CN210488890U - Unmanned aerial vehicle patrols and examines skill training set - Google Patents
Unmanned aerial vehicle patrols and examines skill training set Download PDFInfo
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- CN210488890U CN210488890U CN201921653776.8U CN201921653776U CN210488890U CN 210488890 U CN210488890 U CN 210488890U CN 201921653776 U CN201921653776 U CN 201921653776U CN 210488890 U CN210488890 U CN 210488890U
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Abstract
The utility model provides an unmanned aerial vehicle patrols and examines skill training set, including host computer, display mechanism, flight control box and operating device, flight control box includes square casing, sets up the extension board in the casing and sets up the cooling mechanism above the extension board, cooling mechanism includes the cooling duct that hugs closely the casing inside wall, the cooling duct is equipped with a plurality of cooling mouths at the medial surface, and the cooling duct is equipped with the vent in the outside of two sides of the relative one side of casing, is connected with the fan on one of them vent; the utility model discloses a fly to control the box and protect the flight control machine, like this because the unexpected condition leads to the desktop to vibrate, the inside precision component of protection flight control machine can also be cooled down to the inside wind-force that continuously provides of cooling duct through the fan to the flight control machine, then takes out the heat from another vent to continuously cool down the flight control machine, make the flight control machine guarantee that the temperature can not be too high when long-term operation, further protect inside component not to damage.
Description
Technical Field
The utility model relates to an electric power facility equipment technical field, concretely relates to device that technical training was carried out for unmanned aerial vehicle patrols and examines.
Background
Under the background that unmanned aerial vehicle extensively was applicable to the electric wire netting operation and maintenance work, the operation level and the standardization that promote unmanned aerial vehicle energetically are imperative, and many rotor unmanned aerial vehicle electric wire netting inspection skill simulation training system based on 3D physical engine accords with the requirement and the trend of current technical innovation.
The multi-rotor unmanned aerial vehicle power grid inspection skill simulation training system based on the 3D physical engine combines a multi-rotor unmanned aerial vehicle working theory, a virtual reality technology and a system simulation technology, can be applied to multi-rotor unmanned aerial vehicle skill training of power grid inspection (or collective and individual), is virtual realization of actual multi-rotor unmanned aerial vehicle training and operation processes on a computer, and has the characteristics of prominent space immersion and high simulation. The system can concentrate real multi-rotor unmanned aerial vehicles and power transmission lines in longitudinal and transverse Wolff fields on a computer screen, virtual operation, breakthrough training, subject examination and power transmission line environment flying inspection are carried out through real flight control, real resources and energy are not consumed, safety and high efficiency in the training process are guaranteed, training and evaluation requirements of the multi-rotor unmanned aerial vehicles are met, and the purpose of improving the skill level of training technicians is achieved.
But current unmanned aerial vehicle patrols and examines skill training set still has certain problem, mainly is in the use aspect of flight control, and current flight control machine is generally directly placed beside the host computer, but in the in-service use process, because contain a large amount of accurate components in the flight control machine, factors such as desktop collision may damage the flight control box, and the temperature is too high after the flight control machine is operated for a long time simultaneously, also can damage interior component.
SUMMERY OF THE UTILITY MODEL
Not enough to exist among the prior art, the utility model provides an unmanned aerial vehicle patrols and examines skill training set for solve current unmanned aerial vehicle and patrol and examine skill training set and probably lead to flying to control the box and receive the collision damage when using, perhaps the high problem that leads to damaging of temperature.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
an unmanned aerial vehicle inspection skill training device comprises a host, a display mechanism, a flight control box and an operating mechanism, wherein the host is connected with the display mechanism through an HDMI (high-definition multimedia interface) connecting wire, the host is connected with the flight control box through a USB (universal serial bus) connecting wire, and the host is connected with the operating mechanism through a USB connecting wire, Bluetooth or wifi (wireless fidelity);
the flight control box comprises a square shell, a support plate arranged inside the shell and a cooling mechanism arranged above the support plate, wherein the cooling mechanism comprises a cooling air channel tightly attached to the inner side wall of the shell, the cooling air channel is provided with a plurality of cooling ports on the inner side surface, the cooling air channel is provided with ventilation ports on the outer portions of two sides of one surface, opposite to the shell, of the shell, and one ventilation port is connected with a fan.
Compared with the prior art, the utility model discloses following beneficial effect has:
1. the utility model protects the flight control machine through the flight control box, so that the desktop vibrates due to accidents, and when other articles collide, the collision force can be borne by the shell, thereby avoiding the direct stress of the flight control machine and protecting the precise elements in the flight control machine;
2. the utility model discloses an inside cooling duct that still is equipped with of casing can be to the inside wind-force that continuously provides of cooling duct through the fan, and cold wind cools down the accuse machine that flies through the cooling mouth at the in-process that blows through cooling duct, then takes the heat out from another vent to continuously cool down to flying the accuse machine, make flying the accuse machine guarantee that the temperature can not be too high when long-term operation, further protect inside component not to damage.
Drawings
FIG. 1 is a view of the overall structure of the present invention;
fig. 2 is a top cross-sectional view of the flight control box of the present invention;
in the figure: host computer 1, VR glasses 2, flight control box 3, operating handle 4, cooling duct 31, vent 32, cooling hole 33, preforming 34, spring 35, fan 36.
Detailed Description
The technical solution of the present invention will be further explained with reference to the accompanying drawings and embodiments.
Example (b):
as shown in fig. 1 and 2, the utility model provides an unmanned aerial vehicle patrols and examines skill training set, including host computer 1, display mechanism, fly to control box 3 and operating device, wherein host computer 1 passes through the HDMI connecting wire with display mechanism and is connected, and host computer 1 passes through the USB connecting wire with flying to control box 3 and is connected, is connected through USB connecting wire, bluetooth or wifi between host computer 1 and the operating device. Wherein, display mechanism includes display, projector and VRVR glasses 2 etc. and operating device includes operating handle 4 or operation panel, adopts VRVR glasses 2 as display mechanism in this embodiment to cooperation operating handle 4 is as operating device, and wherein operating handle 4 passes through the USB connecting wire and is connected with host computer 1, thereby carries out human-computer interaction.
The flight control box 3 comprises a square shell, a support plate arranged inside the shell and a cooling mechanism arranged above the support plate, a flight control machine is placed in the flight control box 3, a USB (universal serial bus) connector of the flight control machine is located at the top, and therefore the flight control machine can be connected with the host machine 1 through a USB connecting wire after being placed inside the flight control box 3. The cooling mechanism comprises a cooling air duct 31 tightly attached to the inner side wall of the shell, the cooling air duct 31 is provided with a plurality of cooling openings 33 on the inner side surface, the cooling air duct 31 is provided with ventilation openings 32 on the outer portions of two side surfaces of the opposite surface of the shell, and one ventilation opening 32 is connected with a fan 36. Can continuously provide wind-force to cooling duct 31 is inside through fan 36, and cold wind is cooled down the accuse machine through cooling mouth 33 at the in-process that blows cooling duct 31, then takes the heat out from another vent 32 to continuously cool down the accuse machine of flying, make the accuse machine of flying guarantee the temperature can not be too high when long-term operation, further protect inside component not to damage. In this embodiment, the height of the casing above the supporting plate is greater than the height of the flight control box 3, and the height of the corresponding cooling air duct 31 is greater than the height of the flight control machine, so that the side face of the flight control machine is completely covered, and the cooling effect is ensured.
In the preferred scheme of this embodiment, two sides that do not set up vent 32 in the casing are equipped with symmetrical hold-down mechanism, hold-down mechanism includes two preforming 34 that are parallel to each other, preforming 34 is fixed at the casing inboard by spring 35, and when the size of flight control machine is less than the inside size of flight control box 3, accessible preforming 34 fixes the flight control machine, guarantees that it can not take place to rock, avoids damaging. In the further preferred scheme of this embodiment, still be provided with sponge shock attenuation board between extension board and the interior bottom surface of casing to carry out the shock attenuation to the bottom of flight control machine, play better protection effect.
Finally, although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that the present invention can be modified or replaced by other means without departing from the spirit and scope of the present invention, which should be construed as limited only by the appended claims.
Claims (6)
1. The utility model provides an unmanned aerial vehicle patrols and examines skill training set which characterized in that: the intelligent display device comprises a host, a display mechanism, a flight control box and an operating mechanism, wherein the host is connected with the display mechanism through an HDMI (high-definition multimedia interface) connecting line, the host is connected with the flight control box through a USB (universal serial bus) connecting line, and the host is connected with the operating mechanism through a USB connecting line, Bluetooth or wifi;
the flight control box comprises a square shell, a support plate arranged inside the shell and a cooling mechanism arranged above the support plate, the flight control box is internally provided with a flight control machine, the cooling mechanism comprises a cooling air duct tightly attached to the inner side wall of the shell, the cooling air duct is provided with a plurality of cooling ports on the inner side surface, the cooling air duct is provided with ventilation openings on the outer portions of two side surfaces of one opposite surface of the shell, and one ventilation opening is connected with a fan.
2. The unmanned aerial vehicle inspection skill training device of claim 1, wherein: the height of the shell above the support plate is larger than that of the flight control box used.
3. The unmanned aerial vehicle inspection skill training device of claim 1, wherein: and symmetrical pressing mechanisms are arranged on two sides of the interior of the shell, which are not provided with the ventilation openings, each pressing mechanism comprises two pressing sheets which are parallel to each other, and the pressing sheets are fixed on the inner side of the shell by springs.
4. The unmanned aerial vehicle inspection skill training device of claim 1, wherein: the display mechanism includes a display, a projector, and VR glasses.
5. The unmanned aerial vehicle inspection skill training device of claim 1, wherein: the operating mechanism comprises an operating handle or an operating platform.
6. The unmanned aerial vehicle inspection skill training device of claim 1, wherein: a sponge damping plate is further arranged between the support plate and the inner bottom surface of the shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921653776.8U CN210488890U (en) | 2019-09-30 | 2019-09-30 | Unmanned aerial vehicle patrols and examines skill training set |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921653776.8U CN210488890U (en) | 2019-09-30 | 2019-09-30 | Unmanned aerial vehicle patrols and examines skill training set |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210488890U true CN210488890U (en) | 2020-05-08 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921653776.8U Expired - Fee Related CN210488890U (en) | 2019-09-30 | 2019-09-30 | Unmanned aerial vehicle patrols and examines skill training set |
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| Country | Link |
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| CN (1) | CN210488890U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114035608A (en) * | 2021-11-10 | 2022-02-11 | 广东电网能源发展有限公司 | Unmanned aerial vehicle-based inspection training method and system, training terminal and storage medium |
-
2019
- 2019-09-30 CN CN201921653776.8U patent/CN210488890U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114035608A (en) * | 2021-11-10 | 2022-02-11 | 广东电网能源发展有限公司 | Unmanned aerial vehicle-based inspection training method and system, training terminal and storage medium |
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Legal Events
| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200508 Termination date: 20200930 |
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| CF01 | Termination of patent right due to non-payment of annual fee |