CN211108028U - Unmanned aerial vehicle aircraft bonnet - Google Patents
Unmanned aerial vehicle aircraft bonnet Download PDFInfo
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- CN211108028U CN211108028U CN201922261425.9U CN201922261425U CN211108028U CN 211108028 U CN211108028 U CN 211108028U CN 201922261425 U CN201922261425 U CN 201922261425U CN 211108028 U CN211108028 U CN 211108028U
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- flame retardant
- unmanned aerial
- aerial vehicle
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- hood
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Abstract
The utility model discloses an unmanned aerial vehicle aircraft bonnet, include: the flame retardant hood comprises a flame retardant hood body and four connecting through holes arranged on the periphery of the outer wall of the flame retardant hood body; a GPS positioning antenna arranged at the middle position of the upper surface of the flame retardant hood; a waterproof ceiling disposed above the flame retardant housing, and a spring mechanism mounted between the waterproof ceiling and the flame retardant housing; the four undercarriage bodies are arranged below the flame-retardant hood, and buffering support legs are arranged below the undercarriage bodies; the propeller supporting rod is arranged inside the connecting through hole, and a propeller mounting notch is formed in the propeller supporting rod. It has realized good water-proof effects for unmanned aerial vehicle also can normally operate in the rainy day.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to unmanned aerial vehicle aircraft bonnet.
Background
An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. 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 in 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, disaster relief and the like, and the application of the unmanned aerial vehicle is greatly expanded. Unmanned aerial vehicle aircraft bonnet refers to the device that protects unmanned aerial vehicle from damage with the material of different materials. However, the waterproof performance of present unmanned aerial vehicle aircraft bonnet is general, does not have waterproof sealing member especially in the junction, and the operation has the risk of short circuit in the rain.
The canopy is the building assembly who is used for keeping off the rain, keeps out the wind, prevents that high altitude junk from smashing and hurting in building access & exit or top balcony top, and the sealing washer is the connecting piece commonly used that seals up to the junction, therefore, if combine together canopy, sealing washer and unmanned aerial vehicle aircraft bonnet, will make the aircraft bonnet have good water-proof effects for unmanned aerial vehicle also can normal work in rainy day, has profound meaning.
SUMMERY OF THE UTILITY MODEL
It is an object of the present invention to solve at least the above problems and to provide at least the advantages which will be described later.
The utility model discloses still another purpose provides the unmanned aerial vehicle aircraft bonnet, has realized good water-proof effects for unmanned aerial vehicle also can normally operate in rainy day.
In order to achieve the above and other objects, the present invention adopts the following technical solutions:
unmanned aerial vehicle aircraft bonnet includes:
the flame retardant hood comprises a flame retardant hood body and four connecting through holes arranged on the periphery of the outer wall of the flame retardant hood body;
a GPS positioning antenna arranged at the middle position of the upper surface of the flame retardant hood;
a waterproof ceiling disposed above the flame retardant housing, and a spring mechanism mounted between the waterproof ceiling and the flame retardant housing;
the four undercarriage bodies are arranged below the flame-retardant hood, and buffering support legs are arranged below the undercarriage bodies;
the propeller strut is arranged inside the connecting through hole, and a propeller mounting notch is formed in the propeller strut;
preferably, in the unmanned aerial vehicle aircraft bonnet, four spring mechanism are provided, and four spring mechanism's both ends all are provided with the spring fixing base, spring mechanism's both ends pass through the spring fixing base respectively with fire-retardant aircraft bonnet with waterproof ceiling fixed connection.
Preferably, in the unmanned aerial vehicle aircraft bonnet, be provided with the diversion channel on the outer wall of waterproof ceiling, just the diversion channel is provided with four.
Preferably, in the unmanned aerial vehicle aircraft bonnet, the screw branch with connect the hole's junction installs rubber seal, just rubber seal and screw branch interference fit.
Preferably, in the unmanned aerial vehicle aircraft bonnet, the below of fire-retardant aircraft bonnet is provided with cloud platform protection casing, be provided with the camera on the preceding terminal surface of cloud platform protection casing and shoot the hole.
Preferably, in the unmanned aerial vehicle aircraft bonnet, be provided with the fixed plate on the outer wall of cloud platform protective housing, just the fixed plate with cloud platform protective housing structure as an organic whole, the fixed plate pass through the screw with fire-retardant aircraft bonnet threaded connection.
Preferably, in the unmanned aerial vehicle aircraft bonnet, fire-retardant aircraft bonnet with the lower surface of cloud platform protection casing all is provided with the louvre, just the louvre is provided with a plurality of.
The utility model discloses at least, include following beneficial effect:
the utility model discloses an among the unmanned aerial vehicle aircraft bonnet, through setting up waterproof ceiling, waterproof ceiling has the effect of waterproof keeping off the rain, make unmanned aerial vehicle can operate in the rain, and be provided with four diversion channels on waterproof ceiling and the outer wall, can be with rainwater drainage to the outside of device when raining, avoid top ponding, aggravate unmanned aerial vehicle weight, influence its effect in the rainy day operation, furthermore, rubber seal is installed with the through hole department of being connected of screw branch to the aircraft bonnet, rubber seal has certain elastic expansion, can strengthen the leakproofness of junction, and closely laminate with screw branch, avoid the rainwater from the seam crossing seepage, lead to the short circuit of unmanned aerial vehicle inner line, the waterproof performance of aircraft bonnet has further been improved.
Through set up spring mechanism between waterproof ceiling and flame retardant engine cover, when unmanned aerial vehicle accident turned on one's side, the supporting component can be regarded as to waterproof ceiling, propped up unmanned aerial vehicle again, and carries out certain buffering through the spring mechanism of junction, protects the inside hardware of unmanned aerial vehicle not to receive the damage.
Through setting up the main casing body of fire-retardant aircraft bonnet as the unmanned aerial vehicle aircraft bonnet, can slow down the burning rate of casing when the short circuit burning of unmanned aerial vehicle inner line, give the rescue time, the loss is reduced to the at utmost.
Additional advantages, objects, and features of the invention will be set forth in part in the description which follows and in part will become apparent to those having ordinary skill in the art upon examination of the following or may be learned from practice of the invention.
Drawings
Fig. 1 is the utility model provides a structural schematic of unmanned aerial vehicle aircraft bonnet.
Fig. 2 is the utility model provides a side structure schematic diagram of unmanned aerial vehicle aircraft bonnet.
Fig. 3 is the utility model provides an unmanned aerial vehicle aircraft bonnet's bottom view structure schematic diagram.
Detailed Description
The present invention is described in detail below with reference to the attached drawings so that those skilled in the art can implement the invention by referring to the description.
As shown in fig. 1-3, a drone bonnet comprising: the flame retardant hood comprises a flame retardant hood body 1 and four connecting through holes 4 arranged on the periphery of the outer wall of the flame retardant hood body 1, wherein the number of the connecting through holes 4 is four.
And a GPS positioning antenna 10 arranged at the middle position of the upper surface of the flame retardant housing 1.
And a waterproof ceiling 2 which is arranged above the flame retardant hood 1, and a spring mechanism 8 is installed between the waterproof ceiling 2 and the flame retardant hood 1.
And four landing gears 15 arranged below the flame retardant hood 1, wherein buffering support legs 16 are arranged below the landing gears 15.
And the propeller supporting rod 5 is arranged inside the connecting through hole 4, and a propeller mounting notch 7 is formed in the propeller supporting rod 5.
In the above scheme, adopt fire-retardant aircraft bonnet as the main casing body of unmanned aerial vehicle aircraft bonnet, can slow down the burning rate of casing when the short circuit burning of unmanned aerial vehicle inner line, give rescue time, the loss is reduced to the at utmost, four diversion channels that set up on waterproof ceiling and the outer wall can be when raining, with rainwater drainage extremely the outside of device is avoided the top ponding of device influences rainy day operation work, adopts spring mechanism to connect between waterproof ceiling and the fire-retardant aircraft bonnet, and when unmanned aerial vehicle accident turned on one's side, the waterproof ceiling can regard as the support component, props up unmanned aerial vehicle, and carries out certain buffering through spring mechanism, and protection inside hardware does not receive the damage.
In a preferred scheme, four spring mechanisms 8 are arranged, two ends of each spring mechanism 8 are provided with spring fixing seats 9, and two ends of each spring mechanism 8 are respectively fixedly connected with the flame retardant hood 1 and the waterproof ceiling 2 through the spring fixing seats 9.
In the above scheme, the spring fixing seat plays a role in fixing the two ends of the spring mechanism on the flame retardant engine cover and the waterproof ceiling respectively, so that the spring mechanism can more stably realize damping work, and the spring fixing seat can be fixed with the flame retardant engine cover and the waterproof ceiling in a threaded mounting mode, so that the spring fixing seat is convenient to disassemble and assemble.
In a preferred scheme, the outer wall of the waterproof ceiling 2 is provided with four water guide grooves 3, and the number of the water guide grooves 3 is four.
In above-mentioned scheme, the diversion channel on the waterproof ceiling can be when raining with the rainwater drainage at top extremely the outside of device avoids top ponding, aggravates unmanned aerial vehicle weight, influences its effect at the rainy day operation.
In a preferred scheme, a rubber sealing ring 6 is installed at the joint of the propeller support rod 5 and the connecting through hole 4, and the rubber sealing ring 6 is in interference fit with the propeller support rod 5.
In above-mentioned scheme, rubber seal has certain elastic scalability, can strengthen the leakproofness of screw branch and connect the via hole junction, closely laminates with screw branch, avoids the rainwater from the seam crossing seepage, leads to unmanned aerial vehicle inner line short circuit.
In a preferred scheme, a cradle head protective casing 13 is arranged below the flame retardant casing 1, and a camera shooting hole 14 is arranged on the front end face of the cradle head protective casing 13.
In the above scheme, the cloud platform protection casing can effectively protect inside cloud platform not receive external direct impact, has prolonged the life of cloud platform, and the camera shooting hole on the terminal surface can expose the camera of cloud platform camera before the cloud platform protection casing, is convenient for shoot the operation.
In a preferred scheme, a fixing plate 11 is arranged on the outer wall of the cradle head protective casing 13, the fixing plate 11 and the cradle head protective casing 13 are of an integral structure, and the fixing plate 11 is in threaded connection with the flame retardant housing 1 through a screw 12.
In the above scheme, the fixed plate has played and has fixed the effect in flame retardant housing bottom with cloud platform protection casing, and the fixed plate passes through screw and flame retardant housing threaded connection, the dismouting of being convenient for to regularly overhaul work to the inside cloud platform equipment of unmanned aerial vehicle.
In a preferred scheme, the lower surfaces of the flame retardant hood 1 and the pan/tilt head protection casing 13 are provided with a plurality of heat dissipation holes 17, and the heat dissipation holes 17 are provided with a plurality of heat dissipation holes.
In the above scheme, the louvre can play for the radiating effect of fire-retardant aircraft bonnet and cloud platform protection casing internal component, and the louvre is provided with a plurality of, can effectively promote the radiating effect, avoids the not good risk that leads to the internal component damage of heat dissipation, has prolonged aircraft bonnet internal component's life.
While the embodiments of the invention have been described above, it is not intended to be limited to the details shown, or described, but rather to cover all modifications, which would come within the scope of the invention, as defined by the claims and the equivalents thereof, and which fall within the limits of the claims and the equivalents thereof.
Claims (7)
1. Unmanned aerial vehicle aircraft bonnet, its characterized in that includes:
the flame retardant hood comprises a flame retardant hood body and four connecting through holes arranged on the periphery of the outer wall of the flame retardant hood body;
a GPS positioning antenna arranged at the middle position of the upper surface of the flame retardant hood;
a waterproof ceiling disposed above the flame retardant housing, and a spring mechanism mounted between the waterproof ceiling and the flame retardant housing;
the four undercarriage bodies are arranged below the flame-retardant hood, and buffering support legs are arranged below the undercarriage bodies;
the propeller supporting rod is arranged inside the connecting through hole, and a propeller mounting notch is formed in the propeller supporting rod.
2. The unmanned aerial vehicle hood of claim 1, wherein there are four spring mechanisms, and spring holders are provided at both ends of the four spring mechanisms, and both ends of the spring mechanisms are respectively fixedly connected with the flame retardant hood and the waterproof ceiling through the spring holders.
3. The unmanned aerial vehicle bonnet as defined in claim 1, wherein there are four water gutters provided on an outer wall of the waterproof ceiling.
4. The unmanned aerial vehicle aircraft bonnet of claim 1, wherein the rubber seal is installed to the screw branch with the junction of connect the through-hole, and the rubber seal is with screw branch interference fit.
5. The unmanned aerial vehicle aircraft bonnet of claim 1, wherein a pan-tilt protection casing is disposed below the flame retardant bonnet, and a camera shooting hole is disposed on a front end surface of the pan-tilt protection casing.
6. The unmanned aerial vehicle aircraft bonnet of claim 5, wherein a fixed plate is arranged on the outer wall of the cradle head protection casing, and the fixed plate and the cradle head protection casing are of an integral structure, and the fixed plate is in threaded connection with the flame retardant bonnet through a screw.
7. The unmanned aerial vehicle aircraft bonnet as defined in claim 5, wherein the lower surfaces of flame retardant bonnet and pan/tilt head protection casing are each provided with a plurality of cooling holes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922261425.9U CN211108028U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle aircraft bonnet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922261425.9U CN211108028U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle aircraft bonnet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211108028U true CN211108028U (en) | 2020-07-28 |
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ID=71691933
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922261425.9U Active CN211108028U (en) | 2019-12-04 | 2019-12-04 | Unmanned aerial vehicle aircraft bonnet |
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| Country | Link |
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| CN (1) | CN211108028U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112623208A (en) * | 2021-01-07 | 2021-04-09 | 淮北九天测绘股份有限公司 | Unmanned aerial vehicle for aerial photography |
-
2019
- 2019-12-04 CN CN201922261425.9U patent/CN211108028U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112623208A (en) * | 2021-01-07 | 2021-04-09 | 淮北九天测绘股份有限公司 | Unmanned aerial vehicle for aerial photography |
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