CN209739315U - Many rotor unmanned aerial vehicle horn installed part - Google Patents

Many rotor unmanned aerial vehicle horn installed part Download PDF

Info

Publication number
CN209739315U
CN209739315U CN201920486614.3U CN201920486614U CN209739315U CN 209739315 U CN209739315 U CN 209739315U CN 201920486614 U CN201920486614 U CN 201920486614U CN 209739315 U CN209739315 U CN 209739315U
Authority
CN
China
Prior art keywords
horn
aerial vehicle
unmanned aerial
upper plate
pipe clamp
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
Application number
CN201920486614.3U
Other languages
Chinese (zh)
Inventor
张杨
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhejiang Yihang Technology Co Ltd
Original Assignee
Zhejiang Yihang Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Zhejiang Yihang Technology Co Ltd filed Critical Zhejiang Yihang Technology Co Ltd
Priority to CN201920486614.3U priority Critical patent/CN209739315U/en
Application granted granted Critical
Publication of CN209739315U publication Critical patent/CN209739315U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Landscapes

  • Suspension Of Electric Lines Or Cables (AREA)

Abstract

The utility model relates to a many rotor unmanned aerial vehicle horn installed part, including upper plate and hypoplastron, the last horn pipe clamp of half tubular structure is formed in the downward bending of upper plate side, hypoplastron side kickup forms half tubular lower horn pipe clamp. The structure is simple and light, the weight of the device is reduced, the operation is convenient, compared with the prior art, the number of parts is less, the assembly is convenient, the structure is reliable, and other parts can be installed at the horizontal position.

Description

Many rotor unmanned aerial vehicle horn installed part
Technical Field
The utility model relates to an unmanned aerial vehicle field, in particular to unmanned aerial vehicle's horn installed part.
Background
A drone is an unmanned flying device that is operated using a radio remote control device and a self-contained program control device. With the continuous progress of present science and technology, the rapid development of society, the applicable technique in the unmanned aerial vehicle field is gradually ripe day by day, and unmanned aerial vehicle equipment also has good application prospect in fields such as public safety, transportation, farming, commodity circulation transportation.
In recent years, multiple rotors are widely used due to the reasons of high cost-effectiveness ratio, no casualties and the like, the existing multiple-rotor motor arms are in two modes, one mode is a shell integrated mode, but the size is too large, the transportation is not facilitated, in addition, the mold opening cost is high, the other mode is a detachable or foldable motor arm, hollow and high-strength materials such as carbon fiber tubes and the like are generally selected as the motor arm in the mode, and when the motor arm is installed, the motor arm can be directly connected with a machine body, the structure is complex, the maintenance is difficult, and the reliability is low.
patent CN201721076158.2 discloses an unmanned aerial vehicle horn installation mechanism, and the prior art discloses an unmanned aerial vehicle horn installation mechanism, which comprises a horn, a limit mechanism, a base and a horn rotating shaft; the machine arm rotating shaft is arranged on the base, the machine arm comprises a first end and a second end, the first end of the machine arm penetrates through the machine arm rotating shaft and is connected with the base, and the second end of the machine arm is rotated to enable the machine arm to rotate along the machine arm rotating shaft; the limiting mechanism is arranged on the base; when the horn rotates to the horizontal direction, stop gear limits the first end home range of horn. The above-disclosed technique is used for fixing the horn, but the structure is complicated and inconvenient to install and disassemble.
Disclosure of Invention
The utility model aims at providing a simple structure, simple installation's unmanned aerial vehicle horn installation mechanism.
The utility model provides a many rotor unmanned aerial vehicle horn installed part, including upper plate and hypoplastron, the last horn pipe clamp of half tubular structure is formed in the downward bending of upper plate side, hypoplastron side kickup forms half tubular lower horn pipe clamp.
The upper plate and the lower plate form an upper arm pipe clamp and a lower arm pipe clamp, and the upper arm pipe clamp and the lower arm pipe clamp are used for fixing the arm.
Preferably, the upper arm pipe clamps and the lower arm pipe clamps are arranged in a one-to-one correspondence manner.
Preferably, the number of the upper arm pipe clamps and the lower arm pipe clamps is 4-12.
Preferably, the upper arm clamp and the lower arm clamp may be integrally pressed by using an upper plate and a lower plate.
preferably, the upper arm clamp and the lower arm clamp may be welded to the upper plate and the lower plate.
Preferably, the upper arm pipe clamp and the lower arm pipe clamp extend towards the side edge to be provided with a connecting seat.
Preferably, the connecting base is vertically arranged on the side wall of the upper machine arm pipe clamp and the side wall of the lower machine arm pipe clamp.
Preferably, the connecting seat on the upper arm pipe clamp and the connecting seat on the lower arm pipe clamp are correspondingly arranged.
Preferably, the connecting seats on two sides of the upper machine arm pipe clamp are symmetrically arranged, and the connecting seats on two sides of the lower machine arm pipe clamp are symmetrically arranged.
Preferably, the upper and lower gripper arms may fit together to form a tubular mechanical gripper for placing the robotic arm.
Preferably, the tubular mechanical pipe clamp can adopt a round pipe or a square pipe.
Preferably, the connecting seat is provided with a connecting hole.
Preferably, the connecting hole is internally provided with a thread.
Preferably, the connection of the upper plate and the lower plate is fixed by bolts and nuts through the connection holes.
the above structure fixes the relative position of the upper plate and the lower plate by the connection between the connection holes through the bolt and the nut.
Preferably, the middle parts of the upper plate and the lower plate are provided with wire passing holes.
The wire passing hole is used for passing through an electric wire in the use process after the machine arm is installed.
Preferably, the upper plate and the lower plate are provided with mounting holes.
The mounting hole is used for mounting and fixing the horn mounting piece on the unmanned aerial vehicle.
Preferably, the mounting hole is arranged at the edge of the wire passing hole.
Preferably, the number of the mounting holes can be 4-12.
Preferably, the upper arm pipe clamp and the lower arm pipe clamp are provided with arm fixing holes.
The horn fixing hole is used for mounting and fixing the horn, and the mounting strength of the horn is enhanced.
Preferably, the overlapping ratio of the vertical projection area of the upper plate and the vertical projection area of the lower plate is 85% -100%.
Above-mentioned structure can make upper plate and hypoplastron form better lock and press from both sides tight effect to the horn, and the structure has better stability.
Preferably, the upper plate and the lower plate are flat plates.
Preferably, the unbent portions of the upper and lower plates remain in a flat plate structure.
Preferably, the angle formed between each part of the flat plate structure is-5 degrees.
Above-mentioned upper plate and hypoplastron unbent part keep the flat plate structure for the convenience of device installs on unmanned aerial vehicle.
Preferably, the material selected for the device is aluminum alloy 6061.
The device adopts aluminum alloy 6061, so that the device has the advantages of good processing performance, excellent welding characteristic, electroplating property, good corrosion resistance, high toughness, no deformation after processing and the like.
To sum up, the utility model discloses following beneficial effect has:
1. The structure is simple and light, the weight of the device is reduced, the operation is convenient, and the flying is convenient.
2. Compared with the prior art, the structure has the advantages of fewer parts, convenient assembly, reliable structure and capability of installing other parts in the horizontal position.
3. The upper plate and the lower plate of the structure are the same, so that the production cost can be relatively reduced, and the number of the pipe clamps can be increased or reduced according to actual requirements.
Drawings
Fig. 1 is a schematic structural view of a multi-rotor unmanned aerial vehicle horn mounting member of the present invention;
Fig. 2 is a side view of a multi-rotor drone horn mount of the present invention;
Figure 3 is the utility model relates to a top view of many rotor unmanned aerial vehicle horn installed part.
In the figure: 1-upper plate, 2-lower plate, 11-upper arm pipe clamp, 12-lower arm pipe clamp, 13-connecting seat, 131-connecting hole, 14-wire passing hole, 15-mounting hole and 16-arm fixing hole.
Detailed Description
The present embodiment is only for explaining the present invention, and it is not limited to the present invention, and those skilled in the art can make modifications to the present embodiment without inventive contribution as required after reading the present specification, but all of them are protected by patent laws within the scope of the claims of the present invention.
The following are specific embodiments of the present invention and the accompanying drawings are used to further describe the technical solution of the present invention, but the present invention is not limited to these embodiments.
Referring to FIGS. 1-3;
The first embodiment is as follows:
As shown in fig. 1-3, the multi-rotor unmanned aerial vehicle horn mounting piece comprises an upper plate 1 and a lower plate 2, wherein the side edge of the upper plate 1 is bent downwards to form an upper horn pipe clamp 11 in a semi-tubular structure, and the side edge of the lower plate 2 is bent upwards to form a lower horn pipe clamp 12 in a semi-tubular structure.
The upper plate 1 and the lower plate 2 form an upper arm pipe clamp 11 and a lower arm pipe clamp 12, and the upper arm pipe clamp 11 and the lower arm pipe clamp 12 are used for fixing the arm.
The upper arm pipe clamps 11 and the lower arm pipe clamps 12 are arranged in a one-to-one correspondence manner.
The number of the upper arm clamps 11 and the lower arm clamps 12 is 4.
The upper arm clamp 11 and the lower arm clamp 12 may be integrally pressed by using the upper plate 1 and the lower plate 2.
The upper arm pipe clamp 11 and the lower arm pipe clamp 12 are provided with a connecting base 13 extending to the side.
The connecting base 13 is vertically arranged on the side wall of the upper arm pipe clamp 11 and the side wall of the lower arm pipe clamp 13.
The connecting base 13 on the upper arm pipe clamp 11 and the connecting base 13 on the lower arm pipe clamp 12 are correspondingly arranged.
The connecting seats 13 on two sides of the upper arm pipe clamp 11 are symmetrically arranged, and the connecting seats 13 on two sides of the lower arm pipe clamp 12 are symmetrically arranged.
The upper and lower boom pipe clamps 11, 12 may fit together to form a tubular mechanical pipe clamp for placing a robot arm.
The tubular mechanical pipe clamp can adopt a round pipe.
The connecting base 13 is provided with a connecting hole 131.
And the connecting hole 131 is internally provided with a thread.
The connection of the upper plate 1 and the lower plate 2 is fixed through the connection hole 131 by a bolt and a nut.
The above structure fixes the relative positions of the upper plate 1 and the lower plate 2 by the connection between the connection holes 131 through the bolts and nuts.
The middle parts of the upper plate 1 and the lower plate 2 are provided with wire passing holes 14.
The wire through hole 14 is used for passing through an electric wire in the use process after the installation of the machine arm is finished.
The upper plate 1 and the lower plate 2 are provided with mounting holes 15.
The structure is characterized in that the mounting hole 15 is used for mounting and fixing the mounting piece of the horn on the unmanned aerial vehicle.
The mounting hole 15 is arranged at the edge of the wire passing hole 14.
The number of the mounting holes 15 may be set to 4.
The upper arm pipe clamp 11 and the lower arm pipe clamp 12 are provided with arm fixing holes 16.
The horn fixing hole 16 is used for mounting and fixing the horn, and enhances the mounting strength of the horn.
The upper plate 1 and the lower plate 2 are correspondingly arranged.
The upper plate 1 and the lower plate 2 are flat plates.
The unbent portions of the upper plate 1 and the lower plate 2 are still of a flat plate structure.
The angle formed between each part of the flat plate structure is-5 degrees.
The above-mentioned upper plate 1 and 2 unbent part of hypoplastron keep the flat plate structure for the convenience of device installs on unmanned aerial vehicle.
The material selected for the device is aluminum alloy 6061.
Example two:
As shown in fig. 1-3, the multi-rotor unmanned aerial vehicle arm mounting member comprises an upper plate 1 and a lower plate 2, wherein the side edge of the upper plate 1 is bent downwards to form an upper arm pipe clamp 11 with a semi-tubular structure, and the side edge of the lower plate 2 is bent upwards to form a lower arm pipe clamp 12 with a semi-tubular structure.
The upper plate 1 and the lower plate 2 form an upper arm pipe clamp 11 and a lower arm pipe clamp 12, and the upper arm pipe clamp 11 and the lower arm pipe clamp 12 are used for fixing the arm.
The upper arm pipe clamps 11 and the lower arm pipe clamps 12 are arranged in a one-to-one correspondence manner.
The number of the upper arm clamps 11 and the lower arm clamps 12 is 4.
The upper arm clamp 11 and the lower arm clamp 12 may be welded to the upper plate 1 and the lower plate 2.
The upper arm pipe clamp 11 and the lower arm pipe clamp 12 are provided with a connecting base 13 extending to the side.
The connecting base 13 is vertically arranged on the side wall of the upper arm pipe clamp 11 and the side wall of the lower arm pipe clamp 13.
The connecting base 13 on the upper arm pipe clamp 11 and the connecting base 13 on the lower arm pipe clamp 12 are correspondingly arranged.
The connecting seats 13 on two sides of the upper arm pipe clamp 11 are symmetrically arranged, and the connecting seats 13 on two sides of the lower arm pipe clamp 12 are symmetrically arranged.
The upper and lower boom pipe clamps 11, 12 may fit together to form a tubular mechanical pipe clamp for placing a robot arm.
The tubular mechanical pipe clamp can adopt a round pipe.
the connecting base 13 is provided with a connecting hole 131.
And the connecting hole 131 is internally provided with a thread.
The connection of the upper plate 1 and the lower plate 2 is fixed through the connection hole 131 by a bolt and a nut.
The above structure fixes the relative positions of the upper plate 1 and the lower plate 2 by the connection between the connection holes 131 through the bolts and nuts.
The middle parts of the upper plate 1 and the lower plate 2 are provided with wire passing holes 14.
The wire through hole 14 is used for passing through an electric wire in the use process after the installation of the machine arm is finished.
The upper plate 1 and the lower plate 2 are provided with mounting holes 15.
The structure is characterized in that the mounting hole 15 is used for mounting and fixing the mounting piece of the horn on the unmanned aerial vehicle.
The mounting hole 15 is arranged at the edge of the wire passing hole 14.
The number of the mounting holes 15 may be set to 4.
The upper arm pipe clamp 11 and the lower arm pipe clamp 12 are provided with arm fixing holes 16.
The horn fixing hole 16 is used for mounting and fixing the horn, and enhances the mounting strength of the horn.
The upper plate 1 and the lower plate 2 are correspondingly arranged.
The upper plate 1 and the lower plate 2 are flat plates.
The unbent portions of the upper plate 1 and the lower plate 2 are still of a flat plate structure.
The angle formed between each part of the flat plate structure is-5 degrees.
The above-mentioned upper plate 1 and 2 unbent part of hypoplastron keep the flat plate structure for the convenience of device installs on unmanned aerial vehicle.
The material selected for the device is aluminum alloy 6061.
The specific embodiments described herein are merely illustrative of the spirit of the invention. Various modifications, additions and substitutions for the specific embodiments described herein may be made by those skilled in the art without departing from the spirit of the invention or exceeding the scope of the invention as defined in the accompanying claims.

Claims (9)

1. The utility model provides a many rotor unmanned aerial vehicle horn installed part, its characterized in that includes upper plate (1) and hypoplastron (2), upper plate (1) side downwarping forms last horn pipe clamp (11) of half tubular structure, hypoplastron (2) side upwarping forms lower horn pipe clamp (12) of half tubular.
2. The multi-rotor unmanned aerial vehicle horn mount of claim 1 wherein the upper and lower horn tube clamps (11, 12) are laterally extended with attachment sockets (13).
3. The multi-rotor drone horn mount of claim 1 wherein the upper (11) and lower (12) horn clamps are mateable to form a tubular mechanical clamp for placement of a robotic arm.
4. the multi-rotor unmanned aerial vehicle horn mounting member as claimed in claim 2, wherein the connecting base (13) is formed with a connecting hole (131).
5. The multi-rotor unmanned aerial vehicle horn mounting member as claimed in claim 1, wherein a wire passing hole (14) is formed in the middle of the upper plate (1) and the lower plate (2).
6. A multi-rotor drone horn mount according to claim 1, characterised in that the upper plate (1) and the lower plate (2) are provided with mounting holes (15).
7. The multi-rotor unmanned aerial vehicle horn mount of claim 1 wherein the upper horn tube clamp (11) and the lower horn tube clamp (12) have horn securing holes (16) formed therein.
8. The multi-rotor drone horn mount of claim 1, wherein the overlap of the vertical projected area of the upper plate (1) and the vertical projected area of the lower plate (2) is 85-100%.
9. A multi-rotor drone horn mount according to claim 1, characterised in that the upper plate (1) and lower plate (2) are flat plates.
CN201920486614.3U 2019-04-11 2019-04-11 Many rotor unmanned aerial vehicle horn installed part Expired - Fee Related CN209739315U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920486614.3U CN209739315U (en) 2019-04-11 2019-04-11 Many rotor unmanned aerial vehicle horn installed part

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920486614.3U CN209739315U (en) 2019-04-11 2019-04-11 Many rotor unmanned aerial vehicle horn installed part

Publications (1)

Publication Number Publication Date
CN209739315U true CN209739315U (en) 2019-12-06

Family

ID=68720522

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920486614.3U Expired - Fee Related CN209739315U (en) 2019-04-11 2019-04-11 Many rotor unmanned aerial vehicle horn installed part

Country Status (1)

Country Link
CN (1) CN209739315U (en)

Similar Documents

Publication Publication Date Title
CN209739315U (en) Many rotor unmanned aerial vehicle horn installed part
CN211579549U (en) Tubular bus connecting fitting for lightning arrester
CN208977181U (en) A kind of assemble mechanism of automatic mounting machine motor-car rearview mirror frame
CN207222652U (en) The adjustable cold bending device of band steel side horizontal
CN208513974U (en) Weld positioning tool in rectangular box side
CN207173207U (en) A kind of bottom arm assembly
CN114670613B (en) Electric automobile battery quick change mechanism and electric automobile
CN213831536U (en) Remote monitoring terminal mounting structure on automobile
CN213896966U (en) Adsorption dust suppression and separation device for mine engineering construction
CN207128799U (en) Wire harness fixing support
CN211173480U (en) Emergency unlocking device of electronic lock
CN207644449U (en) A kind of mounting structure of automobile steering device
CN106759889A (en) Beam column
CN207282568U (en) A kind of power battery box structure
CN206265140U (en) A kind of chassis assembly for electric automobile
CN215921853U (en) Driving motor support of hydrogen energy commercial vehicle
CN115402413B (en) Car body suspension mounting structure and vehicle based on aluminium alloy
CN219668132U (en) Wire harness bracket
CN216429825U (en) Center shaft assembly of tower crane type wind driven generator
CN216462875U (en) Automatic pressing and buckling device
CN214921272U (en) Welding wire adjusting device for pipeline welding
CN214045313U (en) DC tubular motor
CN209366280U (en) A kind of car side wall inner plate welding assembly
CN214064835U (en) High strength stage lamp under casing structure of shaking head
CN210941645U (en) Three-phase line fixing structure and automobile

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20191206

Termination date: 20210411

CF01 Termination of patent right due to non-payment of annual fee