CN219039897U - Unmanned aerial vehicle practical training teaching platform - Google Patents
Unmanned aerial vehicle practical training teaching platform Download PDFInfo
- Publication number
- CN219039897U CN219039897U CN202223001359.XU CN202223001359U CN219039897U CN 219039897 U CN219039897 U CN 219039897U CN 202223001359 U CN202223001359 U CN 202223001359U CN 219039897 U CN219039897 U CN 219039897U
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- runway
- aerial vehicle
- unmanned aerial
- take
- 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
Images
Abstract
The utility model discloses an unmanned aerial vehicle practical training teaching platform, which comprises: a first support plate having a first fan disposed therein; one end of the take-off runway is fixedly connected with the first supporting plate; the second supporting plate is internally provided with a second fan, and the other end of the take-off runway is fixedly connected with the second supporting plate; and the protection devices are respectively positioned at two sides of the take-off runway. Through the unmanned aerial vehicle practical training teaching platform disclosed by the utility model, different wind conditions of training can be provided for controlling the unmanned aerial vehicle.
Description
Technical Field
The utility model relates to the technical field of teaching equipment, in particular to an unmanned aerial vehicle practical training teaching platform.
Background
The unmanned aerial vehicle is short for unmanned aerial vehicle, and is mainly operated by wireless remote control equipment and programs in the unmanned aerial vehicle, and a cockpit is not arranged in the unmanned aerial vehicle, but equipment such as an autopilot and a program control device are arranged in the unmanned aerial vehicle, so that the unmanned aerial vehicle can be landed in the same landing mode as that of a common airplane, and can be landed in the modes such as a parachute, a barrier net and the like for remote control.
Training is needed before unmanned aerial vehicle is operated, the unmanned aerial vehicle training teaching demonstration platform can be used in the current unmanned aerial vehicle training, but the current unmanned aerial vehicle training teaching demonstration platform can only carry out single wind condition to take off and land the unmanned aerial vehicle when in use, so that the training effect is reduced. Meanwhile, the existing unmanned aerial vehicle practical training teaching demonstration platform does not have protective equipment, if an unmanned aerial vehicle is in take-off, the unmanned aerial vehicle is easy to fall to the ground due to misoperation, and then the unmanned aerial vehicle is damaged.
Disclosure of Invention
The technical problems to be solved by the utility model are as follows: the unmanned aerial vehicle training teaching platform solves the problem that an existing unmanned aerial vehicle training teaching platform can only perform single wind condition training and does not have protective equipment.
In order to solve the technical problems, the utility model provides the following technical scheme:
an unmanned aerial vehicle practical training teaching platform, comprising:
a first support plate having a first fan disposed therein;
one end of the take-off runway is fixedly connected with the first supporting plate;
the second supporting plate is internally provided with a second fan, and the other end of the take-off runway is fixedly connected with the second supporting plate;
and the protection devices are respectively positioned at two sides of the take-off runway.
In an embodiment of the utility model, the unmanned aerial vehicle training teaching platform further comprises an extension runway, wherein the extension runway is located in the take-off runway, and one end of the extension runway is fixedly connected with the second supporting plate.
In one embodiment of the present utility model, the extended runway includes:
one side of the drawing plate is fixedly connected with the second supporting plate;
the spring is positioned on the drawing plate, and one end of the spring is fixedly connected with the drawing plate;
and the extension plate is fixedly connected with the other end of the spring.
In an embodiment of the utility model, the unmanned aerial vehicle training teaching platform further includes a driving device, and the driving device is located in the second supporting plate, where the driving device includes:
the power device is fixedly connected with the top of the second supporting plate;
one end of the first transmission rod is fixedly connected with the power device;
the sliding sleeve is sleeved on the first transmission rod and is fixedly connected with the shell of the second fan;
and one end of the second transmission rod is fixedly connected with the other end of the first transmission rod.
In an embodiment of the utility model, the driving device further includes:
a rotating rod connected with the bottom of the second supporting plate;
at least rolling wheels which are respectively positioned at two ends of the rotating rod and fixedly connected with the rotating rod, and part of the rolling wheels protrude out of the second supporting plate;
the rotating wheel is positioned between the at least idler wheels and fixedly connected with the rotating rod, and the rotating wheel is also connected with the other end of the second transmission rod.
In one embodiment of the present utility model, the guard includes:
the rotating shafts are fixed at two side edges of the take-off runway;
one end of the connecting rod is movably connected with the rotating shaft,
and the protection net is fixedly connected with the connecting rod.
Compared with the prior art, the utility model has the beneficial effects that:
1. through the second fan, provide "upwind" wind condition for unmanned aerial vehicle seeks wind condition training. The first transmission rod and the second transmission rod are driven to rotate by the power device, the sliding sleeve moves on the first transmission rod, and the sliding sleeve 530 can move upwards or downwards according to different rotating directions of the power device. When the sliding sleeve moves upwards, the second fan is driven to extend out of the top surface of the second supporting plate, and an 'upwind' wind condition is provided for unmanned aerial vehicle wind condition searching training. When the 'upwind' wind condition is not needed, the power device rotates to the other direction, so that the sliding sleeve moves downwards to drive the second fan to retract into the second supporting plate.
2. When avoiding unmanned aerial vehicle "headwind" to take off through extending the runway, strike the second fan, when need control unmanned aerial vehicle and carry out "headwind" training, power device drives first transfer line and second transfer line and rotates, and the slip cap drives the second fan simultaneously and stretches out the second backup pad to and the second driving piece drives the roll through the rotor, and then drives the second backup pad and remove, makes and extends the runway and take out in the runway, extension take off the length of runway.
3. Through setting up protector, in real unmanned aerial vehicle's take off or the in-process that falls, if unmanned aerial vehicle takes place to fall near taking off the runway, the protection network can play the effect of protection to unmanned aerial vehicle this moment, avoids unmanned aerial vehicle to take place to fall when real standard to cause unmanned aerial vehicle's damage.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed for the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic diagram of an unmanned aerial vehicle practical training teaching platform.
Fig. 2 is a schematic diagram of a driving device according to the present utility model.
FIG. 3 is a schematic view of an extended runway according to the present utility model.
Fig. 4 is a schematic view showing the connection of the extension runway and the second support plate according to the present utility model.
Detailed Description
In order to facilitate the understanding of the technical scheme of the present utility model by those skilled in the art, the technical scheme of the present utility model will be further described with reference to the accompanying drawings.
The terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present application, the meaning of "a plurality" is two or more, unless explicitly defined otherwise.
Referring to fig. 1, the present utility model provides an unmanned aerial vehicle training teaching platform, which includes: the first support plate 100, the first fan 210, the second fan 220, the take-off runway 300, the second support plate 400, and the guard 700. The first fan 210 is located in the first support plate 100, the second fan 220 is located in the second support plate 400, the take-off runway 300 is located between the first support plate 100 and the second support plate 400, one end of the take-off runway 300 is fixedly connected with the first support plate 100, and the other end of the take-off runway 300 is fixedly connected with the second support plate 400. By arranging the first fan 210 and the second fan 220 at two ends of the take-off runway 300, the unmanned aerial vehicle training platform is provided with the training of two wind conditions of downwind and upwind. The protection devices 700 are respectively fixed at two sides of the take-off runway 300, and are used for preventing the unmanned aerial vehicle from falling and damaging due to human misoperation when the unmanned aerial vehicle takes off.
Referring to fig. 1, in an embodiment of the present utility model, when the unmanned aerial vehicle takes off on the take-off runway 300, the unmanned aerial vehicle takes off from the position of the first support plate 100 toward the direction of the second support plate 400, that is, the first fan 210 provides the wind condition same as the take-off direction, i.e. "downwind", for the unmanned aerial vehicle wind condition training, and the second fan 220 provides the wind condition opposite to the take-off direction, i.e. "upwind", for the unmanned aerial vehicle wind condition training. Wherein, the top surface of second backup pad 400 is parallel and level with the top surface of runway 300 that takes off, and second fan 220 is located second backup pad 400, and when unmanned aerial vehicle carries out "upwind" and takes off the training, the top surface of second backup pad 400 is protruding to second fan 220, provides "upwind" wind condition for providing unmanned aerial vehicle training. Specifically, the unmanned aerial vehicle practical training teaching platform further comprises a driving device and an extension runway 700.
Referring to fig. 2 and 3, in an embodiment of the present utility model, the driving device includes a power device 510, a first transmission rod 520, a sliding sleeve 530, a second transmission rod 540, a rotating rod 550, a rotating wheel 560, a roller 570 and a telescopic rod 580. Wherein a power unit 510 is fixed to the top of the inside of the second support plate 400 to power the driving unit. The power device 510 is, for example, a motor, one end of the first transmission rod 520 is fixedly connected with the power device 510, and the other end of the first transmission rod 520 is fixedly connected with one end of the second transmission rod 540. The sliding sleeve 530 is sleeved on the first transmission rod 520, and the sliding sleeve 530 is fixedly connected with the housing of the second fan 220, when the power device 510 drives the first transmission rod 520 and the second transmission rod 540 to rotate, the sliding sleeve 530 moves on the first transmission rod 520, and according to different rotation directions of the power device 510, the sliding sleeve 530 can move up or down. When the sliding sleeve 530 moves up, the second fan 220 is driven to extend out of the top surface of the second support plate 400, an 'upwind' wind condition is provided for unmanned aerial vehicle wind finding condition training, and when the 'upwind' wind condition is not needed, the power device 510 rotates in the direction, the sliding sleeve 530 moves down, and the second fan 220 is driven to retract into the second support plate 400. Specifically, the first transmission rod 520 is, for example, a threaded rod, the sliding sleeve 530 is, for example, a threaded sleeve, and the second transmission rod 540 is, for example, a worm. The telescopic rod 580 is located in the second support plate 400, one end of the telescopic rod 580 is fixed in the second support plate 400, the other end of the telescopic rod 580 is fixedly connected with the bottom of the second fan 220 housing, and the telescopic rod 580 provides a supporting function for the second fan 220.
Referring to fig. 2 and 3, in an embodiment of the present utility model, the rotating rod 550 is located in the second support plate 400 and is also located at the bottom of the second support plate 400, and the rotating rod 550 can rotate on the inner side wall of the second support plate 400. The rotating wheels 560 and the rollers 570 are fixedly connected with the transmission rod 550, wherein the number of the rollers 570 is 2, for example, and the rollers 570 are respectively positioned at two ends of the rotating rod 550, and part of the rollers protrude out of the second support plate 400, and when the rotating rod 550 rotates, the rollers 570 are driven to roll, so that the second support plate 400 moves. The rotating wheel 560 is located between the two rollers 570, and the rotating wheel 560 is also connected to the other end of the second transmission lever 540. When the second transmission rod 540 rotates, the rotating wheel 560 is driven to rotate, and when the rotating wheel 560 rotates, the rotating rod 550 is driven to rotate, the rotating rod 550 drives the roller 570 to roll, and then the second support plate 400 is driven to move. Specifically, the rotating wheel 560 is, for example, a turbine, that is, the second transmission rod 540 and the rotating wheel 560 form a worm gear.
Referring to fig. 2 to 4, in an embodiment of the utility model, the unmanned aerial vehicle training platform further includes an extension runway 600, wherein the extension runway 600 is located in the take-off runway 300, and one side of the extension runway is fixedly connected with the second support plate 400. When the unmanned aerial vehicle performs the "upwind" training, the second fan 220 protrudes from the takeoff track 300 and is also located at the opposite side of the takeoff direction of the unmanned aerial vehicle, so as to avoid the collision of the unmanned aerial vehicle with the second fan 220 during the takeoff, and thus the extension runway 600 is provided. The extended runway 600 is located within the takeoff runway 300 when the unmanned aerial vehicle is not "upwind" trained. When the unmanned aerial vehicle needs to be controlled to perform the upwind training, the power device 510 drives the first transmission rod 520 and the second transmission rod 540 to rotate, meanwhile, the sliding sleeve 530 drives the second fan 210 to extend out of the second support plate 400, and the second transmission piece 540 drives the rolling 570 to roll through the rotating wheel 560 and the rotating wheel 560, so that the second support plate 400 is driven to move, the extension runway 600 is pulled out of the take-off runway 300, and the length of the take-off runway 300 is prolonged.
Referring to fig. 2 to 4, in an embodiment of the present utility model, an extension runway 600 includes a pull plate 610, a spring 620 and an extension plate 630. One side of the drawing plate 610 is fixedly connected with the second support plate 400, so that the drawing plate 610 can be drawn out or pushed into the take-off runway 300 when the second support plate 400 moves. One end of the spring 620 is fixedly connected with the drawing plate 610, and the other end of the spring 620 is fixedly connected with the extension plate 630. When the extension runway 600 is withdrawn from the takeoff runway 300, the surface of the extension panel 630 is kept flush with the surface of the takeoff runway 300 due to the characteristics of the springs 620 themselves.
Referring to fig. 1, in an embodiment of the utility model, a protection device 700 includes a rotating shaft 710, a connecting rod 720 and a protection net 730. The number of the rotating shafts 710 is, for example, a plurality of, and they are respectively fixed at both sides of the take-off runway 300. The connecting rod 720 is movably connected with the rotating shaft 710, so that the connecting rod 720 is unfolded at right angles by taking the rotating shaft 710 as a round point. Two rotating shafts 710 are arranged on one side of the take-off runway 300, and each rotating shaft 710 is movably connected with a corresponding connecting rod 720. The both ends of protection network 730 respectively with connecting rod 720 fixed connection, when connecting rod 720 is opened to the one side that keeps away from runway 300 that takes off, make protection network 730 strut, prevent that unmanned aerial vehicle from taking off, drop and break. When the unmanned aerial vehicle training teaching platform is not in use, the connecting rod 720 is closed to the side close to the take-off runway 300, and the protective net 730 is recovered.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein.
The above-described embodiments merely represent embodiments of the utility model, the scope of the utility model is not limited to the above-described embodiments, and it is obvious to those skilled in the art that several variations and modifications can be made without departing from the spirit of the utility model, which are all within the scope of the utility model.
Claims (6)
1. Unmanned aerial vehicle instructs teaching platform in fact, a serial communication port includes:
a first support plate having a first fan disposed therein;
one end of the take-off runway is fixedly connected with the first supporting plate;
the second supporting plate is internally provided with a second fan, and the other end of the take-off runway is fixedly connected with the second supporting plate;
and the protection devices are respectively positioned at two sides of the take-off runway.
2. The unmanned aerial vehicle practical training teaching platform according to claim 1, further comprising an extension runway, wherein the extension runway is located in the take-off runway, and one end of the extension runway is fixedly connected with the second supporting plate.
3. The unmanned aerial vehicle practical training teaching platform of claim 2, wherein the extended runway comprises:
one side of the drawing plate is fixedly connected with the second supporting plate;
the spring is positioned on the drawing plate, and one end of the spring is fixedly connected with the drawing plate;
and the extension plate is fixedly connected with the other end of the spring.
4. The unmanned aerial vehicle practical training teaching platform of claim 1, further comprising a driving device, the driving device being located in the second support plate, wherein the driving device comprises:
the power device is fixedly connected with the top of the second supporting plate;
one end of the first transmission rod is fixedly connected with the power device;
the sliding sleeve is sleeved on the first transmission rod and is fixedly connected with the shell of the second fan;
and one end of the second transmission rod is fixedly connected with the other end of the first transmission rod.
5. The unmanned aerial vehicle practical training teaching platform of claim 4, wherein the driving means further comprises:
a rotating rod connected with the bottom of the second supporting plate;
at least rolling wheels which are respectively positioned at two ends of the rotating rod and fixedly connected with the rotating rod, and part of the rolling wheels protrude out of the second supporting plate;
the rotating wheel is positioned between the at least idler wheels and fixedly connected with the rotating rod, and the rotating wheel is also connected with the other end of the second transmission rod.
6. The unmanned aerial vehicle practical training teaching platform of claim 1, wherein the protective device comprises:
the rotating shafts are fixed at two side edges of the take-off runway;
one end of the connecting rod is movably connected with the rotating shaft,
and the protection net is fixedly connected with the connecting rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223001359.XU CN219039897U (en) | 2022-11-10 | 2022-11-10 | Unmanned aerial vehicle practical training teaching platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223001359.XU CN219039897U (en) | 2022-11-10 | 2022-11-10 | Unmanned aerial vehicle practical training teaching platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219039897U true CN219039897U (en) | 2023-05-16 |
Family
ID=86288984
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223001359.XU Active CN219039897U (en) | 2022-11-10 | 2022-11-10 | Unmanned aerial vehicle practical training teaching platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219039897U (en) |
-
2022
- 2022-11-10 CN CN202223001359.XU patent/CN219039897U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104369635A (en) | Air-ground amphibious vehicle | |
| CN112278310B (en) | Automatic lifting and retracting mechanism for tethered rotor wing and use method thereof | |
| CN112467668B (en) | Aerial cable is with clean deicing unmanned aerial vehicle | |
| CN107528281B (en) | Wire deicing system for high-voltage power transmission and transformation project | |
| CN112874758B (en) | Film wing aircraft | |
| CN108706095B (en) | Be suitable for miniature many rotor unmanned aerial vehicle that has buffer stop that channel patrolled and examined | |
| CN205565512U (en) | Multi -functional large -scale transmission line of wireless communication formula overhauls device | |
| CN219039897U (en) | Unmanned aerial vehicle practical training teaching platform | |
| CN210681182U (en) | Composite wing unmanned aerial vehicle shuts down strorage device | |
| CN204172626U (en) | A kind of air-ground amphibious vehicle | |
| CN213168519U (en) | Air-ground dual-purpose unmanned aerial vehicle | |
| CN206407111U (en) | A kind of contraction type depopulated helicopter undercarriage | |
| CN211996120U (en) | Four-wing unmanned aerial vehicle buffering undercarriage | |
| CN212829062U (en) | VTOL aerial survey unmanned aerial vehicle | |
| EP3276163B1 (en) | Device for generating electric power using a high wind turbine | |
| CN109305351B (en) | Independent retractable type hanging rotor unmanned aerial vehicle | |
| CN105752766A (en) | Cable winding and unwinding device based on cable arrangement by motors | |
| CN210149580U (en) | Composite wing unmanned aerial vehicle stop device | |
| CN211642588U (en) | Four-rotor aircraft | |
| CN112849408A (en) | Intelligent unmanned aerial vehicle used for wind power generation and capable of sowing | |
| CN207782288U (en) | Sliding equipment applied to unmanned plane | |
| RU2485016C1 (en) | Bogdanov's device for carrier lifting and transfer | |
| CN217754138U (en) | Stable form unmanned aerial vehicle machine nest | |
| KR101220990B1 (en) | Power supply system of electric aircraft using rotating power supply line | |
| CN201356982Y (en) | Remote control model airplane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |