CN212861841U - Collapsible unmanned aerial vehicle with flexible support - Google Patents
Collapsible unmanned aerial vehicle with flexible support Download PDFInfo
- Publication number
- CN212861841U CN212861841U CN202021455796.7U CN202021455796U CN212861841U CN 212861841 U CN212861841 U CN 212861841U CN 202021455796 U CN202021455796 U CN 202021455796U CN 212861841 U CN212861841 U CN 212861841U
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- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- rotor support
- vehicle casing
- silica gel
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- Expired - Fee Related
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Abstract
The utility model discloses a collapsible unmanned aerial vehicle with flexible support, including the unmanned aerial vehicle casing, produce the screw of flight power, be used for driving the rotatory motor and the controller of screw, its characterized in that: the both sides of unmanned aerial vehicle casing are equipped with the rotor support, the rotor support is the metal collapsible tube structure, the other end and the motor of rotor support are connected, are equipped with the adhesion layer at the surface of unmanned aerial vehicle casing, rotor support, are equipped with the silica gel layer on the adhesion layer, are equipped with connecting device on the rotor support in the both sides of unmanned aerial vehicle casing, according to metal collapsible tube's structural characteristic, can change angle and direction wantonly, can connect the rotor support of the both sides of unmanned aerial vehicle casing through connecting device like this to the annular structure of shape hand is convenient for when not using, wears in wrist department.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to collapsible unmanned aerial vehicle with flexible support.
Background
With the development of the unmanned aerial vehicle technology, the unmanned aerial vehicle is widely applied to various aspects such as military investigation, civil video shooting and the like. Although the volume of the existing unmanned aerial vehicle is small, a certain problem still exists in the aspect of carrying, and portability still needs to be improved.
Disclosure of Invention
The purpose of the invention is as follows: the utility model aims to provide a collapsible unmanned aerial vehicle with flexible support to prior art not enough.
The technical scheme is as follows: collapsible unmanned aerial vehicle with flexible support, including the unmanned aerial vehicle casing, produce the screw of flight power, be used for driving the rotatory motor of screw and controller the both sides of unmanned aerial vehicle casing are equipped with the rotor support, the rotor support is the metal collapsible tube structure, the other end and the motor of rotor support are connected, are equipped with the adhesion layer at the surface of unmanned aerial vehicle casing, rotor support, are equipped with the silica gel layer on the adhesion layer, are equipped with connecting device on the rotor support of the both sides that are in the unmanned aerial vehicle casing, connecting device makes the rotor leg joint or the separation that is in the both sides of unmanned aerial vehicle casing.
As a further improvement, the connection device includes that the magnetism on the rotor support of unmanned aerial vehicle casing one side is buckled, a plurality of and magnetism on the rotor support of unmanned aerial vehicle casing one side are buckled complex magnetism hole, and magnetism mouth and magnetism hole are established on the silica gel layer.
As a further improvement of the utility model, two rotor supports are arranged on two sides of the unmanned aerial vehicle shell.
As a further improvement, the metal hose is made of aluminum alloy.
As a further improvement of the utility model, a transmission line is arranged in the metal hose, and the transmission line is respectively connected with the motor and the controller.
As a further improvement of the utility model the position department that the silica gel layer is close to the screw is equipped with the protection platform, the protection platform is the colloidal silica body with silica gel layer integrated into one piece, the internal face of protection platform is equipped with the arc wall of quarter arc, the screw is in.
Has the advantages that: (1) the utility model discloses a rotor support is the metal collapsible tube structure, structural characteristic according to metal collapsible tube, when straightening the state, can guarantee certain structural rigidity, guarantee the rigidity demand under the unmanned aerial vehicle flight state, angle and direction can be changed wantonly simultaneously, can connect the rotor support of the both sides of unmanned aerial vehicle casing like this through connecting device, thereby shape hand annular structure, be convenient for when not using, wear in wrist department, simultaneously because be equipped with the silica gel layer, increase the comfort of wearing, it is waterproof also to have simultaneously, the effect of protection.
(2) The specific arrangement of the connecting device can lead the magnetic button to be matched with the magnetic holes at different positions, thereby changing the size and shape of the hand ring shape and adapting to the sizes of the arms of different people.
(3) Metal collapsible tube adopts the aluminum alloy material, makes the holistic structure of unmanned aerial vehicle lighter, and is more portable.
(4) The transmission line is arranged in the metal hose, so that the transmission line can be better protected.
(5) The protection platform can play the guard action to the screw.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the present invention in an unused state;
figure 3 is the structure diagram of the rotor support of the present invention.
Detailed Description
The technical solution of the present invention is described in detail below with reference to the accompanying drawings, but the scope of the present invention is not limited to the embodiments.
Example 1:
shown by figures 1-3, the utility model discloses an unmanned aerial vehicle casing 1, the screw 2 that produces flight power, be used for driving the rotatory motor of screw 2 and controller unmanned aerial vehicle casing 1's both sides respectively are equipped with two rotor support 7, rotor support 7 is the metal collapsible tube structure, metal collapsible tube 3 adopts the aluminum alloy material be equipped with the transmission line in the metal collapsible tube 3, the transmission line is connected with motor, controller respectively, rotor support 7's the other end and motor are connected, are equipped with adhesion layer 4 at unmanned aerial vehicle casing 1, rotor support 7's surface, are equipped with silica gel layer 5 on adhesion layer 4, are equipped with connecting device on the rotor support 7 of the both sides that are in unmanned aerial vehicle casing 1, connecting device makes the rotor support 7 of the both sides that are in unmanned aerial vehicle casing 1 connect or separate, connecting device detains including the magnetism on the rotor support 7 of locating unmanned aerial vehicle casing 1 one side and detains, Locate a plurality of and magnetism on the rotor support 7 of unmanned aerial vehicle casing 1 one side and detain complex magnetism hole, magnetism mouth and magnetism hole are established on silica gel layer 5 is close to the position department of screw 2 and is equipped with protection platform 6, protection platform 6 is the colloidal silica body with silica gel layer 5 integrated into one piece, the internal face of protection platform 6 is equipped with the arc wall of quarter arc, screw 2 is in.
The utility model has the advantages that:
(1) the utility model discloses a rotor support 7 is metal collapsible tube 3 structure, structural characteristic according to metal collapsible tube 3, when straightening the state, can guarantee certain structural rigidity, guarantee the rigidity demand under the unmanned aerial vehicle flight state, angle and direction can be changed wantonly simultaneously, can connect rotor support 7 of the both sides of unmanned aerial vehicle casing 1 like this through connecting device, thereby shape hand ring-shaped structure, be convenient for when not using, wear in wrist department, simultaneously because be equipped with silica gel layer 5, increase the comfort of wearing, it is waterproof also to have simultaneously, the effect of protection.
(2) The specific arrangement of the connecting device can lead the magnetic button to be matched with the magnetic holes at different positions, thereby changing the size and shape of the hand ring shape and adapting to the sizes of the arms of different people.
(3) Metal collapsible tube 3 adopts the aluminum alloy material, makes the holistic structure of unmanned aerial vehicle lighter, and is more portable.
(4) The transmission line is arranged in the metal hose 3, so that the transmission line can be better protected.
(5) The protective platform 6 can protect the propeller 2.
As mentioned above, although the present invention has been shown and described with reference to certain preferred embodiments, it should not be construed as limiting the invention itself. Various changes in form and detail may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.
Claims (6)
1. The utility model provides a collapsible unmanned aerial vehicle with flexible support, includes the unmanned aerial vehicle casing, produces flight power's screw, is used for driving the rotatory motor and the controller of screw, its characterized in that: the utility model discloses a unmanned aerial vehicle, including unmanned aerial vehicle casing, rotor support, motor, adhesive layer, silica gel layer, connecting device make the rotor support connection or the separation that is in the both sides of unmanned aerial vehicle casing, the rotor support is equipped with the rotor support in the both sides of unmanned aerial vehicle casing, the rotor support is the metal collapsible tube structure, the other end and the motor of rotor support are connected, are equipped with the adhesive layer at the surface of unmanned aerial vehicle casing, rotor support, are equipped with the silica gel layer on the adhesive layer, are equipped with connecting device.
2. A foldable drone with flexible support according to claim 1, characterised in that: connecting device detains, locates a plurality of and magnetism on the rotor support of unmanned aerial vehicle casing one side and detains complex magnetism hole including the magnetism of locating on the rotor support of unmanned aerial vehicle casing one side, and magnetism mouth and magnetism hole are established on the silica gel layer.
3. A foldable drone with flexible support according to claim 1, characterised in that: two rotor wing brackets are arranged on two sides of the unmanned aerial vehicle shell.
4. A foldable drone with flexible support according to claim 1, characterised in that: the metal hose is made of an aluminum alloy material.
5. A foldable drone with flexible support according to claim 1, characterised in that: and a transmission line is arranged in the metal hose and is respectively connected with the motor and the controller.
6. A foldable drone with flexible support according to claim 1, characterised in that: the position department that the silica gel layer is close to the screw is equipped with the protection platform, the protection platform is the colloidal silica body with silica gel layer integrated into one piece, the internal face of protection platform is equipped with the arc wall of quarter arc, the screw is in.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021455796.7U CN212861841U (en) | 2020-07-22 | 2020-07-22 | Collapsible unmanned aerial vehicle with flexible support |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021455796.7U CN212861841U (en) | 2020-07-22 | 2020-07-22 | Collapsible unmanned aerial vehicle with flexible support |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212861841U true CN212861841U (en) | 2021-04-02 |
Family
ID=75215994
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021455796.7U Expired - Fee Related CN212861841U (en) | 2020-07-22 | 2020-07-22 | Collapsible unmanned aerial vehicle with flexible support |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212861841U (en) |
-
2020
- 2020-07-22 CN CN202021455796.7U patent/CN212861841U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210402 Termination date: 20210722 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |