CN214493323U - Many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly - Google Patents

Many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly Download PDF

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Publication number
CN214493323U
CN214493323U CN202120429099.2U CN202120429099U CN214493323U CN 214493323 U CN214493323 U CN 214493323U CN 202120429099 U CN202120429099 U CN 202120429099U CN 214493323 U CN214493323 U CN 214493323U
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CN
China
Prior art keywords
seat
connecting plate
fixedly connected
connecting seat
aerial vehicle
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Expired - Fee Related
Application number
CN202120429099.2U
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Chinese (zh)
Inventor
刘向阳
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Putian Kongtian Network Technology Co ltd
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Putian Kongtian Network Technology Co ltd
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Publication date
Application filed by Putian Kongtian Network Technology Co ltd filed Critical Putian Kongtian Network Technology Co ltd
Priority to CN202120429099.2U priority Critical patent/CN214493323U/en
Application granted granted Critical
Publication of CN214493323U publication Critical patent/CN214493323U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly, including the frame main part, the fixed surface of frame main part is connected with the connecting seat, the inner wall sliding connection of connecting seat has the connecting rod, the bottom fixedly connected with connecting plate of frame main part, the bottom fixedly connected with bracing piece of connecting plate, the top of connecting seat is provided with the bolt, the bottom of connecting seat is provided with the nut. The utility model discloses a cooperation between connecting plate, connecting rod, connecting seat and the fixing base can carry out quick assembly disassembly to each part in the frame effectively to make when maintaining it and changing, it is more light convenient, thereby has guaranteed the normal use of unmanned aerial vehicle, has avoided untimely because of changing, thereby it is troublesome to cause unnecessary, simultaneously, can carry out the dismouting to it, also reduces the parking space when conveniently depositing it.

Description

Many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly
Technical Field
The utility model relates to an unmanned aerial vehicle correlation technique field specifically is a many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly.
Background
An unmanned aircraft, referred to as "drone" for short, is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. From a technical point of view, the definition can be divided into: unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane, etc. The existing multi-rotor unmanned aerial vehicle multi-shaft frame has the following defects: the dismouting of being not convenient for, under the condition that takes place to damage, fail in time to change, maintain to influence whole unmanned aerial vehicle's use, cause unnecessary troublesome.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly to solve the problem that above-mentioned background art provided.
In order to solve the technical problem, the utility model provides a following technical scheme: the utility model provides a many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly, includes the frame main part, the fixed surface of frame main part is connected with the connecting seat, the inner wall sliding connection of connecting seat has the connecting rod, the bottom fixedly connected with connecting plate of frame main part, the bottom fixedly connected with bracing piece of connecting plate, the top of connecting seat is provided with the bolt, the bottom of connecting seat is provided with the nut, bolt through connection seat and connecting rod and nut threaded connection, the bottom of connecting plate is provided with the fixing base, the inner wall sliding connection of fixing base and connecting plate, the bottom and the bracing piece fixed connection of fixing base.
Furthermore, the side of connecting plate is provided with the threaded rod, the both sides of connecting plate are first screw ring of fixedly connected with and second screw ring respectively, the threaded rod and connecting plate and fixing base through connection, threaded rod and first screw ring and second screw ring threaded connection.
Further, the bottom fixedly connected with supporting seat of bracing piece, the side fixedly connected with lead screw of supporting seat, the surperficial threaded connection of lead screw has a screw thread section of thick bamboo.
Furthermore, a gasket is arranged between the screw cap and the connecting seat, and the gasket is sleeved on the surface of the bolt.
Furthermore, the end part of the connecting rod is fixedly connected with a paddle seat, and the bottom of the paddle seat is provided with a motor.
Furthermore, the connecting rod is provided with a plurality of, the bracing piece symmetry sets up.
Compared with the prior art, the utility model discloses the beneficial effect who reaches is:
the utility model discloses a cooperation between connecting plate, connecting rod, connecting seat and the fixing base can carry out quick assembly disassembly to each part in the frame effectively to make when maintaining it and changing, it is more light convenient, thereby has guaranteed the normal use of unmanned aerial vehicle, has avoided untimely because of changing, thereby it is troublesome to cause unnecessary, simultaneously, can carry out the dismouting to it, also reduces the parking space when conveniently depositing it.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
fig. 1 is a schematic structural diagram of the present invention;
FIG. 2 is a schematic view of the connection between the connection plate and the support rod of the present invention;
FIG. 3 is an enlarged schematic view at A in FIG. 1;
fig. 4 is a schematic view of the connection between the support seat and the threaded cylinder of the present invention.
In the figure: 1. a rack main body; 2. a connecting seat; 3. a connecting rod; 4. a connecting plate; 5. a support bar; 6. a bolt; 7. a nut; 8. a fixed seat; 9. a threaded rod; 10. a first threaded ring; 11. a second threaded ring; 12. a supporting seat; 13. a screw rod; 14. a threaded barrel; 15. a gasket; 16. a paddle seat; 17. an electric motor.
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 a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, a multi-rotor unmanned aerial vehicle multi-shaft frame convenient for quick assembly and disassembly comprises a frame main body 1, a connecting seat 2 is fixedly connected to the surface of the frame main body 1, a connecting rod 3 is slidably connected to the inner wall of the connecting seat 2, a connecting plate 4 is fixedly connected to the bottom of the frame main body 1, a supporting rod 5 is fixedly connected to the bottom of the connecting plate 4, a bolt 6 is arranged at the top of the connecting seat 2, a nut 7 is arranged at the bottom of the connecting seat 2, the bolt 6 penetrates through the connecting seat 2 and the connecting rod 3 to be in threaded connection with the nut 7, a fixing seat 8 is arranged at the bottom of the connecting plate 4, the fixing seat 8 is slidably connected to the inner wall of the connecting plate 4, the bottom of the fixing seat 8 is fixedly connected to the supporting rod 5, when in use, the connecting seat 2 and the connecting rod 3 can be conveniently fixed through the bolt 6 and the nut 7, and the connecting seat 2 is arranged to play a connecting role, thereby securing the connection between the housing main body 1 and the connecting rod 3.
In this embodiment, the side of connecting plate 4 is provided with threaded rod 9, the both sides of connecting plate 4 are first screw ring 10 of fixedly connected with and second screw ring 11 respectively, threaded rod 9 and connecting plate 4 and fixing base 8 through connection, threaded rod 9 and first screw ring 10 and the 11 threaded connection of second screw ring, when using, through first screw ring 10 and the second screw ring 11 that set up, make after fixing base 8 inserts in connecting plate 4, thereby make when fixing, it is better to fix the effect, the stability of connection has been guaranteed.
In this embodiment, the bottom fixedly connected with supporting seat 12 of bracing piece 5, the side fixedly connected with lead screw 13 of supporting seat 12, the surperficial threaded connection of lead screw 13 has a screw section of thick bamboo 14, when assembling, plays the effect of support through the supporting seat 12 that sets up, when conveniently supporting it through the lead screw 13 and the screw section of thick bamboo 14 that set up, has improved the supporting effect effectively, when carrying out the dismouting, also can conveniently dismantle simultaneously.
In this embodiment, be provided with gasket 15 between nut 7 and the connecting seat 2, gasket 15 cup joints on the surface of bolt 6, through gasket 15 who sets up for bolt 6 and nut 7 are when fixing, and are inseparable more firm, thereby make the connection of connecting seat 2 and connecting rod 3 more stable.
In this embodiment, the end of the connecting rod 3 is fixedly connected with a paddle base 16, a motor 17 is installed at the bottom of the paddle base 16, the motor 17 is conveniently installed through the arranged paddle base 16, and the propeller is conveniently driven through the arranged motor 17.
In this embodiment, connecting rod 3 is provided with a plurality ofly, and 5 symmetries of bracing piece set up, and 3 quantity through the connecting rod that set up are a plurality ofly to make when using, the flight effect is better, and 5 symmetries of bracing piece through setting up set up, have improved the supporting effect effectively.
The utility model discloses a theory of operation: during unmanned aerial vehicle assembly, fix unmanned aerial vehicle's other subassemblies in the bottom or the top of frame main part 1, thereby conveniently use better, when carrying out the dismouting to whole unmanned aerial vehicle, through rotating bolt 6, thereby make bolt 6 and nut 7 take place to separate, make connecting seat 2 and connecting rod 3 take place to break away from, thereby accomplish the dismouting to connecting rod 3, it is more convenient light, through rotating threaded rod 9, make threaded rod 9 take place to break away from with first screw ring 10 and second screw ring 11 respectively, thereby the dismouting to bracing piece 5 is conveniently, thereby make the dismouting of whole unmanned aerial vehicle get up convenient more light.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (6)

1. The utility model provides a many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly, its characterized in that: including frame main part (1), the fixed surface of frame main part (1) is connected with connecting seat (2), the inner wall sliding connection of connecting seat (2) has connecting rod (3), the bottom fixedly connected with connecting plate (4) of frame main part (1), the bottom fixedly connected with bracing piece (5) of connecting plate (4), the top of connecting seat (2) is provided with bolt (6), the bottom of connecting seat (2) is provided with nut (7), bolt (6) run through connecting seat (2) and connecting rod (3) and nut (7) threaded connection, the bottom of connecting plate (4) is provided with fixing base (8), the inner wall sliding connection of fixing base (8) and connecting plate (4), the bottom and bracing piece (5) fixed connection of fixing base (8).
2. A multi-rotor drone multi-axis airframe according to claim 1 with quick release, characterized in that: the side of connecting plate (4) is provided with threaded rod (9), the both sides of connecting plate (4) are first screw ring (10) of fixedly connected with and second screw ring (11) respectively, threaded rod (9) and connecting plate (4) and fixing base (8) through connection, threaded rod (9) and first screw ring (10) and second screw ring (11) threaded connection.
3. A multi-rotor drone multi-axis airframe according to claim 1 with quick release, characterized in that: the bottom fixedly connected with supporting seat (12) of bracing piece (5), the side fixedly connected with lead screw (13) of supporting seat (12), the surperficial threaded connection of lead screw (13) has a screw section of thick bamboo (14).
4. A multi-rotor drone multi-axis airframe according to claim 1 with quick release, characterized in that: a gasket (15) is arranged between the nut (7) and the connecting seat (2), and the gasket (15) is sleeved on the surface of the bolt (6).
5. A multi-rotor drone multi-axis airframe according to claim 1 with quick release, characterized in that: the end part of the connecting rod (3) is fixedly connected with a paddle seat (16), and the bottom of the paddle seat (16) is provided with a motor (17).
6. A multi-rotor drone multi-axis airframe according to claim 1 with quick release, characterized in that: the connecting rods (3) are arranged in a plurality of numbers, and the supporting rods (5) are symmetrically arranged.
CN202120429099.2U 2021-02-27 2021-02-27 Many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly Expired - Fee Related CN214493323U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202120429099.2U CN214493323U (en) 2021-02-27 2021-02-27 Many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202120429099.2U CN214493323U (en) 2021-02-27 2021-02-27 Many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly

Publications (1)

Publication Number Publication Date
CN214493323U true CN214493323U (en) 2021-10-26

Family

ID=78226525

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202120429099.2U Expired - Fee Related CN214493323U (en) 2021-02-27 2021-02-27 Many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly

Country Status (1)

Country Link
CN (1) CN214493323U (en)

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

Granted publication date: 20211026