CN218877589U - Unmanned aerial vehicle transport mechanism - Google Patents

Unmanned aerial vehicle transport mechanism Download PDF

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Publication number
CN218877589U
CN218877589U CN202223041658.6U CN202223041658U CN218877589U CN 218877589 U CN218877589 U CN 218877589U CN 202223041658 U CN202223041658 U CN 202223041658U CN 218877589 U CN218877589 U CN 218877589U
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China
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aerial vehicle
unmanned aerial
casing
groove
seted
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CN202223041658.6U
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Chinese (zh)
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简真友
徐桥桥
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Shantou Chenghai District Huacai Technology Industry And Trade Co ltd
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Individual
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Priority to CN202223041658.6U priority Critical patent/CN218877589U/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
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/70Energy storage systems for electromobility, e.g. batteries

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Abstract

The utility model relates to an unmanned aerial vehicle transports technical field, discloses an unmanned aerial vehicle transport mechanism, which comprises a housin, the opening has been seted up in the middle part of casing upper surface through running through, bolt fixedly connected with servo motor is passed through to one side of casing bottom inner wall, servo motor's motor shaft fixedly connected with lead screw, the top inner wall rotation that the bearing was passed through to the top of lead screw is connected with the casing. The utility model discloses put the constant head tank of a supporting bench upper surface to two sets of U-shaped undercarriage cards of unmanned aerial vehicle body bottom side, the control electro-magnet outage, through the elasticity of spring, can promote the iron plate and keep away from the electro-magnet, further promote the locating lever and insert to the constant head tank in, thereby carry on spacingly to the bottom of U-shaped undercarriage, control servo motor work, the silk pole can drive a supporting bench down and remove through, further drive unmanned aerial vehicle body income to the casing in, rock and collide in avoiding unmanned aerial vehicle body transportation.

Description

Unmanned aerial vehicle transport mechanism
Technical Field
The utility model relates to an unmanned aerial vehicle transports technical field, specifically is an unmanned aerial vehicle transport mechanism.
Background
Unmanned aerial vehicle is the unmanned aircraft that utilizes radio remote control equipment and the program control device of self-contained to control, in the application in fields such as aerial photography, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, observation wild animal, control infectious disease, survey and drawing, news report, electric power are patrolled and examined, relief of disaster, movie & TV are shot, make romantic, great expansion unmanned aerial vehicle's usage itself, after unmanned aerial vehicle uses, need accomodate the transportation.
The inventor finds that there is following problem among the prior art at least and does not obtain solving, and unmanned aerial vehicle is taking in the transportation, appears rocking easily and collides phenomenon such as damage, inconvenient subsequent taking off moreover.
Therefore, an unmanned aerial vehicle transfer mechanism is provided.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle transport mechanism has solved the problem that proposes in the background art.
In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle transport mechanism, includes the casing, the opening has been seted up in the middle part of casing upper surface through running through, bolt fixedly connected with servo motor is passed through to one side of casing bottom inner wall, servo motor's motor shaft fixedly connected with lead screw, the top of lead screw is passed through the bearing and is connected with the top inner wall rotation of casing, the inside of casing is provided with a supporting bench, the vertical run-through in middle part of supporting bench lower surface one side has seted up the thread groove, lead screw and thread groove threaded connection, the constant head tank has been seted up to the bilateral symmetry of supporting bench upper surface, the inner wall of constant head tank one side has been seted up and has been accomodate the groove, the inside sliding connection who accomodates the groove has the iron plate, the iron plate is close to the top level fixed mounting who accomodates groove one side and has the locating lever, the opposite side of iron plate is provided with the spring, accomodate one side of groove top inner wall through screw fixedly connected with the electro-magnet, the below level of iron plate has run through and has seted up the guide slot, the unmanned aerial vehicle body has been placed to the upper surface of supporting bench, the U-shaped undercarriage and constant head tank swing joint of opening.
As an alternative of this application technical scheme, locating lever and constant head tank swing joint, the locating lever cooperatees with the size of accomodating the groove, the unmanned aerial vehicle body cooperatees with the size of casing, surely accomodates the groove and can accomodate the locating lever, avoids the size overlength of locating lever, influences the U-shaped undercarriage and is connected with the constant head tank.
As an alternative of this application technical scheme, the vertical fixed mounting of the inside opposite side of casing has the gag lever post, the vertical run-through has seted up the spacing groove in the opposite side middle part of brace table lower surface, gag lever post and spacing groove sliding connection can improve the mobility stability of brace table, can carry on spacingly to the brace table simultaneously.
As an alternative of this application technical scheme, the horizontal fixed mounting in below of accomodating inslot portion has the guide arm, guide arm and guide slot sliding connection, the spring housing is established in the outside of guide arm, and the guide arm can carry on spacingly to the spring, improves the stability in use of spring.
As an alternative scheme of this application technical scheme, there is control panel the top of casing one side through screw fixedly connected with, control panel's input and external power constitute the electricity through the wire and are connected, control panel's output and servo motor and the input of electro-magnet constitute the electricity through the wire and are connected.
Compared with the prior art, the beneficial effects of the utility model are as follows, put two sets of U-shaped undercarriage cards of unmanned aerial vehicle body bottom side in the constant head tank of a supporting bench upper surface, the outage of control electro-magnet, through the elasticity of spring, can promote the iron plate and keep away from the electro-magnet, further promote the locating lever and insert to the constant head tank in, thereby carry on spacingly to the bottom of U-shaped undercarriage, control servo motor work, can drive a supporting bench down and remove through the lead screw, further drive unmanned aerial vehicle body income to the casing in, rock and collide in the unmanned aerial vehicle body transportation process.
Drawings
Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:
fig. 1 is a front view of an unmanned aerial vehicle transfer mechanism of the present invention;
fig. 2 is the utility model relates to an unmanned aerial vehicle transport mechanism's A position structure schematic diagram.
In the figure: the unmanned aerial vehicle comprises a shell 1, an opening 10, a servo motor 11, a screw rod 12, a support table 13, a thread groove 14, a positioning groove 15, a control panel 16, a containing groove 2, an iron block 21, a positioning rod 22, a spring 23, an electromagnet 24, a guide groove 25, a guide rod 26, an unmanned aerial vehicle body 27, a U-shaped undercarriage 28, a limiting rod 3, a limiting groove 31 and a cover plate 32.
Detailed Description
Referring to fig. 1-2, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle transport mechanism, which comprises a housin 1, the opening 10 has been seted up in the middle part of 1 upper surface of casing through running through, bolt fixedly connected with servo motor 11 is passed through to one side of 1 bottom inner wall of casing, servo motor 11's motor shaft fixedly connected with lead screw 12, the top of lead screw 12 is passed through the bearing and is connected with the top inner wall rotation of casing 1, the inside of casing 1 is provided with brace table 13, the vertical thread groove 14 of having seted up that runs through in middle part of brace table 13 lower surface one side, lead screw 12 and 14 threaded connection of thread groove, constant head tank 15 has been seted up to the bilateral symmetry of brace table 13 upper surface, screw fixedly connected with control panel 16 is passed through to the top of casing 1 one side, control servo motor 11 works, warp screw 12 can drive brace table 13 and reciprocate, make things convenient for accomodating and taking off of unmanned aerial vehicle body 27.
The inner wall of constant head tank 15 one side has been seted up and has been accomodate groove 2, the inside sliding connection who accomodates groove 2 has iron plate 21, iron plate 21 is close to the top level fixed mounting who accomodates groove 2 one side has locating lever 22, iron plate 21's opposite side is provided with spring 23, there is electromagnet 24 one side of accomodating groove 2 top inner wall through screw fixedly connected with, iron plate 21's below level runs through and has been seted up guide slot 25, accomodate the inside below level fixed mounting in groove 2 has guide arm 26, guide arm 26 and guide slot 25 sliding connection, spring 23 cover is established in the outside of guide arm 26, unmanned aerial vehicle body 27 has been placed to the upper surface of brace table 13, U-shaped undercarriage 28 and constant head tank 15 swing joint of unmanned aerial vehicle body 27 bottom side, put two sets of U-shaped undercarriage 28 cards of unmanned aerial vehicle body 27 bottom side in the constant head tank 25 of brace table 13 upper surface, control electromagnet 24 cuts off the power supply, elasticity through spring 23, can promote iron plate 21 and keep away from electromagnet 24, further promote locating lever 22 to insert to constant head tank 15, thereby it is spacing to carry out bottom to U-shaped 28.
The vertical fixed mounting of the inside opposite side of casing 1 has gag lever post 3, and the vertical run-through has been seted up in the opposite side middle part of brace table 13 lower surface has spacing groove 31, gag lever post 3 and spacing groove 31 sliding connection, and the top swing joint of opening 10 has apron 32, can improve the mobility stability of brace table 13 in casing 1, can carry on spacingly to brace table 13 simultaneously.
When an unmanned aerial vehicle transfer mechanism uses, put two sets of U-shaped undercarriage 28 card of unmanned aerial vehicle body 27 bottom side in the constant head tank 25 of brace table 13 upper surface, control electro-magnet 24 cuts off the power supply, elasticity through spring 23, can promote iron plate 21 and keep away from electro-magnet 24, further promote locating lever 22 and insert in constant head tank 15, thereby carry on spacingly to the bottom of U-shaped undercarriage 28, control servo motor 11 work, can drive brace table 13 through lead screw 12 and move down, conveniently transport unmanned aerial vehicle body 27 income to casing 1, when needing to use unmanned aerial vehicle body 27, control servo motor 11 work drives lead screw 12 antiport, can promote unmanned aerial vehicle body 27 above brace table 13 and shift out casing 1 through opening 10, control electro-magnet 24 work produces magnetic attraction, can attract and fix iron plate 21, further stimulate locating lever 22 income to accomodating in groove 2, make things convenient for taking off of unmanned aerial vehicle body 27.

Claims (5)

1. The utility model provides an unmanned aerial vehicle transport mechanism, a serial communication port, which comprises a housin, the opening has been seted up in the middle part of casing upper surface through running through, bolt fixedly connected with servo motor is passed through to one side of casing bottom inner wall, servo motor's motor shaft fixedly connected with lead screw, the top of lead screw is passed through the top inner wall rotation of bearing and casing and is connected, the inside of casing is provided with a supporting bench, the vertical run through in middle part of supporting bench lower surface one side has seted up the thread groove, lead screw and thread groove threaded connection, the constant head tank has been seted up to the bilateral symmetry of supporting bench upper surface, the inner wall of constant head tank one side has been seted up and has been accomodate the groove, the inside sliding connection who accomodates the groove has the iron plate, the iron plate is close to the top level fixed mounting who accomodates groove one side, the opposite side of iron plate is provided with the spring, one side of accomodating groove top inner wall is through screw fixedly connected with the electro-magnet, the below level of iron plate has been run through and has been seted up the guide slot, the unmanned aerial vehicle body has been placed to the upper surface of supporting bench, the unmanned aerial vehicle body's U-shaped undercarriage and constant head tank swing joint, the top of opening is connected with the apron.
2. The unmanned aerial vehicle transfer mechanism of claim 1, wherein: the locating lever and constant head tank swing joint, the locating lever cooperatees with the size of accomodating the groove, the unmanned aerial vehicle body cooperatees with the size of casing.
3. An unmanned aerial vehicle transfer mechanism of claim 1, wherein: the vertical fixed mounting of the inside opposite side of casing has the gag lever post, the vertical run-through has seted up the spacing groove in the opposite side middle part of brace table lower surface, gag lever post and spacing groove sliding connection.
4. The unmanned aerial vehicle transfer mechanism of claim 1, wherein: the guide rod is horizontally and fixedly arranged below the inner part of the accommodating groove, the guide rod is connected with the guide groove in a sliding mode, and the spring sleeve is arranged on the outer side of the guide rod.
5. The unmanned aerial vehicle transfer mechanism of claim 1, wherein: the top of casing one side is through screw fixedly connected with control panel, control panel's input and external power constitute the electricity through the wire and are connected, control panel's output and servo motor and the input of electro-magnet constitute the electricity through the wire and are connected.
CN202223041658.6U 2022-11-16 2022-11-16 Unmanned aerial vehicle transport mechanism Active CN218877589U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202223041658.6U CN218877589U (en) 2022-11-16 2022-11-16 Unmanned aerial vehicle transport mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202223041658.6U CN218877589U (en) 2022-11-16 2022-11-16 Unmanned aerial vehicle transport mechanism

Publications (1)

Publication Number Publication Date
CN218877589U true CN218877589U (en) 2023-04-18

Family

ID=85938301

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202223041658.6U Active CN218877589U (en) 2022-11-16 2022-11-16 Unmanned aerial vehicle transport mechanism

Country Status (1)

Country Link
CN (1) CN218877589U (en)

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Effective date of registration: 20230526

Address after: 515000 North side of Guangyi Road, Guangyi Street, Chenghai District, Shantou City, Guangdong Province

Patentee after: Shantou Chenghai District Huacai Technology Industry and Trade Co.,Ltd.

Address before: No. 458 Shangtang Road, Gongshu District, Hangzhou City, Zhejiang Province, 310000

Patentee before: Jian Zhenyou