CN217198691U - Unmanned aerial vehicle platform - Google Patents

Unmanned aerial vehicle platform Download PDF

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Publication number
CN217198691U
CN217198691U CN202220418826.XU CN202220418826U CN217198691U CN 217198691 U CN217198691 U CN 217198691U CN 202220418826 U CN202220418826 U CN 202220418826U CN 217198691 U CN217198691 U CN 217198691U
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CN
China
Prior art keywords
rod
platform
unmanned aerial
threaded
aerial vehicle
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CN202220418826.XU
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Chinese (zh)
Inventor
肖莉
刘中海
马自强
张国玉
王陈强
柴娟
杨传甲
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Xinjiang Guannong Co ltd
Xinjiang Guannong Testing Technology Co ltd
Original Assignee
Xinjiang Guannong Testing Technology Co ltd
Xinjiang Guannong Fruit Antler Co ltd
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Priority to CN202220418826.XU priority Critical patent/CN217198691U/en
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    • 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
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10Technologies relating to charging of electric vehicles
    • Y02T90/14Plug-in electric vehicles

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle platform, which comprises a shutdown platform panel, wherein a horizontal cavity is arranged in the shutdown platform panel, and two horizontal chutes are symmetrically arranged on the bottom wall of the horizontal cavity in the left-right direction; the platform bracket is hinged at four corners at the bottom end of the shutdown platform panel and is respectively hinged with the shutdown platform panel through a folding mechanism; the folding mechanism comprises a bidirectional threaded rod, a threaded slider and a hinge rod; the bidirectional threaded rod is rotatably connected in the horizontal cavity; the two threaded sliding blocks are respectively in threaded connection with different thread turning positions of the bidirectional threaded rod, and the bottom of each threaded sliding block extends out of the horizontal sliding groove; one end of the hinged rod is pivotally connected with the threaded sliding block, and the other end of the hinged rod is pivotally connected with the platform bracket. The utility model discloses the current unmanned aerial vehicle platform of mainly having solved carries inconvenient problem. The utility model discloses mainly used unmanned aerial vehicle's lift.

Description

Unmanned aerial vehicle platform
Technical Field
The utility model relates to an unmanned air vehicle technique field, more specifically say, relate to an unmanned aerial vehicle platform.
Background
The unmanned aerial vehicle platform is the carrier that supplies unmanned aerial vehicle to go up and down, and unmanned aerial vehicle is the most dangerous stage when starting with descending. At present most people go up and down to unmanned aerial vehicle on naked subaerial, because naked ground debris are more to it is flat inadequately, unmanned aerial vehicle receives the damage easily when going up and down. Therefore, the unmanned aerial vehicle platform can greatly reduce the damage probability of the unmanned aerial vehicle, and the unmanned aerial vehicle is protected. And current unmanned aerial vehicle platform simple structure, the function is single, can not go up and down, fold, makes the platform carry inconveniently like this. In addition, the platform does not possess the shock-absorbing function, can not make unmanned aerial vehicle obtain sufficient protection when descending.
SUMMERY OF THE UTILITY MODEL
To the problem that exists among the current stage technique, the utility model provides a folding, liftable, use, convenient to carry's unmanned aerial vehicle platform.
In order to achieve the above purpose, the utility model provides a technical scheme does:
an unmanned aerial vehicle platform, comprising:
the shutdown platform panel is internally provided with a horizontal cavity, and the bottom wall of the horizontal cavity is bilaterally and symmetrically provided with two horizontal sliding chutes;
the platform bracket is hinged at four corners at the bottom end of the shutdown platform panel and is respectively hinged with the shutdown platform panel through a folding mechanism;
the folding mechanism comprises a bidirectional threaded rod, a threaded sliding block and a hinged rod; the bidirectional threaded rod is rotatably connected in the horizontal cavity; the two threaded sliding blocks are respectively in threaded connection with different thread turning positions of the bidirectional threaded rod, and the bottom of each threaded sliding block extends out of the horizontal sliding groove; one end of the hinged rod is pivotally connected with the threaded sliding block, and the other end of the hinged rod is pivotally connected with the platform bracket.
Furthermore, the number of the horizontal cavities is two, and the two horizontal cavities are symmetrically arranged in the front and back of the panel of the shutdown platform.
Furthermore, a first motor is further arranged and fixedly installed on one side wall of the horizontal cavity, and an output shaft of the first motor is connected with the end portion of the bidirectional threaded rod.
Further, the top of the threaded sliding block is in sliding connection with the top wall of the horizontal cavity, and the bottom of the threaded sliding block is in sliding connection with the horizontal sliding groove.
Furthermore, a vertical cavity is formed in the bottom end of the platform support, and vertical sliding grooves are formed in two sides of the vertical cavity;
the inside of vertical cavity is equipped with elevating system, and elevating system's bottom is equipped with supporting mechanism.
Furthermore, the lifting mechanism comprises a sliding rod, a one-way threaded rod and a lifting plate, the one-way threaded rod is rotatably connected with the vertical cavity, and the one-way threaded rod is rotatably connected with the sliding rod; the sliding rod extends to the outside of the vertical sliding groove and is in sliding connection with the vertical sliding groove, lifting plates are fixedly arranged at two extending end portions of the sliding rod, and a supporting mechanism is arranged below the lifting plates.
Furthermore, a second motor is further arranged, the second motor is fixedly installed in the vertical cavity, and an output shaft of the second motor is connected with the end portion of the one-way threaded rod.
Furthermore, a thread block is further arranged and embedded in the middle of the sliding rod and in threaded connection with the sliding rod.
Still further, the support mechanisms are provided in four.
Further, the supporting mechanism includes bracing piece, overhead gage, spring, shock attenuation pole, lower baffle and stock, bracing piece fixed mounting be in the bottom of slide bar, overhead gage fixed mounting be in the bottom of bracing piece, shock attenuation pole sliding connection be in the bottom of bracing piece, baffle fixed mounting is in down on the shock attenuation pole, stock fixed mounting be in the bottom of shock attenuation pole, the spring housing is established on the shock attenuation pole and is located the overhead gage and between the baffle down.
Compared with the prior art, the beneficial effects of the utility model reside in that:
1. the utility model discloses be equipped with folding mechanism between shutdown platform panel and platform support, this folding mechanism can contract folding to the platform support, has improved the convenient to use nature of this device greatly to make this device carry better.
2. The utility model discloses be equipped with supporting mechanism in platform support's bottom, supporting mechanism's bottom is equipped with the stock, can make this device support more stable, has avoided the problem that unmanned aerial vehicle's unstability when taking off or descending leads to the platform slope. Simultaneously supporting mechanism plays absorbing effect under the effect of spring for unmanned aerial vehicle is more steady when descending.
Drawings
Fig. 1 is a cross-sectional view of the present invention;
FIG. 2 is a sectional view taken along line A-A of FIG. 1;
fig. 3 is an enlarged view of fig. 1 at B.
In the figure: 101. a first motor; 102. a bidirectional threaded rod; 103. a threaded slider; 104. a hinged lever; 201. a second motor; 202. a thread block; 203. a slide bar; 204. a one-way threaded rod; 205. a lifting plate; 301. a support bar; 302. an upper baffle plate; 303. a spring; 304. a shock-absorbing lever; 305. a lower baffle plate; 306. an anchor rod; 4. stopping the platform panel; 5. a horizontal cavity; 6. a horizontal chute; 7. a platform support; 8. a vertical cavity; 9. a vertical chute.
Detailed Description
The following detailed description of the embodiments of the present invention is provided with reference to the accompanying drawings and examples. The following examples are intended to illustrate the invention, but are not intended to limit the scope of the invention.
In the description of the present application, it is to be understood that the terms "center", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience in describing the present application and simplifying the description, but do not indicate or imply that the referred device or element must have a particular orientation, be constructed in a particular orientation, and be operated, and thus should not be construed as limiting the present application.
The terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present application, "a plurality" means two or more unless otherwise specified.
In the description of the present application, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present application can be understood in a specific case by those of ordinary skill in the art.
As shown in 1-3, the utility model discloses an unmanned aerial vehicle platform of preferred embodiment, include: the shutdown platform comprises a shutdown platform panel 4, a horizontal cavity 5 is arranged in the shutdown platform panel, and two horizontal sliding chutes 6 are symmetrically arranged on the bottom wall of the horizontal cavity 5 in the left-right direction; the platform supports 7 are hinged at four corners of the bottom end of the shutdown platform panel 4 and are respectively hinged with the shutdown platform panel 4 through a folding mechanism; the folding mechanism comprises a bidirectional threaded rod 102, a threaded slider 103 and a hinge rod 104; the bidirectional threaded rod 102 is rotatably connected in the horizontal cavity 5; the number of the threaded sliding blocks 103 is two, the two threaded sliding blocks 103 are respectively in threaded connection with different thread turning positions of the bidirectional threaded rod 102, and the bottom of each threaded sliding block 103 extends out of the horizontal sliding groove 6; the hinge rod 104 is pivotally connected at one end to the threaded slider 103 and at the other end to the platform support 7.
It can be understood that four platform supports 7 are arranged and respectively connected to four corners at the bottom end of the shutdown platform panel 4; correspondingly, four folding mechanisms are provided.
The rotation of the bidirectional threaded rod 102 drives the two threaded sliders 103 to move toward or away from each other, so as to drive the hinge rod 104 to rotate, and the hinge rod 104 adjusts the angle between the platform support 7 and the stop platform panel 4. When it is desired to stow the platform support 7, the two threaded blocks 103 are brought closer together, pulling the platform support 7 through the hinge rod 104, thereby stowing the platform support 7.
In some embodiments of the present application, the two horizontal cavities 5 are provided, and the two horizontal cavities 5 are symmetrically arranged in front and back inside the shutdown platform panel 4. The bidirectional threaded rod type motor is characterized by further comprising a first motor 101, wherein the first motor 101 is fixedly installed on one side wall of the horizontal cavity 5, and an output shaft of the first motor 101 is connected with the end portion of the bidirectional threaded rod 102. The top of the threaded sliding block 103 is in sliding connection with the top wall of the horizontal cavity, and the bottom of the threaded sliding block is in sliding connection with the horizontal sliding groove 6.
It can be understood that the first motor 101 is a dc brushless speed reducing motor, which has a large torque, a long life and is easy to control.
In some embodiments of the present application, a vertical cavity 8 is formed inside the bottom end of the platform support 7, and vertical sliding grooves 9 are formed on two sides of the vertical cavity 8; the inside of vertical cavity 8 is equipped with elevating system, and elevating system's bottom is equipped with supporting mechanism.
In some embodiments of the present application, the lifting mechanism comprises a sliding rod 203, a one-way threaded rod 204 and a lifting plate 205, the one-way threaded rod 204 is rotatably connected with the vertical cavity 8, and the one-way threaded rod 204 is rotatably connected with the sliding rod 203; the sliding rod 203 extends to the outside of the vertical sliding chute 9 and is connected with the vertical sliding chute 9 in a sliding manner, the two extending ends of the sliding rod 203 are fixedly provided with lifting plates 205, and a supporting mechanism is arranged below the lifting plates 205. A second motor 201 is further arranged, the second motor 201 is fixedly installed in the vertical cavity 8, and an output shaft of the second motor 201 is connected with the end portion of the one-way threaded rod 204. A thread block 202 is further arranged, and the thread block 202 is embedded in the middle of the sliding rod 203 and is in threaded connection with the sliding rod 203.
The second motor 201 drives the one-way threaded rod 204 to rotate so as to drive the threaded block 202 to lift, thereby driving the sliding rod 203 to lift, and further realizing the lifting of the control supporting mechanism and the lifting of the shutdown platform panel 4.
It can be understood that the second motor 201 is a dc brushless speed reducing motor, which has a large torque, a long life and is easy to control.
On the basis of the embodiment, the folding switch, the lifting switch and the controller are also arranged; the two first motors 101 are respectively and electrically connected with the controller, and the controller receives an instruction of the folding switch, drives the two first motors 101 to synchronously operate, and performs folding and unfolding actions on the platform support 7; the four second motors 201 are respectively electrically connected with the controller, and the controller receives an instruction of the lifting switch to drive the four second motors 201 to synchronously operate so as to lift the supporting mechanism. Wherein folding switch, lifting switch and controller's instruction, controller are not to motor synchronous operation's control method the utility model discloses the protection within range that requires.
In some embodiments of the present application, the support mechanisms are provided in four. The supporting mechanism includes bracing piece 301, overhead gage 302, spring 303, shock attenuation pole 304, baffle 305 and stock 306 down, bracing piece 301 fixed mounting be in the bottom of slide bar 203, overhead gage 302 fixed mounting be in the bottom of bracing piece 301, shock attenuation pole 304 sliding connection be in the bottom of bracing piece 301, baffle 305 fixed mounting is in down on the shock attenuation pole 304, stock 306 fixed mounting be in the bottom of shock attenuation pole 304, spring 303 cover is established on shock attenuation pole 304 and is located between overhead gage 302 and the lower baffle 305.
The inside cavity that is equipped with in bottom of bracing piece 301, overhead gage 302 and cavity sliding connection are passed on the top of shock attenuation pole 304, when needs fix the device, during stock 306 can enter into soil for this device is more stable, and spring 303 can play absorbing effect to this device simultaneously.
The utility model discloses a working process does:
when using this device, at first start first motor 101, first motor 101 drives two-way threaded rod 102 and rotates, because the roof and the horizontal spout 6 sliding connection of screw slider 103 and horizontal cavity 5 to with two-way threaded rod 102 threaded connection, consequently two-way threaded rod 102 rotates and can drive two screw slider 103 and do the motion of keeping away from each other, thereby drive hinge bar 104 and rotate, thereby hinge bar 104 adjusts the angle between platform support 7 and the platform panel 4 that stops. Thereby prop up platform support 7, lead to the supporting mechanism who establishes the bottom at platform support 7 to support this device, when needs adjust the height of this device, start second motor 201, second motor 201 drives one-way threaded rod 204 and rotates and then drive the screw thread piece 202 and go up and down to drive slide bar 203 and go up and down, thereby realize the lift of control supporting mechanism, thereby realize the lift to shutting down platform panel 4.
When it is desired to stow the platform support 7, the two threaded sliders 103 are brought closer together, pulling the platform support 7 through the hinge rod 104, thereby stowing the platform support 7.
The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of modifications and replacements can be made without departing from the technical principle of the present invention, and these modifications and replacements should also be regarded as the protection scope of the present invention.

Claims (10)

1. An unmanned aerial vehicle platform, comprising:
the shutdown platform panel is internally provided with a horizontal cavity, and the bottom wall of the horizontal cavity is bilaterally and symmetrically provided with two horizontal sliding chutes;
the platform bracket is hinged at four corners at the bottom end of the shutdown platform panel and is respectively hinged with the shutdown platform panel through a folding mechanism;
the folding mechanism comprises a bidirectional threaded rod, a threaded slider and a hinge rod; the bidirectional threaded rod is rotatably connected in the horizontal cavity; the two threaded sliding blocks are respectively in threaded connection with different thread turning positions of the bidirectional threaded rod, and the bottom of each threaded sliding block extends out of the horizontal sliding groove; one end of the hinged rod is pivotally connected with the threaded sliding block, and the other end of the hinged rod is pivotally connected with the platform bracket.
2. The unmanned aerial vehicle platform of claim 1, wherein the number of the horizontal cavities is two, and the two horizontal cavities are symmetrically arranged in front and back of the inside of the shutdown platform panel.
3. The unmanned aerial vehicle platform of claim 1, further comprising a first motor, wherein the first motor is fixedly mounted on a side wall of the horizontal cavity, and an output shaft of the first motor is connected with an end of the bidirectional threaded rod.
4. The drone platform of claim 1, wherein the top of the threaded slider is slidably connected to the top wall of the horizontal cavity and the bottom is slidably connected to the horizontal chute.
5. The unmanned aerial vehicle platform of claim 1, wherein a vertical cavity is formed in the bottom end of the platform support, and vertical sliding grooves are formed in two sides of the vertical cavity;
the inside of vertical cavity is equipped with elevating system, and elevating system's bottom is equipped with supporting mechanism.
6. The unmanned aerial vehicle platform of claim 5, wherein the lifting mechanism comprises a slide bar, a one-way threaded rod and a lifting plate, the one-way threaded rod is rotatably connected with the vertical cavity, and the one-way threaded rod is rotatably connected with the slide bar; the sliding rod extends to the outside of the vertical sliding groove and is in sliding connection with the vertical sliding groove, lifting plates are fixedly arranged at two extending end portions of the sliding rod, and a supporting mechanism is arranged below the lifting plates.
7. The unmanned aerial vehicle platform of claim 6, further comprising a second motor fixedly mounted within the vertical cavity, an output shaft of the second motor being connected to an end of the one-way threaded rod.
8. The unmanned aerial vehicle platform of claim 6, further comprising a threaded block embedded in the middle of the sliding rod and in threaded connection with the sliding rod.
9. An unmanned aerial vehicle platform according to claim 6, wherein the support means are provided in the form of four.
10. The unmanned aerial vehicle platform of claim 9, wherein the support mechanism comprises a support rod, an upper baffle, a spring, a shock-absorbing rod, a lower baffle and an anchor rod, the support rod is fixedly mounted at the bottom end of the slide rod, the upper baffle is fixedly mounted at the bottom end of the support rod, the shock-absorbing rod is slidably connected at the bottom end of the support rod, the lower baffle is fixedly mounted on the shock-absorbing rod, the anchor rod is fixedly mounted at the bottom end of the shock-absorbing rod, and the spring is sleeved on the shock-absorbing rod and located between the upper baffle and the lower baffle.
CN202220418826.XU 2022-02-25 2022-02-25 Unmanned aerial vehicle platform Active CN217198691U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220418826.XU CN217198691U (en) 2022-02-25 2022-02-25 Unmanned aerial vehicle platform

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220418826.XU CN217198691U (en) 2022-02-25 2022-02-25 Unmanned aerial vehicle platform

Publications (1)

Publication Number Publication Date
CN217198691U true CN217198691U (en) 2022-08-16

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ID=82753890

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202220418826.XU Active CN217198691U (en) 2022-02-25 2022-02-25 Unmanned aerial vehicle platform

Country Status (1)

Country Link
CN (1) CN217198691U (en)

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GR01 Patent grant
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CP01 Change in the name or title of a patent holder

Address after: 841007 room 101-120, No. 35, building 11, east entrance of 29tuan highway, Kuxi Industrial Park, Tiemenguan City, Bayingolin Mongol Autonomous Prefecture, Xinjiang Uygur Autonomous Region

Patentee after: Xinjiang Guannong Co.,Ltd.

Patentee after: Xinjiang guannong Testing Technology Co.,Ltd.

Address before: 841007 room 101-120, No. 35, building 11, east entrance of 29tuan highway, Kuxi Industrial Park, Tiemenguan City, Bayingolin Mongol Autonomous Prefecture, Xinjiang Uygur Autonomous Region

Patentee before: Xinjiang guannong fruit antler Co.,Ltd.

Patentee before: Xinjiang guannong Testing Technology Co.,Ltd.

CP01 Change in the name or title of a patent holder