CN205971799U - Foldable unmanned aerial vehicle - Google Patents
Foldable unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205971799U CN205971799U CN201620613810.9U CN201620613810U CN205971799U CN 205971799 U CN205971799 U CN 205971799U CN 201620613810 U CN201620613810 U CN 201620613810U CN 205971799 U CN205971799 U CN 205971799U
- Authority
- CN
- China
- Prior art keywords
- axis
- fuselage
- paddle
- hinge
- arm
- 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.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The utility model relates to a foldable unmanned aerial vehicle, the reciprocating impact tunnel drilling machine comprises a machine body, be equipped with the oar arm that a plurality of symmetry plane for in the fuselage are the symmetric distribution on the fuselage, the one end that the fuselage was kept away from to each oar arm is equipped with the paddle subassembly, fuselage bottom central point puts and is connected with the axis, axis outside cover has can follow the axis ring that slides from top to bottom, there is the skeleton in the ring outside through hinge hinge, it is articulated with oar bizhong portion that the skeleton other end passes through the hinge, axis one side is equipped with fixing device, the axis is connected with the undercarriage with the other end that the fuselage is connected, the undercarriage bottom is equipped with shock -absorbing foot. The utility model discloses to starch the arm and together pack up together with motor and paddle when the transportation is carried, and not only reduce occupation space and still be favorable to protection thick liquid arm and paddle not fragile when the transportation is carried.
Description
Technical field
The utility model is related to unmanned plane field, more particularly, to a kind of folding unmanned plane.
Background technology
Unmanned plane, is to start a kind of gradually practical aircraft at present, and it has maneuverability, reacts quick, unmanned
Flight, operation require low advantage.Multiclass sensor, such as camera, it is possible to achieve image passes in real time are loaded on unmanned plane
Defeated, high-risk areas detecting function, is widely used in the fields such as fire-fighting, military affairs, traffic, police service, exploration and meteorology, right to realize
The cruise shooting of designated area and supervision.At present, unmanned plane is to be designed manufacturing based on the flight theory of helicopter mostly,
Can achieve vertical lift and high-altitude hovering, thus meeting the requirement taking photo by plane and monitor, most common is that single shaft single-blade, single shaft are starched altogether
And many rotor (for example, four rotor) forms.
The species of unmanned plane is various at present, but a problem is that paddle arm and blade transport are fragile when carrying, because
This needs a kind of paddle arm can fold the unmanned plane packed up.
Utility model content
The purpose of this utility model is the problem above overcoming prior art to exist, and provides a kind of folding unmanned
Machine, has the advantages that paddle arm can fold and is transported.
For realizing above-mentioned technical purpose, reach above-mentioned technique effect, the utility model is achieved through the following technical solutions：One
Kind of folding unmanned plane, including fuselage, described fuselage be provided with multiple with respect to the symmetrical plane in described fuselage symmetrically
The paddle arm of distribution, described paddle arm passes through hinge with fuselage, and each paddle arm is provided with blade group away from one end of described fuselage
Part, described paddle components include the motor being arranged in described paddle arm and the blade being connected on the output shaft of described motor, often
The rotation axis of a piece of blade is respectively positioned on the same face of cylinder, and described fuselage bottom center is connected with axis, described axis
Outside be cased with to slide up and down annulus along axis, outside described annulus, skeleton is had by hinge, described skeleton with respect in
Axle is symmetric, and the described skeleton other end passes through hinged in the middle part of hinge and paddle arm, and described axis side is provided with fixing device, institute
State the other end that axis is connected with fuselage and be connected with undercarriage, described undercarriage bottom is provided with shock-absorbing foot, described fixing device bag
Include spring, triangle metal piece, described spring one end is fixed on inside axis, and the other end is fixedly connected with triangle metal piece,
Described triangle metal piece wherein a line is vertical with axis.
Further, described axis is hollow circular-tube.
Further, paddle arm is articulated with the bottom of described fuselage.
Further, described fuselage includes controller, battery, gyroscope, signal receiver, and described controller passes through to be electrically connected
Connect and battery, gyroscope, signal receiver, motor connection.
The beneficial effects of the utility model are：When transport carries, slurry arm is together packed up together with motor and blade, not only
Reduction takes up room to also help and protects slurry arm and blade to be hardly damaged when transport carries.
Brief description
Accompanying drawing described herein is used for providing further understanding to of the present utility model, constitutes the part of the application,
Schematic description and description of the present utility model is used for explaining the utility model, does not constitute to of the present utility model improper
Limit.In the accompanying drawings：
Fig. 1 is whole structure schematic diagram of the present utility model；
Fig. 2 is the utility model top view；
Fig. 3 is the utility model front view；
Fig. 4 is the utility model right view；
In figure label declaration：1- fuselage, 2- paddle arm, 3- motor, 4- blade, 5- axis, 6- skeleton, 7- undercarriage, 8- subtract
Shake pin, 9- fixing device, 10- annulus.
Specific embodiment
Below with reference to the accompanying drawings and in conjunction with the embodiments, to describe the utility model in detail.
As shown in Figures 1 to 4, the present embodiment provides a kind of folding unmanned plane, and including fuselage 1, fuselage 1 is provided with multiple
The paddle arm 2 being symmetric with respect to the symmetrical plane in fuselage 1, paddle arm 2 passes through hinge, each paddle arm 2 with fuselage 1
One end away from fuselage 1 is provided with paddle components, and paddle components include the motor 3 being arranged in paddle arm 2 and are connected to the defeated of motor 3
Blade 4 on shaft, often the rotation axis of a piece of blade 4 be respectively positioned on the same face of cylinder, fuselage 1 bottom centre position is connected with
Axis 5, is cased with outside axis 5 to slide up and down annulus 10 along axis 5, there are skeleton 6, skeleton in annulus 10 outside by hinge
6 are symmetric with respect to axis 5, and skeleton 6 other end is hinged with paddle arm 2 middle part by hinge, and axis 5 side is provided with fixing dress
Put 9, when transport carries, slurry arm is together packed up together with motor and blade, not only reducing takes up room also helps protection slurry arm
It is hardly damaged when transport carries with blade, the other end that axis 5 is connected with fuselage 1 is connected with undercarriage 7, undercarriage 7 bottom
It is provided with shock-absorbing foot 8, reduce impulsive force when unmanned plane lands.
As shown in figure 3, paddle arm 2 is articulated with the bottom of fuselage 1；Thus blade 4 is subject to liter upwards when unmanned plane is in flight
During power, paddle arm 2 can be prevented to be folded up.
Axis 5 is hollow circular-tube, mitigates the weight of fuselage, and fixing device 9 includes spring, triangle metal piece, spring one
End is fixed on inside axis 5, and the other end is fixedly connected with triangle metal piece, triangle metal piece wherein a line and axis 5
Vertically, prevent retainer ring landing during use, fuselage 1 includes controller, battery, gyroscope, signal receiver, controller passes through electricity
Connect and battery, gyroscope, signal receiver, motor connection.
Of the present utility model general principle, principal character and of the present utility model advantage have been shown and described above.One's own profession
The technical staff of industry it should be appreciated that the utility model is not restricted to the described embodiments, described in above-described embodiment and specification
Principle of the present utility model is simply described, on the premise of without departing from the utility model spirit and scope, the utility model is also
Have various changes and modifications, these changes and improvements both fall within the range of claimed the utility model.
Claims (4)
1. a kind of folding unmanned plane, including fuselage it is characterised in that described fuselage be provided with multiple with respect to described fuselage
In the paddle arm that is symmetric of symmetrical plane, described paddle arm passes through hinge with fuselage, and each paddle arm is away from described machine
One end of body is provided with paddle components, and described paddle components include the motor being arranged in described paddle arm and are connected to described motor
Blade on output shaft, often the rotation axis of a piece of blade be respectively positioned on the same face of cylinder, described fuselage bottom center is even
It is connected to axis, be cased with outside described axis to slide up and down annulus along axis, outside described annulus, skeleton had by hinge,
Described skeleton is symmetric with respect to axis, and the described skeleton other end passes through hinged, described axis one in the middle part of hinge and paddle arm
Side is provided with fixing device, and the other end that described axis is connected with fuselage is connected with undercarriage, and described undercarriage bottom is provided with damping
Pin, described fixing device includes spring, triangle metal piece, and described spring one end is fixed on inside axis, the other end and triangle
Shape sheet metal is fixedly connected, and described triangle metal piece wherein a line is vertical with axis.
2. a kind of folding unmanned plane according to claim 1 it is characterised in that：Described axis is hollow circular-tube.
3. a kind of folding unmanned plane according to claim 1 it is characterised in that：Described paddle arm is articulated with described fuselage
Bottom.
4. a kind of folding unmanned plane according to claim 1 it is characterised in that：Described fuselage includes controller, electricity
Pond, gyroscope, signal receiver, described controller passes through electrical connection and battery, gyroscope, signal receiver, motor connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620613810.9U CN205971799U (en) | 2016-06-21 | 2016-06-21 | Foldable unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620613810.9U CN205971799U (en) | 2016-06-21 | 2016-06-21 | Foldable unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205971799U true CN205971799U (en) | 2017-02-22 |
Family
ID=58021017
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620613810.9U Expired - Fee Related CN205971799U (en) | 2016-06-21 | 2016-06-21 | Foldable unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205971799U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105882937A (en) * | 2016-06-21 | 2016-08-24 | 石为 | Foldable drone |
-
2016
- 2016-06-21 CN CN201620613810.9U patent/CN205971799U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105882937A (en) * | 2016-06-21 | 2016-08-24 | 石为 | Foldable drone |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202071985U (en) | Novel plane symmetrical layout type multi-rotor unmanned air vehicle | |
| CN207191432U (en) | Rescue four rotor wing unmanned aerial vehicles in a kind of public security waters | |
| CN107963209A (en) | Tandem wing tilting rotor wing unmanned aerial vehicle | |
| CN107512394A (en) | A kind of tail sitting posture VUAV and flight control method | |
| CN205131674U (en) | Small -size all -wing aircraft overall arrangement unmanned aerial vehicle | |
| CN106347625A (en) | Unmanned aerial vehicle linkage folding mechanism | |
| CN205971799U (en) | Foldable unmanned aerial vehicle | |
| CN206664932U (en) | A kind of VTOL fixed-wing unmanned plane | |
| CN205524954U (en) | Four -rotor aircraft | |
| CN107323664A (en) | A kind of aircraft for being stuck in the water surface | |
| CN207360578U (en) | A kind of unmanned plane that can be taken off and quickly be assembled without instrument in case | |
| CN107985574B (en) | Buoyancy assisted lifting unmanned aerial vehicle | |
| CN108248849A (en) | A kind of improved double-deck rotor wing unmanned aerial vehicle | |
| CN207045715U (en) | A kind of novel and multifunctional unmanned plane | |
| CN206782064U (en) | A kind of collapsible rotor wing unmanned aerial vehicle of four axle six | |
| CN105882937A (en) | Foldable drone | |
| CN107757898A (en) | One kind is taken photo by plane folding wings unmanned plane | |
| CN106828914A (en) | A kind of modularization VTOL fixed-wing unmanned vehicle based on culvert type force vector component | |
| CN207523932U (en) | Tandem wing tilting rotor wing unmanned aerial vehicle | |
| CN206141824U (en) | Novel unmanned aerial vehicle | |
| CN216003098U (en) | Gaseous detecting system of unmanned aerial vehicle | |
| CN206125407U (en) | Miniature ducted fan aircraft | |
| CN113511334A (en) | Vector control VTOL unmanned aerial vehicle | |
| CN205469769U (en) | Area hangs six collapsible rotor crafts in cabin | |
| CN207089678U (en) | A kind of vehicle-mounted unmanned aerial vehicle system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170222 Termination date: 20180621 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |