CN212243784U - Portable unmanned aerial vehicle - Google Patents
Portable unmanned aerial vehicle Download PDFInfo
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- CN212243784U CN212243784U CN202021053257.0U CN202021053257U CN212243784U CN 212243784 U CN212243784 U CN 212243784U CN 202021053257 U CN202021053257 U CN 202021053257U CN 212243784 U CN212243784 U CN 212243784U
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Abstract
The utility model provides a portable unmanned aerial vehicle, which comprises a body, a front arm, a rear arm, a front power device and a rear power device, wherein the positions of two sides of the body, which are close to the end part, are provided with front connecting grooves, the positions of the two sides, which are far away from the front connecting grooves and are close to the other end part of the body, one end of the front arm is hinged in the front connecting grooves, one end of the rear arm is hinged in the rear connecting grooves, the front power device is connected with the end, which is far away from the front connecting grooves, on the front arm, the rear power device is connected with the end, which is far away from the rear connecting grooves, on the rear arm, the front power device and the rear power device comprise a motor and; the utility model discloses a portable unmanned aerial vehicle can folding horn through the setting, draws in the fuselage side in with the horn that stretches out, and can fold screw and undercarriage, and occupation space is less during unmanned aerial vehicle closed state, accomodates and carries more conveniently.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field, in particular to portable unmanned aerial vehicle.
Background
Currently, drones are unmanned aircraft that are operated by radio remote control devices and self-contained program control devices, or can be operated autonomously, either completely or intermittently, by an on-board computer. Through the accumulation of technologies for many years and the rapid development of economy, the application scenarios of the existing unmanned aerial vehicle are more and more, for example: aerial photography, crop monitoring, vegetation protection, self-timer, express transportation, disaster relief, wildlife observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, movie and television photography, and the like. The existing unmanned aerial vehicle is large in size and inconvenient to carry.
The above technical problem needs to be solved by providing a portable unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
The utility model provides a portable unmanned aerial vehicle to unmanned aerial vehicle among the solution prior art exists more that the volume is great, carries inconveniently, and the not reasonable problem inadequately of distribution of each part.
In order to solve the technical problem, the utility model adopts the technical scheme that: a portable drone, comprising:
the device comprises a machine body, wherein front connecting grooves are formed in positions, close to end parts, of two side surfaces, rear connecting grooves are formed in positions, far away from the front connecting grooves, close to the other end part of the machine body, of the two side surfaces, and the rear connecting grooves and the front connecting grooves are used for connection;
one end of the front machine arm is hinged in the front connecting groove and used for connection;
one end of the rear arm is hinged in the rear connecting groove and used for connection;
the front power device is connected to one end, far away from the front connecting groove, of the front arm and is used for driving the unmanned aerial vehicle to fly;
the rear power device is connected to one end, far away from the rear connecting groove, of the rear arm and is used for driving the unmanned aerial vehicle to fly;
the portable unmanned aerial vehicle comprises a closed state and an expanded state, when the portable unmanned aerial vehicle is in the closed state, one end, far away from the front connecting groove, of the front arm is in contact with the middle of the vehicle body, and one end, far away from the rear connecting groove, of the rear arm is in contact with the middle of the vehicle body;
when portable unmanned aerial vehicle is located the expansion state, preceding horn is kept away from preceding spread groove one end and is kept away from the fuselage middle part, back horn is kept away from back spread groove one end and is kept away from the fuselage middle part, and preceding horn is with the back horn and is diverged the shape on the fuselage.
In the portable unmanned aerial vehicle, a front undercarriage is arranged at the lower side of one end of the front arm, which is far away from the front connecting groove, a rear undercarriage is arranged at the lower side of one end of the rear arm, which is far away from the rear connecting groove, and the front undercarriage and the rear undercarriage are used for supporting the unmanned aerial vehicle when the unmanned aerial vehicle rises and falls;
the nose landing gear is connected to the nose horn in a bending mode, and the rear landing gear is connected to the rear horn in a bending mode;
when the unmanned aerial vehicle is in a closed state, one end of the front undercarriage, which is far away from the front power device, is in contact with the lower end of the front horn, and one end of the rear undercarriage, which is far away from the rear power device, is in contact with the lower end of the rear horn;
when the unmanned aerial vehicle is in a spreading state, the included angle between the extension direction of the nose landing gear and the lower end face of the nose horn is 90-120 degrees, and the included angle between the extension direction of the rear landing gear and the lower end face of the rear horn is 90-120 degrees.
Among portable unmanned aerial vehicle, preceding spread groove includes:
the first front blocking surface is vertical to the machine body, parallel to the length direction of the machine body and used for limiting the rotation of the front machine arm;
the second front blocking surface is a circular arc surface in the vertical direction, is connected with the first front blocking surface and is used for limiting the rotation of the front horn;
when the portable unmanned aerial vehicle is in a closed state, a front arm contacts the first front blocking surface;
when the portable unmanned aerial vehicle is in the unfolding state, the front arm contacts the tail end of the second front blocking surface, and the included angle between the axis of the front arm and the first front blocking surface is 90-135 degrees.
Among the portable unmanned aerial vehicle, the back spread groove includes:
the first rear blocking surface is vertical to the machine body, parallel to the length direction of the machine body and used for limiting the rotation of the rear machine arm;
the second rear blocking surface is a circular arc surface in the vertical direction, is connected with the first rear blocking surface and is used for limiting the rotation of the rear arm;
when the portable unmanned aerial vehicle is in a closed state, the rear arm contacts the first rear blocking surface;
when the portable unmanned aerial vehicle is in the unfolding state, the rear arm contacts the tail end of the second rear blocking surface, and the included angle between the axis of the rear arm and the first rear blocking surface is 90-135 degrees.
Among the portable unmanned aerial vehicle, the fuselage upper surface is circular-arc, and the fuselage is narrower than both ends along the middle on the length direction.
In the portable unmanned aerial vehicle of the utility model, the front power device comprises a first motor and a first screw, the first screw is connected to the upper side of the first motor, and the first motor is used for driving the first screw to rotate;
the rear power device comprises a second motor and a second propeller, the second propeller is connected to the upper side of the second motor, and the second motor is used for driving the second propeller to rotate.
In the portable unmanned aerial vehicle of the present invention, the first propeller includes first wings and first connecting plates, two of the first wings are hinged to both sides of the first connecting plates, and the first connecting plates are connected to the first motor;
the second propeller comprises a second wing and a second connecting plate, the two second wings are hinged to two sides of the second connecting plate, and the second connecting plate is connected to the second motor.
Among the portable unmanned aerial vehicle, the fuselage downside is provided with module and the safety cover of making a video recording, make a video recording the module with the safety cover is close to preceding draw bail position, the module of making a video recording is used for making a video recording, the safety cover is used for protecting the module of making a video recording.
Among the portable unmanned aerial vehicle, the module of making a video recording includes:
the camera shooting base is connected to the body and used for connection;
the rotary table is of an L-shaped structure, two ends of the rotary table are provided with rotary motors, the axes of the two rotary motors are perpendicular to each other, and the rotary table is connected to the camera base through the rotary motors and used for expanding the visual field;
the connecting seat is of a U-shaped structure, one end of the connecting seat is opened, and the other end of the connecting seat is connected with a rotating motor which is far away from the base and is arranged on the rotating table and used for connection;
the camera is connected in the opening of the connecting seat and used for shooting;
be close to on the base of making a video recording revolving stage one side is provided with first stopper, be close to revolving stage one side on the connecting seat and be provided with the second stopper, first stopper and second stopper are used for restricting the rotatory yardstick of revolving stage.
Among portable unmanned aerial vehicle, fuselage lower extreme middle part is provided with battery compartment and battery case, the battery compartment is square groove form, and the battery case is the cuboid structure, and the battery case passes through the buckle connected mode to be connected in the battery compartment.
The utility model discloses compare in prior art, its beneficial effect is: the utility model discloses a portable unmanned aerial vehicle can folding horn through the setting, draws in the fuselage side in with the horn that stretches out, and can fold screw and undercarriage, and occupation space is less during unmanned aerial vehicle closed state, accomodates and carries more conveniently.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required to be used in the embodiments are briefly introduced below, and the drawings in the following description are only corresponding drawings of some embodiments of the present invention.
Fig. 1 is the utility model discloses a structure schematic diagram during portable unmanned aerial vehicle's expansion state.
Fig. 2 is the utility model discloses a structure schematic diagram during portable unmanned aerial vehicle's closed state.
Fig. 3 is the utility model discloses a structure schematic diagram of portable unmanned aerial vehicle's fuselage.
Fig. 4 is the utility model discloses a portable unmanned aerial vehicle unpacks apart the structure schematic diagram of safety cover and battery case.
Fig. 5 is the utility model discloses a portable unmanned aerial vehicle's the module of making a video recording's structure schematic diagram.
Fig. 6 is the utility model discloses a portable unmanned aerial vehicle's the explosion-proof structure schematic diagram of the module of making a video recording.
The camera comprises a main body 1, a main body 2, a front arm 3, a rear arm 4, a front power device 5, a rear power device 6, a front landing gear 7, a rear landing gear 8, a camera module 11, a front connecting groove 12, a rear connecting groove 13, a battery bin 14, a battery box 41, a first motor 42, a first wing 43, a first connecting plate 51, a second motor 52, a second wing 53, a second connecting plate 81, a protective cover 82, a camera base 83, a rotating table 84, a connecting seat 85, a camera 111, a first front baffle surface 112, a second front baffle surface 121, a first rear baffle surface 122, a second rear baffle surface 821, a first limiting block 841 and a second limiting block.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by the skilled in the art without creative work belong to the protection scope of the present invention.
In the present invention, the directional terms, such as "up", "down", "front", "back", "left", "right", "inner", "outer", "side", "top" and "bottom", refer to the orientation of the drawings, and the directional terms are used for illustration and understanding, but not for limiting the present invention.
The terms "first," "second," and the like in the terms of the present invention are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, nor should they be construed as limiting in any way.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
Unmanned aerial vehicle among the prior art exists more that the volume is great, carries inconveniently.
Following do the utility model provides a pair of can solve above technical problem's portable unmanned aerial vehicle's preferred embodiment.
Please refer to fig. 1 and fig. 2, wherein fig. 1 is a schematic structural diagram of the portable unmanned aerial vehicle in the unfolded state, and fig. 2 is a schematic structural diagram of the portable unmanned aerial vehicle in the closed state.
In the drawings, elements having similar structures are denoted by the same reference numerals.
The utility model provides a portable unmanned aerial vehicle, which comprises a body 1, a front arm 2, a rear arm 3, a front power device 4 and a rear power device 5; the two side surfaces of the machine body 1 are provided with front connecting grooves 11 at positions close to the end parts, the two side surfaces are far away from the front connecting grooves 11 and are provided with rear connecting grooves 12 at positions close to the other end parts of the machine body 1, and the rear connecting grooves 12 and the front connecting grooves 11 are used for connection; one end of the front arm 2 is hinged in the front connecting groove 11 and used for connection; one end of the rear arm 3 is hinged in the rear connecting groove 12 and used for connection; the front power device 4 is connected to one end, far away from the front connecting groove 11, of the front arm 2 and used for driving the unmanned aerial vehicle to fly; the rear power device 5 is connected to one end of the rear arm 3, which is far away from the rear connecting groove 12, and is used for driving the unmanned aerial vehicle to fly. A front undercarriage 6 is arranged on the lower side of one end, far away from the front connecting groove 11, of the front arm 2, a rear undercarriage 7 is arranged on the lower side of one end, far away from the rear connecting groove 12, of the rear arm 3, and the front undercarriage 6 and the rear undercarriage 7 are used for supporting the unmanned aerial vehicle during rising and falling; the nose landing gear 6 is connected on the nose horn 2 in a bending way, and the rear landing gear 7 is connected on the rear horn 3 in a bending way, and the nose horn 2 is connected the nose landing gear 6 position and is provided with first draw-in groove, and the nose landing gear 6 articulates in first draw-in groove, and the rear landing gear 7 position is connected to the rear horn 3 and is provided with the second draw-in groove, and the rear landing gear 7 articulates in the second draw-in groove.
When the portable unmanned aerial vehicle is in a closed state, as shown in fig. 2, the upper surface of the body 1 is arc-shaped, the middle of the body 1 is narrower than two ends in the length direction, after the front arm 2 and the rear arm 3 are folded, the middle of the body 1 is narrower, and the front power device 4 and the rear power device 5 are just placed, one end of the front arm 2, which is far away from the front connecting groove 11, is contacted with the middle of the body 1, one end of the rear arm 3, which is far away from the rear connecting groove 12, is contacted with the middle of the body 1, one end of the front undercarriage 6, which is far away from the front power device 4, is contacted with the lower end of the front arm 2, and one end of; when the portable unmanned aerial vehicle is in an unfolding state, as shown in fig. 1, one end of a front arm 2, which is far away from a front connecting groove 11, is far away from the middle of a machine body 1, one end of a rear arm 3, which is far away from a rear connecting groove 12, is far away from the middle of the machine body 1, the front arm 2 and the rear arm 3 are in a peripheral divergence shape on the machine body 1, an included angle between the extension direction of a nose landing gear 6 and the lower end face of the front arm 2 is 90-120 degrees, an included angle between the extension direction of a rear landing gear 7 and the lower end face of the rear arm 3 is 90-120 degrees, the nose landing gear 6 and the rear.
Referring to fig. 3, fig. 3 is the structure diagram of the body of the portable unmanned aerial vehicle of the present invention. The front connecting groove 11 comprises a first front blocking surface 111 and a second front blocking surface 112, wherein the first front blocking surface 111 is in a vertical direction and is parallel to the length direction of the machine body 1 and used for limiting the rotation of the front machine arm 2; the second front blocking surface 112 is a vertical arc surface, is connected with the first front blocking surface 111, and is used for limiting the rotation of the front horn 2; when the portable unmanned aerial vehicle is in the closed state, the front arm 2 contacts the first front blocking surface 111; when the portable unmanned aerial vehicle is in the unfolding state, the front arm 2 contacts the tail end of the second front baffle surface 112, and the included angle between the axis of the front arm 2 and the first front baffle surface 111 is 90-135 degrees.
The rear connecting groove 12 comprises a first rear blocking surface 121 and a second rear blocking surface 122, wherein the first rear blocking surface 121 is in a vertical direction and is parallel to the length direction of the machine body 1 and used for limiting the rotation of the rear machine arm 3; the second rear blocking surface 122 is a circular arc surface in the vertical direction, is connected with the first rear blocking surface 121, and is used for limiting the rotation of the rear arm 3; when the portable unmanned aerial vehicle is in the closed state, the rear arm 3 contacts the first rear blocking surface 121; when the portable unmanned aerial vehicle is in the unfolded state, the rear arm 3 contacts the end of the second rear blocking surface 122, and the included angle between the axis of the rear arm 3 and the first rear blocking surface 121 is 90-135 degrees. Keep off face 112 and second back fender face 122 before setting up the second, the expansion degree of preceding horn 2 and back horn 3 is limited, and convenient preceding horn 2 is stabilized the card in preceding spread groove 11, and back horn 3 is stabilized the card in back spread groove 12, and unmanned aerial vehicle flight process is stable.
Referring to fig. 1 and 2, the front power device 4 includes a first motor 41 and a first propeller, the first propeller is connected to an upper side of the first motor 41, and the first motor 41 is used for driving the first propeller to rotate; the first propeller comprises a first wing 42 and a first connecting plate 43, the two first wings 42 are hinged on two sides of the first connecting plate 43, and the first connecting plate 43 is connected to the first motor 41; the rear power device 5 comprises a second motor 51 and a second propeller, the second propeller is connected to the upper side of the second motor 51, and the second motor 51 is used for driving the second propeller to rotate; the second screw includes second wing 52 and second connecting plate 53, and two second wings 52 articulate in second connecting plate 53 both sides, and second connecting plate 53 is connected on second motor 51, sets up folding screw, and when unmanned aerial vehicle was located the closure state, first wing 42 and second wing 52 all can draw in and be close to fuselage 1 department, and the whole occupation space of unmanned aerial vehicle reduces, accomodates the convenience.
Referring to fig. 4, fig. 4 is the utility model discloses a portable unmanned aerial vehicle unpacks apart the structural schematic diagram of safety cover and battery case. 2 downside of fuselage is provided with camera module 8 and safety cover 81, camera module 8 is close to preceding spread groove 11 position with safety cover 81, camera module 8 is used for making a video recording, safety cover 81 is used for protecting camera module 8, safety cover 81 detachable sets up on the fuselage 1, including protection skull and protection tail-hood, protection skull and protection tail-hood are articulated, protection tail-hood is kept away from protection skull one end and is provided with the buckle spare, it is provided with the buckle recess to correspond the buckle spare on the fuselage 1, the buckle spare is used for the joint in the buckle recess, make things convenient for the dismantlement of safety cover 81. 1 lower extreme middle part of fuselage is provided with battery compartment 13 and battery case 14, and battery compartment 13 is the square groove form, and battery case 14 is the cuboid structure, and battery case 14 is connected in battery compartment 13 through buckle connected mode, and battery case 14 is used for providing the power for unmanned aerial vehicle.
Referring to fig. 5 and fig. 6, wherein fig. 5 is the utility model discloses a portable unmanned aerial vehicle's the structure schematic diagram of the module of making a video recording, fig. 6 is the utility model discloses a portable unmanned aerial vehicle's the explosion structure schematic diagram of the module of making a video recording.
The camera module 8 comprises a camera base 82, a rotary table 83, a connecting seat 84 and a camera 85, wherein the camera base 82 is connected to the machine body 1 for connection; the rotating platform 83 is of an L-shaped structure, two ends of the rotating platform are provided with rotating motors, the axes of the two rotating motors are perpendicular to each other, and the rotating platform 83 is connected to the camera base 82 through the rotating motors and used for expanding the visual field; the connecting base 84 is a U-shaped structure, one end of which is open, and the other end of which is connected with a rotating motor on the rotating platform 83 far away from the camera base 82 for connection; the camera 85 is connected in the opening of the connecting seat 84 and used for shooting; the camera base 82 is provided with a first limiting block 821 on one side close to the rotating platform 83, the connecting base 84 is provided with a second limiting block 841 on one side close to the rotating platform 83, and the first limiting block 821 and the second limiting block 841 are used for limiting the rotating scale of the rotating platform 83.
The utility model discloses a theory of operation: take out unmanned aerial vehicle, unmanned aerial vehicle initial state is the closure state, launch fore horn 2 and rear horn 3 respectively, launch nose landing gear 6 and rear landing gear 7 respectively again, launch first screw and second screw again, take off safety cover 81, install battery case 14 in the battery compartment 13, place nose landing gear 6 and rear landing gear 7 at the horizontal plane down, battery case 14 provides the power for unmanned aerial vehicle, drive the operation of fore-going power device 4 and rear power device 5, and then drive the flight of unmanned aerial vehicle, the use is controlled unmanned aerial vehicle's flight with the supporting remote controller of unmanned aerial vehicle.
This completes the use process of the portable drone of the preferred embodiment.
In summary, although the present invention has been described with reference to the preferred embodiments, the above-described preferred embodiments are not intended to limit the present invention, and those skilled in the art can make various changes and modifications without departing from the spirit and scope of the present invention, so that the scope of the present invention shall be determined by the scope of the appended claims.
Claims (10)
1. A portable unmanned aerial vehicle, comprising:
the device comprises a machine body, wherein front connecting grooves are formed in positions, close to end parts, of two side surfaces, rear connecting grooves are formed in positions, far away from the front connecting grooves, close to the other end part of the machine body, of the two side surfaces, and the rear connecting grooves and the front connecting grooves are used for connection;
one end of the front machine arm is hinged in the front connecting groove and used for connection;
one end of the rear arm is hinged in the rear connecting groove and used for connection;
the front power device is connected to one end, far away from the front connecting groove, of the front arm and is used for driving the unmanned aerial vehicle to fly;
the rear power device is connected to one end, far away from the rear connecting groove, of the rear arm and is used for driving the unmanned aerial vehicle to fly;
the portable unmanned aerial vehicle comprises a closed state and an expanded state, when the portable unmanned aerial vehicle is in the closed state, one end, far away from the front connecting groove, of the front arm is in contact with the middle of the vehicle body, and one end, far away from the rear connecting groove, of the rear arm is in contact with the middle of the vehicle body;
when portable unmanned aerial vehicle is located the expansion state, preceding horn is kept away from preceding spread groove one end and is kept away from the fuselage middle part, back horn is kept away from back spread groove one end and is kept away from the fuselage middle part, and preceding horn is with the back horn and is diverged the shape on the fuselage.
2. The portable unmanned aerial vehicle of claim 1, wherein a nose landing gear is arranged on the lower side of one end of the nose arm, which is far away from the front connecting groove, and a rear landing gear is arranged on the lower side of one end of the rear arm, which is far away from the rear connecting groove, and the nose landing gear and the rear landing gear are used for supporting the unmanned aerial vehicle during rising and falling;
the nose landing gear is connected on the nose horn in a bending mode, and the rear landing gear is connected on the rear horn in a bending mode.
3. The portable drone of claim 1, wherein the front attachment slot includes:
the first front blocking surface is vertical to the machine body, parallel to the length direction of the machine body and used for limiting the rotation of the front machine arm;
the second front blocking surface is a circular arc surface in the vertical direction, is connected with the first front blocking surface and is used for limiting the rotation of the front horn;
when the portable unmanned aerial vehicle is in a closed state, a front arm contacts the first front blocking surface;
when the portable unmanned aerial vehicle is in the unfolding state, the front arm contacts the tail end of the second front blocking surface, and the included angle between the axis of the front arm and the first front blocking surface is 90-135 degrees.
4. The portable drone of claim 1, wherein the rear attachment slot includes:
the first rear blocking surface is vertical to the machine body, parallel to the length direction of the machine body and used for limiting the rotation of the rear machine arm;
the second rear blocking surface is a circular arc surface in the vertical direction, is connected with the first rear blocking surface and is used for limiting the rotation of the rear arm;
when the portable unmanned aerial vehicle is in a closed state, the rear arm contacts the first rear blocking surface;
when the portable unmanned aerial vehicle is in the unfolding state, the rear arm contacts the tail end of the second rear blocking surface, and the included angle between the axis of the rear arm and the first rear blocking surface is 90-135 degrees.
5. The portable unmanned aerial vehicle of claim 1, wherein the upper surface of the body is arc-shaped, and the body is narrower in the middle than at both ends in the length direction.
6. The portable unmanned aerial vehicle of claim 1, wherein the front power device comprises a first motor and a first propeller, the first propeller is connected to the upper side of the first motor, and the first motor is used for driving the first propeller to rotate;
the rear power device comprises a second motor and a second propeller, the second propeller is connected to the upper side of the second motor, and the second motor is used for driving the second propeller to rotate.
7. The portable drone of claim 6, wherein the first propeller includes a first wing and a first connection plate, both of the first wings hinged on either side of the first connection plate, the first connection plate connected to the first motor;
the second propeller comprises a second wing and a second connecting plate, the two second wings are hinged to two sides of the second connecting plate, and the second connecting plate is connected to the second motor.
8. The portable unmanned aerial vehicle of claim 1, wherein a camera module and a protective cover are arranged on the lower side of the body, the camera module and the protective cover are close to the front connecting groove, the camera module is used for taking a picture, and the protective cover is used for protecting the camera module.
9. The portable unmanned aerial vehicle of claim 8, wherein the camera module comprises:
the camera shooting base is connected to the body and used for connection;
the rotary table is of an L-shaped structure, two ends of the rotary table are provided with rotary motors, the axes of the two rotary motors are perpendicular to each other, and the rotary table is connected to the camera base through the rotary motors and used for expanding the visual field;
the connecting seat is of a U-shaped structure, one end of the connecting seat is opened, and the other end of the connecting seat is connected with a rotating motor which is far away from the base and is arranged on the rotating table and used for connection;
the camera is connected in the opening of the connecting seat and used for shooting;
be close to on the base of making a video recording revolving stage one side is provided with first stopper, be close to revolving stage one side on the connecting seat and be provided with the second stopper, first stopper and second stopper are used for restricting the rotatory yardstick of revolving stage.
10. The portable unmanned aerial vehicle of claim 1, wherein a battery compartment and a battery box are arranged in the middle of the lower end of the unmanned aerial vehicle body, the battery compartment is in a square groove shape, the battery box is in a cuboid structure, and the battery box is connected in the battery compartment in a buckling connection mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021053257.0U CN212243784U (en) | 2020-06-09 | 2020-06-09 | Portable unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021053257.0U CN212243784U (en) | 2020-06-09 | 2020-06-09 | Portable unmanned aerial vehicle |
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| CN212243784U true CN212243784U (en) | 2020-12-29 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115583332A (en) * | 2022-10-18 | 2023-01-10 | 李涛 | Unmanned aerial vehicle rotor beta structure and unmanned aerial vehicle |
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- 2020-06-09 CN CN202021053257.0U patent/CN212243784U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115583332A (en) * | 2022-10-18 | 2023-01-10 | 李涛 | Unmanned aerial vehicle rotor beta structure and unmanned aerial vehicle |
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