CN212776560U

CN212776560U - Multifunctional easy-to-dismount damping cradle head of CHs unmanned aerial vehicle

Info

Publication number: CN212776560U
Application number: CN202021709627.1U
Authority: CN
Inventors: 韩建平; 阚博才
Original assignee: Beijing Zhongke Tianhua Remote Sensing Technology Co ltd
Current assignee: Qingdao National Laboratory for Marine Science and Technology Development Center
Priority date: 2020-08-17
Filing date: 2020-08-17
Publication date: 2021-03-23
Anticipated expiration: 2030-08-17

Abstract

The utility model discloses a multi-functional just, tearing open shock attenuation cloud platform of CHs unmanned aerial vehicle, including the bottom extension board, the equal cartridge in four corners of bottom extension board has linear bearing, linear bearing's the equal vertical cartridge in inside has the guiding axle, guiding axle support is installed to the upper end of guiding axle outer axostylus axostyle, carry type elevating gear in installing in the upper end of bottom extension board, the utility model provides a multi-functional just, tearing open shock attenuation cloud platform of CHs unmanned aerial vehicle can be convenient dismantle the unmanned aerial vehicle cassette through dismantling X axle baffle and Y axle baffle, and the unmanned aerial vehicle cassette on the installation simultaneously can adjust its height at will according to the environmental requirement, can suitably adjust its horizontal ascending position, can be through screwing first hexagonal knob and second hexagonal knob and come locking device after the adjustment, carries out the shock attenuation to equipment through the shock insulation support, simple structure, convenient adjustment and.

Description

Multifunctional easy-to-dismount damping cradle head of CHs unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned aerial vehicle accessory technical field, specific field is the multi-functional shock attenuation cloud platform of just tearing open of CHs unmanned aerial vehicle.

Background

With the rapid development of scientific technology, unmanned planes (called unmanned planes for short) are more and more widely applied to the fields of military, scientific research, civil use and the like due to the advantages of flexibility, quick response, unmanned flight, low operation requirement and the like. In order to enable the unmanned aerial vehicle to be widely applied, especially in the fields of electric power, communication, meteorology, agriculture, oceans, exploration, photography, disaster prevention and reduction, crop estimation, drug and personal enforcement, border patrol, public security and counter terrorism and the like, a camera or other rescue equipment is often required to be carried on the body of the unmanned aerial vehicle, and a part for carrying the camera or the rescue equipment on the unmanned aerial vehicle is a cradle head. Traditional cloud platform adopts non-detachable connection structure with the organism, and the dismouting is inconvenient, the range of application is narrower. At present, there are a lot of cloud platforms and unmanned aerial vehicle's connection to adopt a large amount of screw connections on the market, though can dismantle, nevertheless need the instrument during dismouting, the dismouting process will consume a large amount of time, does not have the cushioning effect moreover.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a CHs unmanned aerial vehicle is multi-functional just, tears shock attenuation cloud platform open to traditional cloud platform that proposes in solving above-mentioned background adopts undetachable connection structure with the organism, and the dismouting is inconvenient, the range of application is narrower. At present, there are a lot of cloud platforms and unmanned aerial vehicle's connection to adopt a large amount of screw connections on the market, though can dismantle, need instrument during the dismouting, the problem that the dismouting process will consume a large amount of time.

In order to achieve the above object, the utility model provides a following technical scheme: the multifunctional easy-to-dismount shock-absorbing cradle head of the CHs unmanned aerial vehicle comprises a bottom support plate, linear bearings are inserted into four corners of the bottom support plate, guide shafts are longitudinally inserted into the linear bearings, guide shaft supports are installed at the upper ends of outer shaft rods of the guide shafts, a middle-load type lifting device is installed at the upper ends of the bottom support plate, limiting columns are connected between adjacent end surfaces of connecting rods on the front side and the rear side of the middle-load type lifting device in a pin joint mode, the number of the limiting columns is two, the limiting columns are connected to the left side and the right side of a connecting rod in the middle of the middle-load type lifting device in a pin joint mode, the middle of the limiting columns on the left side and the right side transversely penetrates through a guide rod, a radial type hand wheel is installed at the left end of the guide rod, a lifting plate is installed at the upper end of the middle-load type lifting device, the front side and the rear side of the upper end face of the lifting plate are respectively provided with a first linear guide rail, the upper end of the first linear guide rail is provided with a first linear sliding block, the upper end of the first linear sliding block is provided with an X-axis sliding plate, the left end of the X-axis sliding plate is provided with a second knob top plate, the left side and the right side of the upper end face of the X-axis sliding plate are respectively provided with a second linear guide rail, the upper end of the second linear guide rail is provided with a second linear sliding block, the upper end of the second linear sliding block is provided with a Y-axis sliding plate, the upper end of the Y-axis sliding plate is provided with an unmanned aerial vehicle holder, the left side and the right side of the upper surface of the unmanned aerial vehicle holder are respectively provided with a semicircular groove, the semicircular grooves are internally and slidably provided with a limiting handle, the middle part of the front end face of the X-axis sliding plate is provided with a, the middle part of the left end face of the Y-axis sliding plate is provided with a second knob seat, the middle part of the second knob seat is provided with a second hexagonal knob in a threaded manner, and the right end of the second hexagonal knob is fixed on the left end face of the second knob top plate.

Preferably, full-thread bolts are installed on the front side and the rear side of the upper end face of the bottom support plate in a longitudinal threaded mode.

Preferably, an X-axis baffle is longitudinally installed on the left end face of the lifting plate, the midpoint of the X-axis baffle and the midpoint of the first linear guide rail on the rear side are both on the same transverse straight line, and the width of the X-axis baffle is greater than that of the first linear guide rail.

Preferably, a Y-axis baffle is longitudinally installed on the front end face of the X-axis sliding plate, the midpoint of the Y-axis baffle and the midpoint of the second linear guide rail on the right side are both on the same longitudinal straight line, and the width of the Y-axis baffle is greater than that of the second linear guide rail.

Preferably, rectangular through holes are formed in the middle of the lifting plate, the middle of the X-axis baffle and the middle of the Y-axis baffle.

Preferably, the middle part of the upper end surface of the unmanned aerial vehicle holder is provided with an unmanned aerial vehicle clamping seat.

Preferably, the lower end of the guide shaft is in threaded connection with a vibration isolating support.

Compared with the prior art, the beneficial effects of the utility model are that: the utility model provides a CHs unmanned aerial vehicle multi-functional just, tear shock attenuation cloud platform open can be convenient dismantles the unmanned aerial vehicle cassette through dismantling X axle baffle and Y axle baffle, and the unmanned aerial vehicle cassette on the installation can adjust its height at will according to the environmental requirement simultaneously, can suitably adjust its horizontal ascending position, can come locking device through screwing first hexagonal knob and second hexagonal knob after the adjustment, carry out the shock attenuation to equipment through the shock insulation support, simple structure, convenient adjustment and dismouting.

Drawings

Fig. 1 is a schematic view of the structure of the present invention;

FIG. 2 is a schematic side view of the present invention;

fig. 3 is a schematic top view of the present invention.

In the figure: 1-bottom support plate, 2-linear bearing, 3-guide shaft, 4-guide shaft support, 5-middle load type lifting device, 6-limit column, 7-guide rod, 8-spoke type hand wheel, 9-lifting plate, 10-first knob top plate, 11-first linear guide rail, 12-first linear sliding block, 13-X shaft sliding plate, 14-second knob top plate, 15-second linear guide rail, 16-second linear sliding block, 17-Y shaft sliding plate, 18-unmanned aerial vehicle tripod head, 19-semicircular groove, 20-limit handle, 21-first knob seat, 22-first hexagonal knob, 23-second knob seat, 24-second hexagonal knob, 25-X shaft baffle, 26-Y shaft baffle, 27-unmanned aerial vehicle clamping seat, 28-seismic isolation support.

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. 1-3, the present invention provides a technical solution: a multifunctional conveniently-disassembled damping cradle head of a CHs unmanned aerial vehicle comprises a bottom support plate 1, linear bearings 2 are inserted into four corners of the bottom support plate 1, guide shafts 3 are longitudinally inserted into the linear bearings 2, the guide shafts 3 can slide and lift in the linear bearings 2, guide shaft supports 4 are mounted at the upper ends of outer shaft rods of the guide shafts 3, the guide shaft supports 4 are fixed at the upper ends of the outer shaft rods of the guide shafts 3, a middle-loading type lifting device 5 is mounted at the upper end of the bottom support plate 1, the middle-loading type lifting device 5 is a lifting system consisting of a plurality of connecting rods stacked in a bidirectional direction and can search and purchase existing technical products at each large network station, limiting columns 6 are connected between adjacent end surfaces of the connecting rods at the front side and the rear side of the middle-loading type lifting device 5 in a pin mode, the number of the limiting columns 6 is two and is connected to the left side and the right side of the connecting rods at the middle of, the middle parts of the left and right side limiting columns 6 transversely penetrate through the guide rod 7, the left end of the guide rod 7 is provided with a radial hand wheel 8, the relative distance between the front and rear limiting columns 6 can be changed by rotating the radial hand wheel 8, so that the height of the middle-load type lifting device 5 is changed, the upper end of the middle-load type lifting device 5 is provided with a lifting plate 9, the lifting action of the middle-load type lifting device 5 can directly drive the lifting plate 9 to lift, the corner of the lower end surface of the lifting plate 9 is fixed on the upper end surface of the guide shaft support 4, the front end of the lifting plate 9 is provided with a first knob top plate 10, the front and rear sides of the upper end surface of the lifting plate 9 are provided with first linear guide rails 11, the upper end of the first linear guide rails 11 is provided with first linear slide blocks 12, the upper end of the first linear slide blocks 12 is provided with X-axis slide plates 13, the left end of the X-axis slide plates 13 is provided with second knob top plates, a second linear slide block 16 is arranged at the upper end of the second linear guide rail 15, a Y-axis slide plate 17 is arranged at the upper end of the second linear slide block 16, an unmanned aerial vehicle pan-tilt 18 is arranged at the upper end of the Y-axis slide plate 17, can change the relative position of unmanned aerial vehicle cloud platform 18 on the device through slip X axle slide 13 and Y axle slide 17, the left and right sides of unmanned aerial vehicle cloud platform 18 upper surface all is provided with semicircular groove 19, slidable mounting has spacing handle 20 in the semicircular groove 19, the mid-mounting of terminal surface has first knob seat 21 before the X axle slide 13, first hexagonal knob 22 is installed to the middle part screw thread of first knob seat 21, the rear end face of first hexagonal knob 22 is fixed in the preceding terminal surface of first knob roof 10, the mid-mounting of Y axle slide 17 left end face has second knob seat 23, second hexagonal knob 24 is installed to the middle part screw thread of second knob seat 23, the right-hand member of second hexagonal knob 24 is fixed in the left end face of second knob roof 14.

Specifically, full-thread bolts are longitudinally threaded on the front side and the rear side of the upper end surface of the bottom support plate 1.

Specifically, an X-axis baffle 25 is longitudinally mounted on the left end surface of the lifting plate 9, the midpoint of the X-axis baffle 25 and the midpoint of the rear first linear guide 11 are both on the same transverse straight line, and the width of the X-axis baffle 25 is greater than that of the first linear guide 11.

Specifically, a Y-axis baffle 26 is longitudinally mounted on the front end surface of the X-axis sliding plate 13, the middle point of the Y-axis baffle 26 and the middle point of the right second linear guide 15 are both on the same longitudinal straight line, and the width of the Y-axis baffle 26 is greater than that of the second linear guide 15.

Specifically, rectangular through holes are formed in the middle portions of the lifting plate 9, the X-axis baffle plate 25 and the Y-axis baffle plate 26.

Particularly, the middle part of the upper end surface of the unmanned aerial vehicle holder 18 is provided with an unmanned aerial vehicle clamping seat 27.

Particularly, the lower extreme threaded connection of guiding axle 3 has isolation bearing 28, and isolation bearing 28 can separate the vibration that unmanned aerial vehicle produced at the lift in-process.

The working principle is as follows: the utility model discloses when using, can change the relative distance of the spacing post 6 of both sides around through rotatory spoke formula hand wheel 8, and then carry type elevating gear 5's height in the change, indirect adjustment unmanned aerial vehicle cloud platform 18's height, when needing to dismantle unmanned aerial vehicle cloud platform 18, pull down X axle baffle 25 and Y axle baffle 26 and just can take off unmanned aerial vehicle cloud platform 18, the first hexagonal knob 22 of unscrewing and second hexagonal knob 24, can change the relative position of unmanned aerial vehicle cloud platform 18 on the device through slip X axle slide 13 and Y axle slide 17, make it can adapt to multiple environment.

In the description of the present invention, unless expressly stated or limited otherwise, the terms "mounted," "connected," and "fixed" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral part; 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 in specific cases to those skilled in the art.

The utility model discloses the standard part that uses all can purchase from the market, and dysmorphism piece all can be customized according to the description with the record of drawing of description, and the concrete connection mode of each part all adopts conventional means such as ripe bolt, rivet, welding among the prior art, and machinery, part and equipment all adopt prior art, and conventional model, including circuit connection adopts conventional connection mode among the prior art, does not detailed here again.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

The multifunctional easy-to-dismount damping cradle head of the CHs unmanned aerial vehicle comprises a bottom support plate (1) and is characterized in that: the four corners of the bottom support plate (1) are all inserted with linear bearings (2), the interior of each linear bearing (2) is longitudinally inserted with a guide shaft (3), the upper end of an outer shaft rod of each guide shaft (3) is provided with a guide shaft support (4), the upper end of the bottom support plate (1) is provided with a middle-load type lifting device (5), limit posts (6) are connected between the adjacent end surfaces of connecting rods on the front side and the rear side of the middle-load type lifting device (5) in a pin joint mode, the number of the limit posts (6) is two and connected to the left side and the right side of a connecting rod in the middle of the middle-load type lifting device (5) in a pin joint mode, the middle of the limit posts (6) on the left side and the right side transversely penetrates through the guide rods (7), the left end of each guide rod (7) is provided with a radial hand wheel (8), the upper end of the middle-load type lifting device (5) is provided with a lifting plate (9), and corners, a first knob top plate (10) is installed at the front end of the lifting plate (9), first linear guide rails (11) are installed on the front side and the rear side of the upper end face of the lifting plate (9), first linear sliding blocks (12) are installed on the upper ends of the first linear guide rails (11), an X-axis sliding plate (13) is installed on the upper ends of the first linear sliding blocks (12), a second knob top plate (14) is installed on the left end of the X-axis sliding plate (13), second linear guide rails (15) are installed on the left side and the right side of the upper end face of the X-axis sliding plate (13), second linear sliding blocks (16) are installed on the upper ends of the second linear sliding blocks (15), a Y-axis sliding plate (17) is installed on the upper end of the Y-axis sliding plate (17), an unmanned aerial vehicle cloud platform (18) is installed on the upper end of the Y-axis sliding plate (17), and semicircular grooves (19), there is spacing handle (20) in semicircular groove (19), the mid-mounting of terminal surface has first knob seat (21) before X axle slide (13), first hexagonal knob (22) are installed to the middle part screw thread of first knob seat (21), the rear end face of first hexagonal knob (22) is fixed in the preceding terminal surface of first knob roof (10), the mid-mounting of Y axle slide (17) left end face has second knob seat (23), second hexagonal knob (24) are installed to the middle part screw thread of second knob seat (23), the right-hand member of second hexagonal knob (24) is fixed in the left end face of second knob roof (14).
2. The multifunctional easy-to-disassemble shock-absorbing cradle head of the CHs unmanned aerial vehicle as claimed in claim 1, wherein: and full-thread bolts are arranged on the front side and the rear side of the upper end surface of the bottom support plate (1) in a longitudinal threaded manner.
3. The multifunctional easy-to-disassemble shock-absorbing cradle head of the CHs unmanned aerial vehicle as claimed in claim 1, wherein: x-axis baffle (25) are longitudinally installed on the left end face of the lifting plate (9), the middle point of the X-axis baffle (25) and the rear side of the middle point of the first linear guide rail (11) are on the same transverse straight line, and the width of the X-axis baffle (25) is larger than that of the first linear guide rail (11).
4. The multifunctional easy-to-disassemble shock-absorbing cradle head of the CHs unmanned aerial vehicle as claimed in claim 3, wherein: the X-axis sliding plate is characterized in that a Y-axis baffle (26) is longitudinally arranged on the front end face of the X-axis sliding plate (13), the middle point of the Y-axis baffle (26) and the middle point of the second linear guide rail (15) on the right side are on the same longitudinal straight line, and the width of the Y-axis baffle (26) is greater than that of the second linear guide rail (15).
5. The multifunctional easy-to-disassemble shock-absorbing cradle head of the CHs unmanned aerial vehicle as claimed in claim 4, wherein: the middle parts of the lifting plate (9), the X-axis baffle (25) and the Y-axis baffle (26) are provided with rectangular through holes.
6. The multifunctional easy-to-disassemble shock-absorbing cradle head of the CHs unmanned aerial vehicle as claimed in claim 1, wherein: the middle part of the upper end surface of the unmanned aerial vehicle holder (18) is provided with an unmanned aerial vehicle clamping seat (27).
7. The multifunctional easy-to-disassemble shock-absorbing cradle head of the CHs unmanned aerial vehicle as claimed in claim 1, wherein: the lower end of the guide shaft (3) is in threaded connection with a shock insulation support (28).