CN212125562U - Unmanned aerial vehicle simulation flight platform - Google Patents
Unmanned aerial vehicle simulation flight platform Download PDFInfo
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- CN212125562U CN212125562U CN201922141630.1U CN201922141630U CN212125562U CN 212125562 U CN212125562 U CN 212125562U CN 201922141630 U CN201922141630 U CN 201922141630U CN 212125562 U CN212125562 U CN 212125562U
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- unmanned aerial
- aerial vehicle
- flight platform
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- transparent cover
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- 238000004088 simulation Methods 0.000 title claims abstract description 11
- 238000003466 welding Methods 0.000 claims abstract description 11
- 238000009423 ventilation Methods 0.000 claims abstract description 5
- 238000001179 sorption measurement Methods 0.000 claims description 21
- 239000007921 spray Substances 0.000 claims description 10
- 238000001125 extrusion Methods 0.000 claims description 8
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 5
- 230000006835 compression Effects 0.000 claims description 2
- 238000007906 compression Methods 0.000 claims description 2
- 239000003595 mist Substances 0.000 claims description 2
- 230000000694 effects Effects 0.000 description 6
- 238000010521 absorption reaction Methods 0.000 description 5
- 208000035473 Communicable disease Diseases 0.000 description 1
- 206010044565 Tremor Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
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Abstract
The utility model provides an unmanned aerial vehicle simulation flight platform belongs to unmanned air vehicle technical field, include: the bottom plate, the translucent cover has been cup jointed to the bottom plate top, translucent cover inner wall left side embedding is equipped with the exhaust fan, translucent cover right side wall opening is equipped with the ventilation hole, the embedding of translucent cover inner wall top is equipped with the shower nozzle, translucent cover right side bottom opening is equipped with the drain pipe, the positive fixed surface of translucent cover bonds and has control panel, surface opening is equipped with first spout on the bottom plate, the embedding is equipped with first slider in the first spout, first slider welding has the fly leaf, this kind of unmanned aerial vehicle simulation flight platform, can simulate unmanned aerial vehicle multi-angle flight, and can observe unmanned aerial vehicle and meet its self influence of bad weather under natural condition.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle simulation flight platform.
Background
A drone is an unmanned aircraft that is operated with a radio remote control device and self-contained program control, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle is applied to the industry and is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Most simulation unmanned aerial vehicle actual flight's flying platform on the market at present can only realize the action of swaying of small-amplitude usually, and what have can only realize the rotation on the horizontal plane, has certain limitation, consequently, to this current situation, an unmanned aerial vehicle simulation flying platform of urgent need development to overcome not enough in the current practical application.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle simulation flight platform who proposes, in order to realize above-mentioned purpose, the utility model discloses a following technical scheme:
an unmanned aerial vehicle simulated flight platform comprising: a bottom plate, a transparent cover is sleeved above the bottom plate, an exhaust fan is embedded in the left side of the inner wall of the transparent cover, a vent hole is formed in the opening of the right side wall of the transparent cover, a spray head is embedded in the top end of the inner wall of the transparent cover, a drain pipe is arranged in the opening of the right side bottom of the transparent cover, a control panel is fixedly bonded on the front surface of the transparent cover, a first chute is formed in the opening of the upper surface of the bottom plate, a first slider is embedded in the first chute, a movable plate is welded on the first slider, first push rods are fixedly mounted on the two sides of the first chute and the surface of the bottom plate, the output end of each first push rod is fixedly connected with the front surface of the movable plate, a second chute is formed in the opening of the upper surface of the movable plate, a second push rod is fixedly connected on the right, second push rod output and third push rod right side wall fixed connection, the welding of third push rod output has the backup pad, and backup pad upper surface embedding is equipped with first absorption piece, the welding of backup pad top central point puts the bracing piece, the welding of bracing piece top has the activity ball, the activity of activity ball top is equipped with the mounting panel, mounting panel bottom opening is equipped with the embedded groove, the embedding of mounting panel lower surface is equipped with the second and adsorbs the piece, and mounting panel upper surface opening is equipped with the mounting hole, the bracing piece outer wall has cup jointed the extrusion spring, extrusion spring below and bracing piece outer wall welding have the dog.
Preferably, the number of the first push rods is two, the two first push rods are symmetrically distributed by taking the first sliding groove as a central line, and the first push rods, the second push rods and the third push rods are all electric push rods with the same model.
Preferably, the first sliding groove, the first sliding block, the second sliding groove and the second sliding block are all in a T shape.
Preferably, the exhaust fan air outlet is just to the translucent cover inside, and the ventilation hole is a plurality of, evenly distributed in the exhaust fan corresponds the side.
Preferably, the spray head is a mist spray head, and the water inlet end of the spray head is connected with an external flowing water source.
Preferably, backup pad and mounting panel are the same cylinder of big or small shape, and first adsorption block and second adsorption block are four at least, first adsorption block is the electro-magnet, the second adsorption block is permanent magnet, and accessible control panel carries out single control to first adsorption block, but the mounting panel passes through 360 degrees shakings of level in the activity ball embedding embedded groove on bracing piece top.
Preferably, the pressing spring is pressed between the mounting plate and the stopper in a compressed state.
Compared with the prior art, the utility model provides an unmanned aerial vehicle simulation flight platform possesses following beneficial effect:
1. in the utility model, the transparent cover is sleeved on the surface of the bottom plate, and the exhaust fan and the vent hole are arranged in the transparent cover, so that air flow and rainwater can be produced when the unmanned aerial vehicle simulates flying, and the influence of natural environment change on the flying of the unmanned aerial vehicle can be observed;
2. in the utility model, the flight state of the unmanned aerial vehicle, such as horizontal, longitudinal and vertical take-off and landing, can be simulated by the cooperation of the first push rod, the movable plate, the second push rod, the third push rod, the first chute, the second chute, the first slider and the second slider, and the real flight state of the unmanned aerial vehicle is displayed;
3. the utility model discloses in, adsorb the piece through setting up first absorption piece, backup pad and second, through the start-up of the first absorption piece in the control panel control support board, the angle of inclination of steerable mounting panel to simulation unmanned aerial vehicle's multi-angle flight.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is an enlarged schematic view of the position A of the present invention;
FIG. 3 is a schematic view of a partial cross-sectional structure of the present invention;
fig. 4 is a schematic view of the connection structure of the middle movable plate and the bottom plate of the present invention.
In the figure: 1-a bottom plate; 2-a transparent cover; 3-an exhaust fan; 4-a vent hole; 5-a spray head; 6, a drain pipe; 7-a control panel; 8-a first chute; 9-a first slider; 10-a movable plate; 11-a first push rod; 12-a second runner; 13-a second push rod; 14-a second slide; 15-a third push rod; 16-a support plate; 17-a first adsorption mass; 18-a support bar; 19-a movable ball; 20-mounting a plate; 21-an embedded groove; 22-a compression spring; 23-a stopper; 24-a second adsorption block; 25-mounting holes.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Referring to fig. 1-4, an unmanned aerial vehicle simulated flight platform comprises: the bottom plate 1 is characterized in that a transparent cover 2 is sleeved above the bottom plate 1, an exhaust fan 3 is embedded in the left side of the inner wall of the transparent cover 2, a vent hole 4 is formed in an opening of the right side wall of the transparent cover 2, a spray head 5 is embedded in the top end of the inner wall of the transparent cover 2, a drain pipe 6 is arranged in an opening of the right side bottom of the transparent cover 2, a control panel 7 is fixedly bonded on the front surface of the transparent cover 2, a first chute 8 is formed in an opening of the upper surface of the bottom plate 1, a first slide block 9 is embedded in the first chute 8, a movable plate 10 is welded on the first slide block 9, first push rods 11 are fixedly mounted on the two sides of the first chute 8 and the surface of the bottom plate 1, the output end of each first push rod 11 is fixedly connected with the front surface of the movable plate 10, a second chute 12 is formed in an opening of, 14 top welding of second slider has third push rod 15, 13 output ends of second push rod and 15 right side wall fixed connection of third push rod, 15 output welding of third push rod has backup pad 16, and 16 upper surface embeddings of backup pad are equipped with first absorption block 17, 16 top central points of backup pad put the welding have bracing piece 18, 18 top welding of bracing piece has movable ball 19, the activity of 19 tops of movable ball is equipped with mounting panel 20, 20 bottom openings of mounting panel are equipped with embedded groove 21, 20 lower surface embeddings of mounting panel are equipped with second absorption block 24, and 20 upper surface openings of mounting panel are equipped with mounting hole 25, 18 outer walls of bracing piece have cup jointed extrusion spring 22, extrusion spring 22 below and 18 outer wall welding of bracing piece have dog 23.
Preferably, 11 quantity of first push rod are two, and two first push rods 11 use first spout 8 to distribute as the central line symmetry, and first push rod 11, second push rod 13 and third push rod 15 are the electric putter of the same model, under the promotion of first push rod 11, can simulate unmanned aerial vehicle's vertical flight, under the promotion of second push rod 13, can simulate unmanned aerial vehicle's horizontal flight, under the promotion of third push rod 15, can simulate unmanned aerial vehicle's vertical lift.
Preferably, the first sliding chute 8, the first sliding block 9, the second sliding chute 12 and the second sliding block 14 are all in a "T" shape, so that the moving stability of the movable plate 10 and the third push rod 15 can be ensured.
Preferably, 3 air outlets of exhaust fan are just to 2 insides of translucent cover, and ventilation hole 4 is a plurality of, and evenly distributed is in 3 corresponding sides of exhaust fan, can imitate unmanned aerial vehicle and run into the influence that strong wind weather produced self flight under natural environment.
Preferably, shower nozzle 5 is vaporific shower nozzle, and shower nozzle 5 is intake and is held and be connected with external flowing water source, can imitate unmanned aerial vehicle and run into the influence that the rainy day produced to self flight under natural environment.
Preferably, backup pad 16 and mounting panel 20 are the same cylinder of size shape, and first adsorption block 17 and second adsorption block 24 are at least four, first adsorption block 17 is the electro-magnet, second adsorption block 24 is permanent magnet, and accessible control panel 7 carries out single control to first adsorption block 17, but mounting panel 20 passes through the movable ball 19 embedding embedded groove 21 on bracing piece 18 top and can level 360 degrees and rock, through the open mode of first adsorption block 17 on the control panel 7 control backup pad 16, can simulate unmanned aerial vehicle multi-angle flight.
Preferably, the extrusion spring 22 is extruded between the mounting plate 20 and the stop block 23 in a compressed state, and when the unmanned aerial vehicle needs horizontal flight, the unmanned aerial vehicle can be always kept in a horizontal state under the elastic force of the extrusion spring 22 by disconnecting the current of all the first adsorption blocks 17.
The working principle is as follows: during the use, install unmanned aerial vehicle on mounting panel 20, through control panel 7 control first push rod 11, second push rod 13 and third push rod 15 remove, can simulate unmanned horizontal and vertical flight and vertical lift, first adsorption block 17 through different positions on control panel 7 control support plate 16 starts, under the magnetic force effect, realize mounting panel 20's multi-angle slope, thereby simulate unmanned aerial vehicle multi-angle slope flight, through starting air discharge fan 3 or switch-on shower nozzle 5 on the translucent cover 2, can simulate unmanned aerial vehicle and meet the influence that strong wind or rainy day caused its self flight under natural environment.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (7)
1. An unmanned aerial vehicle simulated flight platform comprising: the bottom plate (1) is characterized in that a transparent cover (2) is sleeved above the bottom plate (1), an exhaust fan (3) is embedded in the left side of the inner wall of the transparent cover (2), a ventilation hole (4) is formed in the opening of the right side wall of the transparent cover (2), a spray head (5) is embedded in the top end of the inner wall of the transparent cover (2), a drain pipe (6) is arranged in the opening of the bottom of the right side of the transparent cover (2), a control panel (7) is fixedly bonded on the front surface of the transparent cover (2), a first sliding chute (8) is formed in the opening of the upper surface of the bottom plate (1), a first sliding block (9) is embedded in the first sliding chute (8), a movable plate (10) is welded on the first sliding block (9), first push rods (11) are fixedly mounted on the two sides of the first sliding chute (8) and the surface of the bottom plate (1), and, the movable plate is characterized in that a second sliding groove (12) is arranged at an upper surface opening of the movable plate (10), a second push rod (13) is fixedly connected to the right side of the second sliding groove (12) and the surface of the movable plate (10), a second slider (14) is arranged in the second sliding groove (12) in an inner movable manner, a third push rod (15) is welded at the top end of the second slider (14), an output end of the second push rod (13) is fixedly connected with the right side wall of the third push rod (15), a support plate (16) is welded at an output end of the third push rod (15), a first adsorption block (17) is embedded in the upper surface of the support plate (16), a support rod (18) is welded at the top center position of the support plate (16), a movable ball (19) is welded at the top end of the support rod (18), a mounting plate (20) is movably arranged above the movable, the embedding of mounting panel (20) lower surface is equipped with second and adsorbs piece (24), and mounting panel (20) upper surface opening is equipped with mounting hole (25), bracing piece (18) outer wall has cup jointed extrusion spring (22), extrusion spring (22) below and bracing piece (18) outer wall welding have dog (23).
2. The unmanned aerial vehicle simulated flight platform of claim 1, characterized in that the number of the first push rods (11) is two, and two first push rods (11) are symmetrically distributed with the first chute (8) as a center line, and the first push rods (11), the second push rods (13) and the third push rods (15) are all electric push rods of the same type.
3. An unmanned aerial vehicle simulated flight platform as claimed in claim 1, wherein the first runner (8), the first slider (9), the second runner (12) and the second slider (14) are all "T" shaped.
4. An unmanned aerial vehicle simulation flight platform of claim 1, characterized in that exhaust fan (3) air outlet is just to the inside of translucent cover (2), and ventilation hole (4) are a plurality of, evenly distributed in exhaust fan (3) corresponding side.
5. An unmanned aerial vehicle simulated flight platform as claimed in claim 1, wherein the spray head (5) is a mist spray head, and the water inlet end of the spray head (5) is connected with an external flowing water source.
6. The unmanned aerial vehicle simulated flight platform of claim 1, characterized in that the supporting plate (16) and the mounting plate (20) are cylinders with the same size and shape, and the first adsorption block (17) and the second adsorption block (24) are both at least four blocks, the first adsorption block (17) is an electromagnet, the second adsorption block (24) is a permanent magnet, and the first adsorption block (17) can be controlled individually by the control panel (7), and the mounting plate (20) can be swung horizontally by 360 degrees by embedding the movable ball (19) at the top end of the supporting rod (18) into the embedding groove (21).
7. An unmanned aerial vehicle simulated flight platform as claimed in claim 1, wherein the compression spring (22) is compressed between the mounting plate (20) and the stop (23).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922141630.1U CN212125562U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle simulation flight platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922141630.1U CN212125562U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle simulation flight platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212125562U true CN212125562U (en) | 2020-12-11 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922141630.1U Expired - Fee Related CN212125562U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle simulation flight platform |
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| Country | Link |
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| CN (1) | CN212125562U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112623132A (en) * | 2020-12-25 | 2021-04-09 | 山东科技大学 | Offshore platform capable of recycling unmanned aerial vehicle |
| CN112874812A (en) * | 2021-03-19 | 2021-06-01 | 山东太古飞机工程有限公司 | Functional reliability testing device for PSU oxygen system of airplane |
| CN113859582A (en) * | 2021-11-30 | 2021-12-31 | 中国飞机强度研究所 | Airplane test freezing fog and freezing rain environment simulation system |
-
2019
- 2019-12-04 CN CN201922141630.1U patent/CN212125562U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112623132A (en) * | 2020-12-25 | 2021-04-09 | 山东科技大学 | Offshore platform capable of recycling unmanned aerial vehicle |
| CN112874812A (en) * | 2021-03-19 | 2021-06-01 | 山东太古飞机工程有限公司 | Functional reliability testing device for PSU oxygen system of airplane |
| CN113859582A (en) * | 2021-11-30 | 2021-12-31 | 中国飞机强度研究所 | Airplane test freezing fog and freezing rain environment simulation system |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201211 |