CN216994833U - Folding unmanned aerial vehicle - Google Patents
Folding unmanned aerial vehicle Download PDFInfo
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- CN216994833U CN216994833U CN202220353036.8U CN202220353036U CN216994833U CN 216994833 U CN216994833 U CN 216994833U CN 202220353036 U CN202220353036 U CN 202220353036U CN 216994833 U CN216994833 U CN 216994833U
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Abstract
The utility model provides a folding unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicles and comprises the following components: an unmanned aerial vehicle main body and a leg main body; through set up the horn holding tank in the unmanned aerial vehicle main part, in flight process, the horn main part rotates for the unmanned aerial vehicle main part, the horn main part removes towards the direction of horn holding tank, the horn main part is accomodate into the horn holding tank, effectively avoid the horn main part to influence the effect of taking photo by plane of unmanned aerial vehicle main part, and unmanned aerial vehicle is in the transportation, accomodate the whole space that reduces unmanned aerial vehicle to the horn main part of horn holding tank, be convenient for transport, the horn structure that traditional unmanned aerial vehicle that exists used has been alleviated among the prior art, the horn is clapped easily to the camera, and unmanned aerial vehicle is in the transportation, the horn structure is accomodate inconveniently, the big technical problem of transportation occupation space.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a foldable unmanned aerial vehicle.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle controlled by a radio remote control device or an onboard computer program control system. The unmanned aerial vehicle has the advantages of simple structure and low use cost, not only can complete the task executed by the piloted aircraft, but also is more suitable for the task which is not suitable for being executed by the piloted aircraft. The emergency early warning device has great effects on emergency and early warning of emergencies.
The unmanned aerial vehicle aerial photography uses an unmanned aerial vehicle as an aerial platform, uses airborne remote sensing equipment such as a high-resolution CCD digital camera, a light optical camera, an infrared scanner, a laser scanner, a magnetic measuring instrument and the like to acquire information, processes image information by using a computer, and makes the image according to certain precision requirements.
However, the traditional leg structure that unmanned aerial vehicle used, the camera was clapped the leg easily to unmanned aerial vehicle is in the transportation, and the leg structure is accomodate inconveniently, and the transportation occupation space is big.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a folding unmanned aerial vehicle, which solves the technical problems that in the prior art, a leg structure used by the traditional unmanned aerial vehicle is easy to shoot by a camera, and the leg structure is inconvenient to store and occupies a large space in the transportation process of the unmanned aerial vehicle.
In a first aspect, the present invention provides a foldable drone, comprising: an unmanned aerial vehicle main body and a leg main body;
the unmanned aerial vehicle main part has the horn holding tank, the horn main part with the unmanned aerial vehicle main part rotates to be connected, the configuration of horn main part can for the unmanned aerial vehicle main part orientation the direction of horn holding tank rotates.
In an alternative embodiment of the method of the present invention,
the horn main part is located when the horn holding tank, the surface of horn main part with the surface parallel and level of unmanned aerial vehicle main part.
In an alternative embodiment of the method of the present invention,
the folding unmanned aerial vehicle also comprises a leg transmission component;
one end of the leg transmission member is rotatably connected with the unmanned aerial vehicle main body, and the other end of the leg transmission member is rotatably connected with the leg main body.
In an alternative embodiment of the method of the present invention,
the stand driving component comprises a first driving piece and a second driving piece;
the first driving medium unmanned aerial vehicle main part the second driving medium with the leg main part encloses and establishes and forms the parallelogram.
In an alternative embodiment of the method of the present invention,
the folding unmanned aerial vehicle also comprises a main body of the arm;
the unmanned aerial vehicle main part has the horn holding tank, the horn main part with the unmanned aerial vehicle main part rotates to be connected, the horn main part configuration can for the unmanned aerial vehicle main part orientation the direction of horn holding tank rotates.
In an alternative embodiment of the method of the present invention,
the horn main part is located when in the horn holding tank, the surface of horn main part with the surface parallel and level of unmanned aerial vehicle main part.
In an alternative embodiment of the method of the present invention,
the unmanned aerial vehicle main body is internally provided with a machine arm driving piece, and the machine arm driving piece is in transmission connection with the machine arm main body.
In an alternative embodiment of the method of the present invention,
the end part of the horn main body is provided with two wing blades, and the two wing blades can rotate relative to the horn main body.
In an alternative embodiment of the method of the present invention,
when the horn main part is located in the horn holding tank, two the wing paddle is parallel and level each other.
In an alternative embodiment of the method of the present invention,
the bottom of unmanned aerial vehicle main part is provided with the camera of taking photo by plane.
The utility model provides a folding unmanned aerial vehicle, comprising: an unmanned aerial vehicle main body and a leg main body; through set up the horn holding tank in the unmanned aerial vehicle main part, in flight process, the horn main part rotates for the unmanned aerial vehicle main part, the horn main part removes towards the direction of horn holding tank, the horn main part is accomodate into the horn holding tank, effectively avoid the horn main part to influence the effect of taking photo by plane of unmanned aerial vehicle main part, and unmanned aerial vehicle is in the transportation, accomodate the whole space that the horn main part of horn holding tank reduces unmanned aerial vehicle, the transportation of being convenient for, the horn structure that traditional unmanned aerial vehicle that exists used among the prior art has been alleviated, the horn is clapped easily to the camera, and unmanned aerial vehicle is in the transportation, the horn structure is accomodate inconveniently, the technical problem that transportation occupation space is big.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the embodiments or the prior art descriptions will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and other drawings can be obtained by those skilled in the art without creative efforts.
Fig. 1 is a schematic view of an overall structure of a folding type unmanned aerial vehicle according to an embodiment of the present invention;
fig. 2 is a schematic view of an overall structure of the folding type unmanned aerial vehicle in a storage state according to the embodiment of the present invention.
An icon: 100-a drone body; 110-leg receiving slots; 120-horn receiving slot; 130-horn actuation; 200-a leg body; 300-a leg transmission member; 310-a first transmission member; 320-a second transmission member; 400-a horn body; 500-wing blade.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all embodiments of the present invention. The components of embodiments of the present invention generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations.
Thus, the following detailed description of the embodiments of the present invention, presented in the figures, is not intended to limit the scope of the utility model, as claimed, but is merely representative of selected embodiments of the utility model. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings or orientations or positional relationships that the products of the present invention are conventionally placed in use, and are only for convenience of describing the present invention and simplifying the description, but do not indicate or imply that the device or element to which the description refers must have a specific orientation, be constructed in a specific orientation, and be operated, and thus should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.
Furthermore, the terms "horizontal", "vertical", "overhang" and the like do not imply that the components are required to be absolutely horizontal or overhang, but may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in a specific case to those of ordinary skill in the art.
Some embodiments of the utility model are described in detail below with reference to the accompanying drawings. The embodiments and features of the embodiments described below can be combined with each other without conflict.
As shown in fig. 1 and fig. 2, the folding unmanned aerial vehicle provided by this embodiment includes: a drone main body 100 and a leg main body 200; unmanned aerial vehicle main part 100 has leg holding tank 110, and leg main part 200 rotates with unmanned aerial vehicle main part 100 to be connected, and leg main part 200 configures to can rotate towards the direction of leg holding tank 110 for unmanned aerial vehicle main part 100.
Specifically, leg holding tank 110 has been seted up on unmanned aerial vehicle main part 100's surface, in unmanned aerial vehicle flight process or transportation, leg main part 200 rotates for unmanned aerial vehicle main part 100, leg main part 200 stretches into in leg holding tank 110, reduce whole unmanned aerial vehicle's space, and effectively avoid leg main part 200 to influence the shooting of camera, take off or descend the in-process at unmanned aerial vehicle main part 100, leg main part 200 stretches out in the leg holding tank 110, so that leg main part 200 supports unmanned aerial vehicle main part 100.
The foldable unmanned aerial vehicle that this embodiment provided includes: a drone main body 100 and a leg main body 200; through set up horn holding tank 110 on unmanned aerial vehicle main part 100, in flight process, horn main part 200 rotates for unmanned aerial vehicle main part 100, horn main part 200 removes towards the direction of horn holding tank 110, horn main part 200 is accomodate into horn holding tank 110 in, effectively avoid horn main part 200 to influence the effect of taking photo by plane of unmanned aerial vehicle main part 100, and unmanned aerial vehicle is in the transportation, the horn main part 200 of accomodating to horn holding tank 110 reduces unmanned aerial vehicle's whole space, be convenient for transport, the horn structure that traditional unmanned aerial vehicle that exists used has been alleviated among the prior art, the camera is clapped the horn easily, and unmanned aerial vehicle is in the transportation, the horn structure is accomodate inconveniently, the big technical problem of transportation occupation space.
On the basis of the above embodiment, in an optional implementation manner, when the leg main body 200 in the foldable unmanned aerial vehicle provided by this embodiment is located in the leg accommodating groove 110, the surface of the leg main body 200 is flush with the surface of the unmanned aerial vehicle main body 100.
Specifically, in order to reduce unmanned aerial vehicle's whole occupation space, the cell wall shape of horn holding tank 110 is the same with the shape of horn main part 200, and when horn main part 200 stretched into horn holding tank 110, horn main part 200 and unmanned aerial vehicle main part 100 parallel and level.
In an alternative embodiment, the folding drone further comprises a leg gear member 300; one end of the leg transmission member 300 is rotatably connected to the main body 100 of the unmanned aerial vehicle, and the other end of the leg transmission member 300 is rotatably connected to the leg main body 200.
Specifically, leg transmission member 300 sets up between unmanned aerial vehicle main part 100 and leg transmission member 300, and the driving piece in unmanned aerial vehicle main part 100 passes through leg transmission member 300 and drives leg main part 200 and rotate, realizes that leg main part 200 stretches into or stretches out leg holding tank 110.
In an alternative embodiment, leg transmission member 300 includes a first transmission piece 310 and a second transmission piece 320; the first transmission piece 310, the main body 100 of the unmanned aerial vehicle, the second transmission piece 320 and the main body 200 of the leg are arranged in a surrounding manner to form a parallelogram.
Specifically, first driving medium 310 and second driving medium 320 interval set up, and first driving medium 310, unmanned aerial vehicle main part 100, second driving medium 320 and leg main part 200 enclose the parallelogram structure of establishing and can make leg main part 200 move towards the direction of leg holding tank 110, make leg main part 200 accomodate completely in leg holding tank 110.
The foldable unmanned aerial vehicle that this embodiment provided, through the setting of horn transmission member 300, drive horn main part 200 and remove for unmanned aerial vehicle main part 100, accomplish the action that horn main part 200 stretched into or stretched out horn holding tank 110.
In an alternative embodiment, the folding drone further comprises a horn body 400; the unmanned aerial vehicle main part 100 has horn holding groove 120, and horn main part 400 rotates with unmanned aerial vehicle main part 100 and is connected, and horn main part 400 is configured as can rotating towards the direction of horn holding groove 120 for unmanned aerial vehicle main part 100.
Specifically, horn holding tank 120 is seted up on the surface of horn main part 400, and when unmanned aerial vehicle main part 100 was in flight state, horn main part 400 stretched out horn holding tank 120, provides flight power, and in the time of unmanned aerial vehicle main part 100 shut down transportation, horn main part 400 stretched into horn holding tank 120, reduced whole unmanned aerial vehicle's occupation space.
In an alternative embodiment, when the horn main body 400 is located within the horn receiving slot 120, the surface of the horn main body 400 is flush with the surface of the drone main body 100.
Specifically, the shape of the groove wall of the horn receiving groove 120 is the same as that of the horn main body 400, and when the horn main body 400 extends into the horn receiving groove 120, the horn main body 400 is flush with the drone main body 100.
In an alternative embodiment, the main body 100 of the drone has an arm driver 130 therein, and the arm driver 130 is in driving connection with the main body 400 of the drone.
Specifically, be provided with horn driving piece 130 in unmanned aerial vehicle main part 100, horn driving piece 130 can set up to driving motor, drives horn main part 400 and rotates for unmanned aerial vehicle main part 100, accomplishes the action that horn main part 400 stretched into or stretched out horn holding tank 120.
In an alternative embodiment, two wing blades 500 are provided at the end of the horn body 400, both wing blades 500 being rotatable relative to the horn body 400.
Specifically, the end of each horn main body 400 is provided with two wing blades 500, and the two wing blades 500 rotate relative to the horn main body 400 to form the flight driving force of the unmanned aerial vehicle.
In an alternative embodiment, the two wing blades 500 are flush with each other when the horn body 400 is positioned within the horn receiving slot 120.
Specifically, when the unmanned aerial vehicle shuts down the transportation, horn main part 400 is accomodate in horn holding tank 120 to two wing blades 500 are close to the parallel and level each other towards the direction of unmanned aerial vehicle main part 100, reduce whole occupation space.
In an alternative embodiment, the bottom of the drone main body 100 is provided with an aerial camera.
Specifically, set up the mounting equipment in the bottom of unmanned aerial vehicle main part 100, the mounting equipment can carry on the camera of taking photo by plane, provides the function of taking photo by plane.
In addition, it should be noted that the horn main body 400 and the leg main body 200 may be provided in plural according to actual situations, the number of the horn main body 400 and the horn receiving groove 120 is one-to-one corresponding to each other, and the number of the leg main body 200 and the leg receiving groove 110 is one-to-one corresponding to each other.
The foldable unmanned aerial vehicle that this embodiment provided, through set up horn holding tank 120 on unmanned aerial vehicle main part 100's surface, in the unmanned aerial vehicle transportation, horn main part 400 rotates and enters into horn holding tank 120, makes the surface of horn main part 400 and unmanned aerial vehicle main part 100's surface parallel and level, effectively reduces unmanned aerial vehicle's occupation space.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; while the utility model has been described in detail and with reference to the foregoing embodiments, it will be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; and these modifications or substitutions do not depart from the spirit of the corresponding technical solutions of the embodiments of the present invention.
Claims (9)
1. A foldable unmanned aerial vehicle, comprising: a main unmanned aerial vehicle body (100) and a leg body (200);
the unmanned aerial vehicle main body (100) is provided with a leg accommodating groove (110), the leg main body (200) is rotatably connected with the unmanned aerial vehicle main body (100), and the leg main body (200) is configured to be capable of rotating relative to the unmanned aerial vehicle main body (100) towards the direction of the leg accommodating groove (110);
the folding drone further comprises a horn body (400);
the unmanned aerial vehicle main part (100) has horn holding tank (120), horn main part (400) with unmanned aerial vehicle main part (100) rotate to be connected, horn main part (400) configure to can for unmanned aerial vehicle main part (100) orientation horn holding tank (120) direction rotates.
2. The folding drone of claim 1,
when leg main part (200) are located in leg holding tank (110), the surface of leg main part (200) with the surface parallel and level of unmanned aerial vehicle main part (100).
3. The folding drone of claim 2,
the folding drone further comprises a leg transmission member (300);
the one end of horn transmission member (300) with unmanned aerial vehicle main part (100) rotate to be connected, the other end of horn transmission member (300) with horn main part (200) rotate to be connected.
4. The folding drone of claim 3,
the leg transmission member (300) comprises a first transmission piece (310) and a second transmission piece (320);
the first transmission piece (310), the unmanned aerial vehicle main body (100), the second transmission piece (320) and the leg main body (200) are enclosed to form a parallelogram.
5. The folding drone of claim 1,
when horn main part (400) are located horn holding tank (120), the surface of horn main part (400) with the surface parallel and level of unmanned aerial vehicle main part (100).
6. The folding drone of claim 5,
an arm driving piece (130) is arranged in the unmanned aerial vehicle main body (100), and the arm driving piece (130) is in transmission connection with the arm main body (400).
7. The folding drone of claim 5,
two wing blades (500) are arranged at the end part of the horn main body (400), and the two wing blades (500) can rotate relative to the horn main body (400).
8. The folding drone of claim 7,
when the horn main body (400) is located in the horn receiving groove (120), the two wing blades (500) are flush with each other.
9. The folding drone of claim 1,
the bottom of unmanned aerial vehicle main part (100) is provided with the camera of taking photo by plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220353036.8U CN216994833U (en) | 2022-02-21 | 2022-02-21 | Folding unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220353036.8U CN216994833U (en) | 2022-02-21 | 2022-02-21 | Folding unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216994833U true CN216994833U (en) | 2022-07-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220353036.8U Active CN216994833U (en) | 2022-02-21 | 2022-02-21 | Folding unmanned aerial vehicle |
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| Country | Link |
|---|---|
| CN (1) | CN216994833U (en) |
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- 2022-02-21 CN CN202220353036.8U patent/CN216994833U/en active Active
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