CN210455225U

CN210455225U - Unmanned aerial vehicle machine carries pylon

Info

Publication number: CN210455225U
Application number: CN201921491456.7U
Authority: CN
Inventors: 孙哲; 王洪美; 王永革
Original assignee: Shandong Zhonghang Biotechnology Co ltd
Current assignee: Shandong Zhonghang Biotechnology Co ltd
Priority date: 2019-09-09
Filing date: 2019-09-09
Publication date: 2020-05-05
Anticipated expiration: 2029-09-09

Abstract

The utility model belongs to the technical field of the unmanned air vehicle technique and specifically relates to an unmanned aerial vehicle machine carries pylon, including the base plate, outer lane capstan head bearing is installed to the bottom of base plate, install inner circle capstan head bearing on the outer lane capstan head bearing, adjust the pylon is installed to inner circle capstan head bearing's bottom, coupling mechanism is installed on the top of base plate, coupling mechanism is including welding the fixed block on the base plate top, the top integrated into one piece of the horizontal board of fixed block has the fixture block, form first draw-in groove between fixture block and the fixed block, first screw hole has been seted up to the well below symmetry of the vertical board of fixed block, the second screw hole has been seted up to the middle part symmetry of fixture block, first screw hole female connection has the threaded rod, the side welding of the horizontal board of fixed block has first magnet, the opposite side symmetrical welding of first magnet has the. The utility model discloses a coupling mechanism simple structure, simple to operate.

Description

Unmanned aerial vehicle machine carries pylon

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle machine carries pylon.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.

The mechanism that is used for being connected with unmanned aerial vehicle in the current unmanned aerial vehicle machine carries the pylon is too loaded down with trivial details for installation unmanned aerial vehicle's time overlength, thereby waste time has reduced work efficiency.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the problem that the mechanism connected with the unmanned aerial vehicle in the prior art is too loaded down with trivial details shortcoming, and the unmanned aerial vehicle machine carries pylon who proposes.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

an unmanned aerial vehicle airborne tower is designed, and comprises a base plate, wherein an outer ring turret bearing is installed at the bottom end of the base plate, an inner ring turret bearing is installed on the outer ring turret bearing, an adjusting tower is installed at the bottom end of the inner ring turret bearing, a connecting mechanism is installed at the top end of the base plate and comprises fixing blocks welded at four corners of the top end of the base plate, the fixing blocks are of an L-shaped structure, a clamping block is integrally formed at the top end of a transverse plate of each fixing block, a first clamping groove is formed between each clamping block and each fixing block, first threaded holes are symmetrically formed in the middle lower portion of a longitudinal plate of each fixing block, second threaded holes are symmetrically formed in the middle portion of each clamping block, threaded rods are connected in the first threaded holes in an internal threaded mode, first magnets are welded on the side faces of the, the outer surface of dead lever has cup jointed the slide, the second draw-in groove has been seted up to slide and the relative one side top symmetry of fixture block, the welding of slide and the relative one side below of fixture block has second magnet, the other end threaded connection of dead lever has the limiting plate, supplementary fixed establishment is installed to the top of the relative one side of longitudinal plate of fixed block.

Preferably, the threaded rod passes through the second screw hole, extends to the outside of second screw hole to with second draw-in groove cooperation joint, threaded rod and second draw-in groove matched with part do not have the screw thread.

Preferably, the first threaded hole, the second threaded hole, the threaded rod and the second clamping groove are concentric.

Preferably, the first magnet is matched with the second magnet.

Preferably, the auxiliary fixing mechanism comprises a fixing plate symmetrically welded above one side of the longitudinal plate of the fixing block, and the middle of the top end of the fixing plate is welded with the insertion rod.

Preferably, the length of the fixing plate is equal to the length of the first clamping groove.

The utility model provides a pair of unmanned aerial vehicle machine carries pylon, beneficial effect lies in:

1. the cooperation setting between base plate, outer lane capstan head bearing, inner circle capstan head bearing and the regulation pylon can adjust the gesture of rifle to be convenient for aim, coupling mechanism's simple structure, simple to operate, thereby great having saved the installation time between airborne pylon and the unmanned aerial vehicle, thereby can improve the installation effectiveness.

2. Cooperation between first screw hole, second screw hole, threaded rod and the second draw-in groove is connected, can make machine-carried pylon and unmanned aerial vehicle carry out fine being connected, and cooperation between first magnet and the second magnet is connected, can make the connection between machine-carried pylon and the unmanned aerial vehicle more stable.

Drawings

Fig. 1 is a schematic view of a main view structure of an airborne tower of an unmanned aerial vehicle according to the present invention;

fig. 2 is a schematic diagram of a right-view structure of an airborne tower of an unmanned aerial vehicle according to the present invention;

fig. 3 is a schematic front view of a cross-sectional structure of a connecting mechanism of an airborne tower of an unmanned aerial vehicle according to the present invention;

fig. 4 is a schematic top cross-sectional structural view of a connecting mechanism of an airborne tower of an unmanned aerial vehicle according to the present invention;

fig. 5 is the utility model provides a coupling mechanism's of unmanned aerial vehicle machine carries pylon looks sideways at the structure sketch map.

In the figure: the device comprises a base plate 1, an outer ring turret bearing 2, an inner ring turret bearing 3, an adjusting tower 4, a connecting mechanism 5, a fixing block 6, a clamping block 7, a first clamping groove 8, a first threaded hole 9, a second threaded hole 10, a threaded rod 11, a first magnet 12, a fixing rod 13, a sliding plate 14, a second clamping groove 15, a second magnet 16, a limiting plate 17, a fixing plate 18 and an inserting rod 19.

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.

Example 1

Referring to fig. 1-5, an airborne tower of an unmanned aerial vehicle comprises a base plate 1, an outer ring turret bearing 2 is installed at the bottom end of the base plate 1, an inner ring turret bearing 3 is installed on the outer ring turret bearing 2, an adjusting tower 4 is installed at the bottom end of the inner ring turret bearing 3, a connecting mechanism 5 is installed at the top end of the base plate 1, the connecting mechanism 5 comprises fixing blocks 6 welded at four corners of the top end of the base plate 1, each fixing block 6 is of an L-shaped structure, a clamping block 7 is integrally formed at the top end of a transverse plate of each fixing block 6, a first clamping groove 8 is formed between each clamping block 7 and each fixing block 6, first threaded holes 9 are symmetrically formed in the middle lower portion of a longitudinal plate of each fixing block 6, second threaded holes 10 are symmetrically formed in the middle portion of each clamping block 7, threaded rods 11 are connected to the first threaded holes 9 in, can adjust the gesture of rifle to be convenient for aim, coupling mechanism 5's simple structure, simple to operate, thereby great saving the installation time between airborne pylon and the unmanned aerial vehicle, thereby can improve the installation effectiveness.

A first magnet 12 is welded on the side surface of a transverse plate of the fixed block 6, a fixed rod 13 is symmetrically welded on the other side of the first magnet 12, a sliding plate 14 is sleeved on the outer surface of the fixed rod 13, a second clamping groove 15 is symmetrically formed above one side of the sliding plate 14 opposite to the clamping block 7, a second magnet 16 is welded below one side of the sliding plate 14 opposite to the clamping block 7, a limiting plate 17 is connected with the other end of the fixed rod 13 through threads, an auxiliary fixing mechanism is installed above one side of the fixed block 6 opposite to a longitudinal plate, a threaded rod 11 penetrates through a second threaded hole 10, extends to the outer side of the second threaded hole 10 and is matched and clamped with the second clamping groove 15, the part of the threaded rod 11 matched with the second clamping groove 15 does not have threads, the first threaded hole 9, the second threaded hole 10, the threaded rod 11 and the second clamping groove 15 share a central line, the first magnet 12 is matched, except the one side that the cooperation is connected, other sides all bond and have the protection pad, and the cooperation between first screw hole 9, second screw hole 10, threaded rod 11 and the second draw-in groove 15 is connected, can make the machine-carried pylon carry out fine being connected with unmanned aerial vehicle, and the cooperation between first magnet 12 and the second magnet 16 is connected, can make the connection between machine-carried pylon and the unmanned aerial vehicle more stable.

When the on-board pylon is connected with unmanned aerial vehicle, earlier with on the unmanned aerial vehicle with first draw-in groove 8 and fixture block 7 complex part joint, then rotatory threaded rod 11 in the first screw hole 9, make threaded rod 11 run through unmanned aerial vehicle's coupling part, and pass second screw hole 10, extend to the outside of screw hole 10, then remove slide 14, make second draw-in groove 15 on the slide 14 and the tip joint of threaded rod 11, in threaded

rod

11 and 15 joints of second draw-in groove, first magnet 12 and the actuation of second magnet 16.

Example 2

Referring to fig. 3 and 5, as the utility model discloses a further preferred embodiment, the difference with embodiment 1 lies in, supplementary fixed establishment includes the fixed plate 18 of symmetry welding in 6 vertical board one side tops of fixed block, the welding of the top middle part of fixed plate 18 has peg graft pole 19, the length of fixed plate 18 equals with the length of first draw-in groove 8, fixed block 6, cooperation setting between fixed plate 18 and the peg pole 19, can be further strengthened and carry the tower and be connected between unmanned aerial vehicle, when connecting, the 18 joints of fixed plate is on unmanned aerial vehicle in rather than the complex draw-in groove, peg pole 19 pegs graft on unmanned aerial vehicle rather than the matched with spliced eye.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. The airborne tower of the unmanned aerial vehicle comprises a base plate (1) and is characterized in that an outer ring turret bearing (2) is installed at the bottom end of the base plate (1), an inner ring turret bearing (3) is installed on the outer ring turret bearing (2), an adjusting tower (4) is installed at the bottom end of the inner ring turret bearing (3), a connecting mechanism (5) is installed at the top end of the base plate (1), the connecting mechanism (5) comprises fixing blocks (6) welded at four corners of the top end of the base plate (1), the fixing blocks (6) are of an L-shaped structure, a clamping block (7) is integrally formed at the top end of a transverse plate of each fixing block (6), a first clamping groove (8) is formed between each clamping block (7) and each fixing block (6), first threaded holes (9) are symmetrically formed in the middle lower portion of a longitudinal plate of each fixing block (6), second threaded holes (10) are symmetrically formed in the middle portion, first screw hole (9) female connection has threaded rod (11), the side welding of the horizontal board of fixed block (6) has first magnet (12), the opposite side symmetrical welding of first magnet (12) has dead lever (13), slide (14) have been cup jointed to the surface of dead lever (13), second draw-in groove (15) have been seted up to slide (14) and one side top symmetry relative with fixture block (7), slide (14) have second magnet (16) with one side below welding relative with fixture block (7), the other end threaded connection of dead lever (13) has limiting plate (17), supplementary fixed establishment is installed to the top of one side relative to the vertical board of fixed block (6).

2. The airborne tower of the unmanned aerial vehicle of claim 1, wherein the threaded rod (11) passes through the second threaded hole (10), extends to the outer side of the second threaded hole (10), and is in fit clamping connection with the second clamping groove (15), and the part of the threaded rod (11) matched with the second clamping groove (15) is not threaded.

3. An unmanned aerial vehicle airborne tower according to claim 1, wherein the first threaded hole (9), the second threaded hole (10), the threaded rod (11) and the second slot (15) are concentric.

4. The tower of claim 1, wherein the first magnet (12) cooperates with the second magnet (16).

5. The airborne tower of an unmanned aerial vehicle according to claim 1, wherein the auxiliary fixing mechanism comprises a fixing plate (18) symmetrically welded above one side of a longitudinal plate of the fixing block (6), and a plug rod (19) is welded in the middle of the top end of the fixing plate (18).

6. An airborne tower of unmanned aerial vehicle according to claim 5, wherein the length of the fixing plate (18) is equal to the length of the first card slot (8).