CN214930596U - Scalable shooting unmanned aerial vehicle - Google Patents
Scalable shooting unmanned aerial vehicle Download PDFInfo
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- CN214930596U CN214930596U CN202120721897.2U CN202120721897U CN214930596U CN 214930596 U CN214930596 U CN 214930596U CN 202120721897 U CN202120721897 U CN 202120721897U CN 214930596 U CN214930596 U CN 214930596U
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Abstract
The utility model belongs to the technical field of the unmanned air vehicle technique and specifically relates to indicate a scalable shooting unmanned aerial vehicle, it includes the unmanned aerial vehicle body, scalable wing bracing piece, the screw, surveillance camera head, a machine support, protection component and waterproof component, the scalable wing bracing piece of lateral wall symmetry fixedly connected with all around of unmanned aerial vehicle body, the end and the screw fixed connection of scalable wing bracing piece, the bottom of unmanned aerial vehicle body respectively with frame and surveillance camera head fixed connection, surveillance camera head is located between the frame, the top and the protection component fixed connection of unmanned aerial vehicle body, scalable wing bracing piece includes the dead lever, telescopic link and lock pearl fixed connection, the through-hole has been seted up to the side of dead lever, dead lever and telescopic link are worn to locate the through-hole fixedly through the lock pearl, waterproof component and dead lever fixed connection. The utility model provides a scalable unmanned aerial vehicle that shoots is convenient for accomodate, and protective capacities is strong, and waterproof performance is good simultaneously.
Description
Technical Field
The utility model belongs to the technical field of the unmanned air vehicle technique and specifically relates to indicate a scalable unmanned aerial vehicle of shooing.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", 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 + the industry application 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. Although the scalable unmanned aerial vehicle of shooing that uses at present can also realize the shrink and accomodate, nevertheless be not convenient for waterproof, protective capacities is not enough simultaneously.
Disclosure of Invention
The to-be-solved technical problem of the utility model is to provide a scalable shooting unmanned aerial vehicle, this scalable shooting unmanned aerial vehicle is convenient for accomodate, and protective capacities is strong, and waterproof performance is good simultaneously.
In order to solve the technical problem, the utility model discloses a following technical scheme:
a retractable shooting unmanned aerial vehicle comprises an unmanned aerial vehicle body, retractable wing supporting rods, propellers, a monitoring camera, a rack, a protective component and a waterproof component, wherein the retractable wing supporting rods are symmetrically and fixedly connected with the peripheral side wall of the unmanned aerial vehicle body, the tail ends of the retractable wing supporting rods are fixedly connected with the propellers, the bottom of the unmanned aerial vehicle body is respectively fixedly connected with the rack and the monitoring camera, the monitoring camera is positioned between the racks, the top of the unmanned aerial vehicle body is fixedly connected with the protective component, the retractable wing supporting rods comprise fixing rods, retractable rods and locking beads, the retractable rods are fixedly connected with the locking beads, through holes are formed in the side faces of the fixing rods, the fixing rods and the retractable rods are fixedly arranged in the through holes through the locking beads, the waterproof component is fixedly connected with the fixing rods, the waterproof component is positioned under the through holes, the waterproof component can be covered on the through holes, and a storage battery and a control host are arranged in the unmanned aerial vehicle body, the propeller, the monitoring camera and the storage battery are all electrically connected with the control host.
Further, waterproof assembly includes connecting block and buckler, connecting block and buckler fixed connection, the through-hole is located to the buckler.
Further, the protection component includes bumper shock absorber and guard plate, bumper shock absorber and guard plate fixed connection, the guard plate is located the top of unmanned aerial vehicle body.
Further, the bumper shock absorber includes mount pad, spring and lower mount pad, go up the top of mount pad and the bottom fixed connection of guard plate, the bottom of mount pad and the top fixed connection of unmanned aerial vehicle body down, the both ends of spring respectively with the bottom of last mount pad and the top fixed connection of mount pad down.
Further, a handle is arranged at the top of the protection plate.
The utility model has the advantages that: during the in-service use, scalable wing bracing piece is used for the device of erection joint, the screw is used for supporting the unmanned aerial vehicle body and flies, the surveillance camera head is used for carrying out the surveillance camera, the frame is used for supporting the unmanned aerial vehicle body, the protection subassembly is used for protecting the shock attenuation to the unmanned aerial vehicle body, the telescopic link can slide in the inside of dead lever, and wear to locate the through-hole through the lock pearl and fix, waterproof assembly is used for carrying out waterproofly to the through-hole, through-hole when need not use is waterproof, open waterproof assembly when the through-hole that needs used. The utility model provides a scalable unmanned aerial vehicle that shoots is convenient for accomodate, and protective capacities is strong, and waterproof performance is good simultaneously.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Description of reference numerals: unmanned aerial vehicle body 1, scalable wing bracing piece 2, dead lever 21, through-hole 211, telescopic link 22, lock pearl 23, screw 3, surveillance camera head 4, frame 5, protection component 6, bumper shock absorber 61, go up mount pad 611, spring 612, mount pad 613 down, guard plate 62, handle 621, waterproof component 7, connecting block 71, buckler 72.
Detailed Description
In order to facilitate understanding of those skilled in the art, the present invention will be further described with reference to the following examples and drawings, which are not intended to limit the present invention.
As shown in fig. 1, the utility model provides a retractable shooting unmanned aerial vehicle, which comprises an unmanned aerial vehicle body 1, a retractable wing support rod 2, a propeller 3, a monitoring camera 4, a frame 5, a protection component 6 and a waterproof component 7, wherein the peripheral side wall of the unmanned aerial vehicle body 1 is symmetrically and fixedly connected with the retractable wing support rod 2, the end of the retractable wing support rod 2 is fixedly connected with the propeller 3, the bottom of the unmanned aerial vehicle body 1 is fixedly connected with the frame 5 and the monitoring camera 4 respectively, the monitoring camera 4 is positioned between the frame 5, the top of the unmanned aerial vehicle body 1 is fixedly connected with the protection component 6, the retractable wing support rod 2 comprises a fixing rod 21, a retractable rod 22 and a locking bead 23, the retractable rod 22 is fixedly connected with the locking bead 23, the side surface of the fixing rod 21 is provided with a through hole 211, the fixing rod 21 and the retractable rod 22 are fixed through the locking bead 23, waterproof component 7 and dead lever 21 fixed connection, waterproof component 7 are located through-hole 211 under, and waterproof component 7 can cover and locate through-hole 211, and the inside of unmanned aerial vehicle body 1 is provided with battery and main control system, and screw 3, surveillance camera head 4 and battery all are connected with the main control system electricity.
During the in-service use, scalable wing bracing piece 2 is used for the device of erection joint, screw 3 is used for supporting unmanned aerial vehicle body 1 and flies, surveillance camera head 4 is used for monitoring and camera shooting, frame 5 is used for supporting unmanned aerial vehicle body 1, protection component 6 is used for protecting the shock attenuation to unmanned aerial vehicle body 1, telescopic link 22 can slide in the inside of dead lever 21, and wear to locate through-hole 211 through lock pearl 23 and fix, waterproof component 7 is used for preventing water through-hole 211, through-hole 211 that need not use is waterproof, open waterproof component 7 when through-hole 211 that needs use.
The utility model provides a scalable unmanned aerial vehicle that shoots is convenient for accomodate, and protective capacities is strong, and waterproof performance is good simultaneously.
As shown in fig. 1, in this embodiment, the waterproof assembly 7 includes a connection block 71 and a waterproof cover 72, the connection block 71 and the waterproof cover 72 are fixedly connected, and the waterproof cover 72 is covered on the through hole 211. In actual use, the connecting block 71 is used for connecting the waterproof cover 72, and the waterproof cover 72 covers the through hole 211 to protect the through hole 211 from water.
As shown in fig. 1, in this embodiment, the protection assembly 6 includes a shock absorber 61 and a protection plate 62, the shock absorber 61 and the protection plate 62 are fixedly connected, and the protection plate 62 is located above the drone body 1. During the in-service use, bumper shock absorber 61 is used for the shock attenuation energy-absorbing, and guard plate 62 is used for providing protection, protecting against shock to unmanned aerial vehicle body 1.
As shown in fig. 1, in this embodiment, the shock absorber 61 includes an upper mounting seat 611, a spring 612, and a lower mounting seat 613, the top of the upper mounting seat 611 is fixedly connected to the bottom of the protection plate 62, the bottom of the lower mounting seat 613 is fixedly connected to the top of the drone body 1, and two ends of the spring 612 are fixedly connected to the bottom of the upper mounting seat 611 and the top of the lower mounting seat 613, respectively. In actual use, the upper mount 611 and the lower mount 613 are used to fix the connected device and the mounting spring 612.
In the embodiment, as shown in fig. 1, a handle 621 is disposed on the top of the protection plate 62. During the in-service use, through setting up handle 621, the handheld unmanned aerial vehicle body 1 of people of being convenient for.
All the technical features in the embodiment can be freely combined according to actual needs.
The above embodiments are preferred implementations of the present invention, and in addition, the present invention includes other implementations, and any obvious replacement is within the protection scope of the present invention without departing from the concept of the present invention.
Claims (5)
1. The utility model provides a scalable unmanned aerial vehicle that shoots, its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body, a telescopic wing supporting rod, a propeller, a monitoring camera, a rack, a protection component and a waterproof component, wherein the telescopic wing supporting rod is symmetrically and fixedly connected with the peripheral side wall of the unmanned aerial vehicle body, the tail end of the telescopic wing supporting rod is fixedly connected with the propeller, the bottom of the unmanned aerial vehicle body is respectively fixedly connected with the rack and the monitoring camera, the monitoring camera is positioned between the racks, the top of the unmanned aerial vehicle body is fixedly connected with the protection component, the telescopic wing supporting rod comprises a fixed rod, a telescopic rod and a locking bead, the telescopic rod is fixedly connected with the locking bead, the side surface of the fixed rod is provided with a through hole, the fixed rod and the telescopic rod are fixed through the locking bead, the waterproof component is fixedly connected with the fixed rod, the waterproof component is positioned under the through hole, the waterproof component can cover the through hole, and a storage battery and a control host are arranged in the unmanned aerial vehicle body, the propeller, the monitoring camera and the storage battery are all electrically connected with the control host.
2. The retractable filming drone of claim 1, wherein: the waterproof assembly comprises a connecting block and a waterproof cover, the connecting block is fixedly connected with the waterproof cover, and the waterproof cover is arranged on the through hole.
3. The retractable filming drone of claim 1, wherein: the protection component comprises a shock absorber and a protection plate, the shock absorber is fixedly connected with the protection plate, and the protection plate is located above the unmanned aerial vehicle body.
4. The retractable filming drone of claim 3, wherein: the bumper shock absorber includes mount pad, spring and lower mount pad, go up the top of mount pad and the bottom fixed connection of guard plate, the bottom of mount pad and the top fixed connection of unmanned aerial vehicle body down, the both ends of spring respectively with the bottom of last mount pad and the top fixed connection of mount pad down.
5. The retractable filming drone of claim 3, wherein: and a lifting handle is arranged at the top of the protection plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120721897.2U CN214930596U (en) | 2021-04-09 | 2021-04-09 | Scalable shooting unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120721897.2U CN214930596U (en) | 2021-04-09 | 2021-04-09 | Scalable shooting unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214930596U true CN214930596U (en) | 2021-11-30 |
Family
ID=79044344
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120721897.2U Active CN214930596U (en) | 2021-04-09 | 2021-04-09 | Scalable shooting unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214930596U (en) |
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2021
- 2021-04-09 CN CN202120721897.2U patent/CN214930596U/en active Active
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