CN215098215U

CN215098215U - Cloud platform unmanned aerial vehicle

Info

Publication number: CN215098215U
Application number: CN202121269045.0U
Authority: CN
Inventors: 肖磊; 张佳佳; 赵振皓; 王敏娟; 周明; 陈香; 曹鸣
Original assignee: Jiangnan University
Current assignee: Jiangnan University
Priority date: 2021-06-07
Filing date: 2021-06-07
Publication date: 2021-12-10
Anticipated expiration: 2031-06-07

Abstract

The utility model belongs to the technical field of the unmanned air vehicle technique and specifically relates to a cloud platform unmanned aerial vehicle, including cloud platform and unmanned aerial vehicle, the detachable one end of installing at unmanned aerial vehicle of cloud platform, unmanned aerial vehicle includes the body and installs the flexible unit in the body both sides, be equipped with the master switch on the body, shooting switch and cloud platform position remote sensing that control cloud platform was shot, be equipped with the mouth that charges on the body, the inside battery that is equipped with of body, flexible unit includes the wing arm, a plurality of rotor arms and a plurality of rotary unit, the both sides of body are equipped with the holding tank, rotary unit installs on the wing arm, rotary unit includes the motor, mount pad and two folding arms, the rotor arm is rotatable to following two kinds of states: the first state is a contraction state, namely the rotating arm, the wing arm and the folding arm in a folding state are accommodated in the accommodating groove; the second state is the expansion state, and the rotor arm expandes promptly and makes two wing arm overhangs in the both sides of body, and this application can realize handheld cloud platform and unmanned aerial vehicle and shoot difunctional, and it is comparatively convenient to use.

Description

Cloud platform unmanned aerial vehicle

Technical Field

The utility model belongs to the technical field of the unmanned air vehicle technique and specifically relates to a cloud platform unmanned aerial vehicle.

Background

At present, cloud platform unmanned aerial vehicle uses comparatively extensively as a shooting equipment in daily life, and current cloud platform unmanned aerial vehicle majority is inconvenient to be carried, and the formula as an organic whole between cloud platform and the unmanned aerial vehicle, and the installation is inconvenient with the dismantlement, is not convenient for accomodate, also can lead to carrying inconveniently.

SUMMERY OF THE UTILITY MODEL

The applicant provides a cloud platform unmanned aerial vehicle who conveniently carries to the shortcoming among the above-mentioned prior production technique, realizes handheld cloud platform and unmanned aerial vehicle and shoots difunctional, and it is comparatively convenient to use.

The utility model discloses the technical scheme who adopts as follows: a tripod head unmanned aerial vehicle comprises a tripod head and an unmanned aerial vehicle, wherein the tripod head is detachably arranged at one end of the unmanned aerial vehicle, the unmanned aerial vehicle comprises a body and telescopic units arranged at two sides of the body, a main switch, a shooting switch for controlling shooting of the tripod head and tripod head azimuth remote sensing are arranged on the body, a charging port is arranged on the body, a storage battery is arranged in the body, the telescopic units comprise a wing arm, a plurality of rotating arms and a plurality of rotating units, one end of each rotating arm is hinged on the wing arm, the other end articulates on the body, and the both sides of body are equipped with the holding tank, and rotary unit installs on the wing arm, and rotary unit includes motor, mount pad and two folding arms, and two folding arms are articulated to be installed on the mount pad and two folding arms are rotatable to fold condition or expand and be a rectilinear state, and the motor is used for driving the mount pad and rotates, and the rotor arm is rotatable to following two kinds of states: the first state is a contraction state, namely the rotating arm, the wing arm and the folding arm in a folding state are accommodated in the accommodating groove; the second state is a deployed state, i.e. the rotor arms are deployed such that both arms overhang the body.

As a further improvement of the above technical solution:

the utility model discloses a battery contact point of unmanned aerial vehicle, including the base, the base is equipped with the terminal surface of base, the terminal surface of base is equipped with the connecting portion of hollow cylindricality on the terminal surface of the installation end of cloud platform, the ring channel is seted up to the one end of body, screw thread one is seted up to the interior week lateral wall of ring channel, screw thread two is seted up to the interior perisporium of connecting portion, connecting portion assign in the ring channel and realize detachable connection through threaded connection, the outer terminal surface face of the body that is located ring channel center department is equipped with bellied battery contact one, be equipped with bellied battery contact two on the terminal surface of the inside cloud platform installation end of connecting portion, during connecting portion and ring channel threaded connection, battery contact one and battery contact two contact realize cloud platform and unmanned aerial vehicle's electricity and be connected.

The body is the casing of button head parallel key type, and the both sides face department of casing is equipped with the holding tank, the wing arm includes that the inboard lateral buckling of the one end of rectangular shape casing section and rectangular shape casing section forms the arc casing section, and the inboard of rectangular shape casing section is seted up along length direction and is dodged the rotor arm pivoted bar and dodge the groove, when the rotor arm rotates to the shrink state, the rectangular shape casing section of two wing arms is accomodate to corresponding in the holding tank, the arc casing section overhang of two wing arms is outside the holding tank, the terminal surface of the arc casing section of two wing arms pastes and leans on and arc casing section and cloud platform distribute in the both ends department of body mutually.

The body is provided with a plug-in port, an audio controller is inserted into the plug-in port, the audio controller is provided with a hook, and an audio receiver matched with the audio controller is arranged inside the body.

Every flexible unit includes two rotor arms and two rotary unit, two cylinders of vertical fixation between the mounting panel that the mount pad includes two parallels and two mounting panels, and the one end of two folding arms is established respectively on the cylinder, and two folding arms can rotate to fold condition or expand to be a rectilinear state round the cylinder, and the motor is installed in the casing of wing arm, and the mount pad overhang is in one side of wing arm, and when two folding arms were folding together, two parallel clearances of folding arm were arranged in one side of wing arm.

The utility model has the advantages as follows: this application has mainly fused handheld cloud platform and unmanned aerial vehicle and has shot two kinds of functions, and when this application was not used, accomodate the folding arm of rotor arm, wing arm and fold condition to the holding tank of body in, the volume is less, conveniently carries, also can revolve to twist the cloud platform soon and pull down it from unmanned aerial vehicle, reduces whole length, also does benefit to and carries.

Drawings

Fig. 1 is the utility model discloses unmanned aerial vehicle's structure graph.

Fig. 2 is a structural view of the head.

Fig. 3-5 are the structural diagrams of the present invention in different states.

Fig. 6 is a structural view of the rotating unit.

Wherein: 10. a holder; 11. a connecting portion; 12. a battery contact II; 21. a body; 211. accommodating grooves; 212. a shooting switch; 213. a master switch; 214. remote sensing of the azimuth of the holder; 22. a wing arm; 221. an elongate housing section; 222. an arcuate shell section; 223. an avoidance groove; 23. a rotating arm; 24. a mounting seat; 241. mounting a plate; 25. a folding arm; 26. an annular groove; 27. a first battery contact; 28. a motor; 30. an audio controller; 31. and (4) hanging hooks.

Detailed Description

The following describes embodiments of the present invention with reference to the drawings.

As shown in fig. 1-6, the pan/tilt/unmanned aerial vehicle of this embodiment comprises a pan/tilt head 10 and an unmanned aerial vehicle, the pan/tilt head 10 is detachably mounted at one end of the unmanned aerial vehicle, the unmanned aerial vehicle comprises a body 21 and telescopic units mounted at both sides of the body 21, the body 21 is provided with a main switch 213, a shooting switch 212 for controlling shooting by the pan/tilt head 10 and a pan/tilt/azimuth remote sensing 214, the body 21 is provided with a charging port, the body 21 is internally provided with a storage battery, the telescopic units comprise a wing arm 22, a plurality of rotating arms 23 and a plurality of rotating units, one end of each rotating arm 23 is hinged on the wing arm 22, the other end is hinged on the body 21, both sides of the body 21 are provided with a holding groove 211, the rotating units are mounted on the wing arm 22, the rotating units comprise a motor 28, a mounting seat 24 and two folding arms 25, the two folding arms 25 are hinged on the mounting seat 24, and the two folding arms 25 can be rotated to a folded state or unfolded to form a straight line state, the motor 28 is used to drive the mounting seat 24 to rotate, and the rotating arm 23 can rotate to the following two states: the state of the third embodiment is a contracted state in which the rotating arm 23, the wing arm 22 and the folded arm 25 in the folded state are received in the receiving groove 211; the second state is a deployed state in which the rotor arms 23 are deployed so that the two wing arms 22 overhang the body 21.

Perpendicularly be equipped with hollow cylindricality connecting portion 11 on the terminal surface of cloud platform 10's installation end, ring channel 26 is seted up to the one end of body 21, screw thread one is seted up to ring channel 26's interior week lateral wall, screw thread two is seted up to connecting portion 11's interior perisporium, connecting portion 11 assigns into ring channel 26 and realizes detachable the connection through threaded connection, the outer terminal surface face of body 21 that is located ring channel 26 center department is equipped with bellied battery contact 27, be located and be equipped with bellied battery contact two 12 on the terminal surface of the inside cloud platform 10 installation end of connecting portion 11, during connecting portion 11 and ring channel 26 threaded connection, battery contact 27 and the contact of battery contact two 12 realize cloud platform 10 and unmanned aerial vehicle's electricity and are connected.

The body 21 is a round-head flat key type shell, and both sides of the shell are provided with accommodating grooves 211, the wing arms 22 include elongated shell sections 221 and arc-shaped shell sections 222 formed by bending one ends of the elongated shell sections 221 inwards, the inner sides of the elongated shell sections 221 are provided with strip-shaped avoiding grooves 223 avoiding the rotation of the rotating arms 23 along the length direction, when the rotating arms 23 rotate to the contraction state, the elongated shell sections 221 of the two wing arms 22 are accommodated in the corresponding accommodating grooves 211, the arc-shaped shell sections 222 of the two wing arms 22 are suspended outside the accommodating grooves 211, the end surfaces of the arc-shaped shell sections 222 of the two wing arms 22 are attached to each other, and the arc-shaped shell sections 222 and the pan/tilt head 10 are distributed at both ends of the body 21.

The body 21 is provided with a plug interface, an audio controller 30 is inserted into the plug interface, the audio controller 30 is provided with a hook 31, and the body 21 is internally provided with an audio receiver matched with the audio controller 30.

Each telescopic unit comprises two rotating arms 23 and two rotating units, the mounting seat 24 comprises two parallel mounting plates 241 and two columns vertically fixed between the two mounting plates 241, one ends of the two folding arms 25 are respectively sleeved on the columns, the two folding arms 25 can rotate to a folding state or unfold to be in a linear state around the columns, the motor 28 is mounted in the shell of the wing arm 22, the mounting seat 24 is suspended on one side of the wing arm 22, and when the two folding arms 25 are folded together, the two folding arms 25 are arranged on one side of the wing arm 22 in a parallel gap mode.

When specifically processing, this application can be through software, hardware design for this application adaptation is in cell-phone APP, through the action of cell-phone APP control this application.

This application has mainly fused handheld cloud platform and unmanned aerial vehicle and has shot two kinds of functions.

When as handheld cloud platform use: the rotary arm 23, the wing arm 22, and the folded arm 25 are accommodated in the accommodating groove 211 of the main body 21, the main switch 213 is turned on, and the pan/tilt head 10 is controlled by the photographing switch 212 to photograph. Is more convenient.

When shooting as unmanned aerial vehicle and using: directly seizing two wing arms 22 and outwards pulling with the hand, rotor arm 23 expandes, two wing arms 22 remove to the both sides of body 21, two folding arms 25 that rotate every rotary unit with the hand expand to being a rectilinear state, starter motor 28, motor 28 drives mount pad 24 and two folding arms 25 and together rotates, thereby it rises together to drive cloud platform 10 and unmanned aerial vehicle, can utilize cell-phone APP to control this moment, perhaps utilize audio controller 30 to carry out speech control and shoot, it is comparatively convenient.

This application is as when unmanned aerial vehicle shoots the use, need take out audio controller 30 from body 21, utilizes couple 31 to hang audio controller 30 on the clothes, makes things convenient for pronunciation. The audio controller 30 is inserted into the socket and can be fixed by magnetic attraction.

When this application does not use, accomodate rotor arm 23, wing arm 22 and fold condition's folding arm 25 to body 21's holding tank 211, the volume is less, conveniently carries, also can twist soon to revolve cloud platform 10 and pull down it from unmanned aerial vehicle, reduces whole length, also does benefit to and carries.

The above description is for the purpose of explanation and not limitation of the invention, which is defined in the claims, and any modifications may be made within the scope of the invention.

Claims

1. The utility model provides a cloud platform unmanned aerial vehicle which characterized in that: including cloud platform (10) and unmanned aerial vehicle, the detachable one end of installing at unmanned aerial vehicle in cloud platform (10), unmanned aerial vehicle includes body (21) and installs the flexible unit in body (21) both sides, be equipped with master switch (213) on body (21), shooting switch (212) and cloud platform position remote sensing (214) that control cloud platform (10) were shot, be equipped with the mouth that charges on body (21), the inside battery that is equipped with of body (21), flexible unit includes wing arm (22), a plurality of rotor arms (23) and a plurality of rotary unit, wherein one end of every rotor arm (23) articulates on wing arm (22), the other end articulates on body (21), the both sides of body (21) are equipped with holding tank (211), rotary unit installs on wing arm (22), rotary unit includes motor (28), mount pad (24) and two folding arms (25), two folding arms (25) are articulated to installing on mount pad (24) and two folding arms (25) are to fold condition or exhibition to fold or exhibition condition The opening is in a straight line state, the motor (28) is used for driving the mounting seat (24) to rotate, and the rotating arm (23) can rotate to the following two states: the first state is a contraction state, namely the rotating arm (23), the wing arm (22) and the folding arm (25) in a folding state are accommodated in the accommodating groove (211); the second state is a deployed state, namely, the rotating arms (23) are deployed so that the two wing arms (22) are suspended on two sides of the body (21).

2. The pan-tilt-unmanned aerial vehicle of claim 1, wherein: perpendicularly be equipped with hollow cylindricality connecting portion (11) on the terminal surface of the installation end of cloud platform (10), ring channel (26) are seted up to the one end of body (21), screw thread one is seted up to the interior week lateral wall of ring channel (26), screw thread two is seted up to the interior perisporium of connecting portion (11), connecting portion (11) are inserted in ring channel (26) and are realized detachable the connection through threaded connection, the outer terminal surface face that is located body (21) of ring channel (26) center department is equipped with bellied battery contact one (27), be located and be equipped with bellied battery contact two (12) on the terminal surface of cloud platform (10) installation end of connecting portion (11) inside, when connecting portion (11) and ring channel (26) threaded connection, battery contact one (27) and battery contact two (12) contact realize cloud platform (10) and unmanned aerial vehicle's electricity and are connected.

3. The pan-tilt-unmanned aerial vehicle of claim 2, wherein: the body (21) is the casing of button head flat key type, and the both sides face department of casing is equipped with holding tank (211), wing arm (22) include that the inboard lateral buckling of one end of rectangular shape casing section (221) and rectangular shape casing section (221) forms arc casing section (222), the inboard of rectangular shape casing section (221) is seted up along length direction and is dodged rotor arm (23) pivoted bar and dodged groove (223), when rotor arm (23) rotate to the shrink state, rectangular shape casing section (221) of two wing arms (22) are accomodate to corresponding in holding tank (211), arc casing section (222) overhang of two wing arms (22) are outside holding tank (211), the terminal surface of arc casing section (222) of two wing arms (22) is paste and arc casing section (222) and cloud platform (10) distribute at the both ends department of body (21).

4. The pan-tilt-unmanned aerial vehicle of claim 1, wherein: the body (21) is provided with a plug-in port, an audio controller (30) is inserted into the plug-in port, the audio controller (30) is provided with a hook (31), and an audio receiver matched with the audio controller (30) is arranged inside the body (21).

5. A pan-tilt-unmanned aerial vehicle according to claim 3, wherein: every flexible unit includes two rotor arms (23) and two rotary unit, mount pad (24) include two columns of vertical fixation between two parallel mounting panel (241) and two mounting panel (241), the one end cover respectively of two folding arms (25) is established on the column, two folding arms (25) can rotate to fold condition or expand and be a rectilinear state round the column, motor (28) are installed in the casing of wing arm (22), mount pad (24) overhang is in one side of wing arm (22), when two folding arms (25) are folded together, two folding arm (25) parallel clearance arrange in one side of wing arm (22).