ordinary skill in the art in a specific case.
The utility model is further described below with reference to the accompanying drawings:
as shown in fig. 1 to 5, an impact force test device comprises a supporting seat 1 and a supporting plate 2, wherein the supporting plate 2 is welded above the supporting seat 1, and further comprises a test mechanism 3 for testing the impact force of an unmanned aerial vehicle, and the test mechanism 3 is fixed above the supporting plate 2.
In the utility model, a test mechanism 3 comprises a test box 301, a box door 302, a vertical plate 303, a fixed box 304, a motor 305, a rotating shaft 306, a winding wheel 307, traction ropes 308, a lifting plate 309, lifting rods 310, pneumatic clamping claws 311, a fixed plate 312 and an observation window 313, wherein the box door 302 is arranged on the side surface of the test box 301, the vertical plate 303 is welded above the test box 301, the fixed box 304 is welded above the vertical plate 303, the motor 305 is arranged on the side surface of the fixed box 304 through bolts, the rotating shaft 306 is fixed at the output end of the motor 305, the winding wheel 307 is fixed on the outer side of the rotating shaft 306, the traction ropes 308 are arranged on the winding wheel 307, the lifting plate 309 is fixed at one end of the traction ropes 308, the lifting rods 310 are welded on two sides of the lifting plate 309, the pneumatic clamping claws 311 are fixed below the lifting plate 309 through bolts, the fixed plate 312 is arranged at the front part and the rear part of the pneumatic clamping claws 311, and the observation window 313 is arranged at the front part of the test box 301; the fixed box 304 is made of aluminum alloy, the lifting rods 310 are four in number, the fixed plate 312 is welded with the lifting plate 309, and the observation window 313 is made of explosion-proof glass; when the device is used, the box door 302 is opened, the unmanned aerial vehicle is placed on the pneumatic clamping jaw 311, the pneumatic clamping jaw 311 clamps and fixes the unmanned aerial vehicle, the box door 302 is closed, the motor 305 is started, the motor 305 drives the winding wheel 307 to rotate through the rotating shaft 306, the winding wheel 307 rotates to wind the traction rope 308, the traction rope 308 drives the unmanned aerial vehicle to ascend, the motor 305 stops running when the unmanned aerial vehicle ascends to a corresponding height, the pneumatic clamping jaw 311 releases the fixation of the unmanned aerial vehicle, the unmanned aerial vehicle rapidly descends under the action of gravity, the impact resistance of the unmanned aerial vehicle is tested, a worker can observe the test condition through the observation window 313, and the test box 301 and the box door 302 cooperate together to enable the test to be carried out in a closed environment, so that the accidental injury can be effectively avoided.
In the utility model, a cleaning mechanism 4 is arranged on a test mechanism 3, the cleaning mechanism 4 comprises a mounting plate 401, a first magic tape 402, a second magic tape 403 and a cleaning wiper 404, the first magic tape 402 is adhered to the front part of the mounting plate 401, the second magic tape 403 is arranged on the front part of the first magic tape 402, and the cleaning wiper 404 is adhered to the front part of the second magic tape 403; the cleaning wiper 404 is made of sponge; when the pneumatic clamping jaw 311 moves up and down, the cleaning wiper 404 moves along with the pneumatic clamping jaw, and the cleaning wiper 404 moves to clean impurities attached to the observation window 313, so that a worker can observe the test condition more clearly.
In the above structure: when the device is used, the box door 302 is opened, the unmanned aerial vehicle is placed on the pneumatic clamping jaw 311, the pneumatic clamping jaw 311 clamps and fixes the unmanned aerial vehicle, the box door 302 is closed, the motor 305 is started, the motor 305 drives the winding wheel 307 to rotate through the rotating shaft 306, the winding wheel 307 rotates to wind the traction rope 308, the traction rope 308 drives the unmanned aerial vehicle to ascend, the motor 305 stops running when the unmanned aerial vehicle ascends to a corresponding height, the pneumatic clamping jaw 311 releases the fixation of the unmanned aerial vehicle, the unmanned aerial vehicle rapidly drops under the action of gravity, the impact resistance of the unmanned aerial vehicle is tested, a worker can observe the test condition through the observation window 313, when the pneumatic clamping jaw 311 moves up and down, the cleaning wiper 404 moves along with the test condition, and therefore impurities attached to the observation window 313 are cleaned, and the worker can observe the test condition more clearly.
The foregoing has shown and described the basic principles, principal features and advantages of the utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims.
Claims (6)
1. The utility model provides an impact force test device, includes supporting seat (1), backup pad (2) are welded supporting seat (1) top, its characterized in that: the test device also comprises a test mechanism (3) for testing the impact resistance of the unmanned aerial vehicle, wherein the test mechanism (3) is fixed above the supporting plate (2);
the test mechanism (3) comprises a test box (301), a box door (302), a vertical plate (303), a fixed box (304), a motor (305), a rotating shaft (306), a winding wheel (307), a traction rope (308), a lifting plate (309), a lifting rod (310), a pneumatic clamping jaw (311), a fixed plate (312) and an observation window (313), wherein the box door (302) is arranged on the side surface of the test box (301), the vertical plate (303) is welded above the test box (301), the fixed box (304) is welded above the vertical plate (303), the motor (305) is arranged on the side surface of the fixed box (304), the rotating shaft (306) is fixed at the output end of the motor (305), the winding wheel (307) is fixed on the outer side of the rotating shaft (306), the traction rope (308) is arranged on the winding wheel (307), the lifting plate (309) is fixed at one end of the traction rope (308), the lifting rod (310) is welded on two sides of the lifting plate (309), the pneumatic clamping jaw (311) is fixed below the lifting plate (309) through a fixed bolt (311) and the front clamping jaw (312), the viewing window (313) is mounted in front of the test chamber (301).
2. An impact force testing device according to claim 1, wherein: cleaning mechanism (4) are installed on experimental mechanism (3), cleaning mechanism (4) are pasted (404) including mounting panel (401), first magic subsides (402), second magic, are pasted (403), the clearance, first magic is pasted (402) and is pasted the mounting panel (401) front portion, second magic is pasted (403) and is installed first magic is pasted (402) front portion, cleaning is pasted (404) and is fixed second magic is pasted (403) front portion.
3. An impact force testing device according to claim 1, wherein: the motor (305) is connected with the fixed box (304) through bolts, and the fixed box (304) is made of aluminum alloy.
4. An impact force testing device according to claim 1, wherein: the number of the lifting rods (310) is four, and the lifting rods are made of high manganese steel.
5. An impact force testing device according to claim 1, wherein: the fixing plate (312) is welded with the lifting plate (309), and the observation window (313) is made of explosion-proof glass.
6. An impact force testing device according to claim 2, wherein: the cleaning wiper (404) is adhered to the second magic tape (403), and the cleaning wiper (404) is made of sponge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320780181.9U CN219657121U (en) | 2023-04-11 | 2023-04-11 | Impact force test device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320780181.9U CN219657121U (en) | 2023-04-11 | 2023-04-11 | Impact force test device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219657121U true CN219657121U (en) | 2023-09-08 |
Family
ID=87857923
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320780181.9U Active CN219657121U (en) | 2023-04-11 | 2023-04-11 | Impact force test device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219657121U (en) |
-
2023
- 2023-04-11 CN CN202320780181.9U patent/CN219657121U/en active Active
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