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CN109502040B - A fixed storage device for unmanned aerial vehicle and a platform fixing method thereof - Google Patents

  • ️Tue Nov 12 2024
A fixed storage device for unmanned aerial vehicle and a platform fixing method thereof Download PDF

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Publication number
CN109502040B
CN109502040B CN201811635145.3A CN201811635145A CN109502040B CN 109502040 B CN109502040 B CN 109502040B CN 201811635145 A CN201811635145 A CN 201811635145A CN 109502040 B CN109502040 B CN 109502040B Authority
CN
China
Prior art keywords
platform
aerial vehicle
unmanned aerial
remote
parking platform
Prior art date
2018-12-29
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CN201811635145.3A
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CN109502040A (en
Inventor
蔡仁平
王洋
刘寒辉
牟俊其
朱智佳
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Shenzhen DY Innovations Technology Co ltd
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Shenzhen DY Innovations Technology Co ltd
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2018-12-29
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2018-12-29
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2024-11-12
2018-12-29 Application filed by Shenzhen DY Innovations Technology Co ltd filed Critical Shenzhen DY Innovations Technology Co ltd
2018-12-29 Priority to CN201811635145.3A priority Critical patent/CN109502040B/en
2019-03-22 Publication of CN109502040A publication Critical patent/CN109502040A/en
2024-11-12 Application granted granted Critical
2024-11-12 Publication of CN109502040B publication Critical patent/CN109502040B/en
Status Active legal-status Critical Current
2038-12-29 Anticipated expiration legal-status Critical

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • 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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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

本发明公开了一种无人机的固定存放装置及其平台固定方法,包括综合无人机应用平台,所述综合无人机应用平台上设置有双开的开关门,所述综合无人机应用平台的顶部活动安装有天窗,所述天窗为左右对称设置,所述综合无人机应用平台的顶端为停机平台,所述停机平台上停放有遥控无人飞机。本发明的有益效果是:不仅可以让无人机随时处于准备起飞的状态而且还简化了操作流程,同时还能够缩减综合无人机平台的空间。

The present invention discloses a fixed storage device for unmanned aerial vehicles and a platform fixing method thereof, comprising an integrated unmanned aerial vehicle application platform, the integrated unmanned aerial vehicle application platform is provided with a double-opening switch door, a skylight is movably installed on the top of the integrated unmanned aerial vehicle application platform, the skylight is symmetrically arranged, the top of the integrated unmanned aerial vehicle application platform is a parking platform, and a remote-controlled unmanned aircraft is parked on the parking platform. The beneficial effects of the present invention are: not only can the unmanned aerial vehicle be ready to take off at any time, but also the operation process is simplified, and at the same time, the space of the integrated unmanned aerial vehicle platform can be reduced.

Description

Fixed storage device of unmanned aerial vehicle and platform fixing method thereof

Technical Field

The invention relates to the technical field of unmanned aerial vehicles, in particular to a fixed storage device of an unmanned aerial vehicle and a platform fixing method thereof.

Background

The comprehensive unmanned aerial vehicle application platform rapidly develops. And when synthesizing unmanned aerial vehicle application platform transportation and dormancy state, need protect unmanned aerial vehicle in the platform, avoid unmanned aerial vehicle damage. The invention solves the problem, and achieves the functions of protection and positioning by additionally arranging a device for fixing the unmanned aerial vehicle in the comprehensive platform.

Disclosure of Invention

The invention solves the technical problem of overcoming the defects existing in the prior art and provides a fixed storage device of an unmanned aerial vehicle and a platform fixing method thereof. The unmanned aerial vehicle fixing and storing device and the platform fixing method thereof not only can enable the unmanned aerial vehicle to be in a state of being ready for take-off at any time, but also can simplify the operation flow, and meanwhile, the space of the comprehensive unmanned aerial vehicle platform can be reduced.

In order to achieve the above purpose, the present invention provides the following technical solutions:

The utility model provides a fixed strorage device of unmanned aerial vehicle and platform fixed method thereof, includes synthesizing unmanned aerial vehicle application platform, be provided with the switch door of two divisions on the synthesize unmanned aerial vehicle application platform, synthesize unmanned aerial vehicle application platform's top movable mounting has the skylight, the skylight is bilateral symmetry setting, synthesize unmanned aerial vehicle application platform's top for shutting down the platform, it has the remote control unmanned aerial vehicle to park on the platform to shut down.

Preferably, the shutdown platform comprises a rail groove, the rail groove penetrates through the upper bottom and the lower bottom of the shutdown platform, a servo driving device is fixedly installed at the bottom of the shutdown platform, a limiting block is fixedly installed on the driving device, the limiting block is movably clamped with the remote control unmanned plane, and the limiting block is located at the top of the shutdown platform.

Preferably, the driving device comprises a servo motor, the power output end of the servo motor is fixedly connected with a rotating shaft, two ends of the rotating shaft are vertically and drivingly connected with a synchronous belt, a sliding block is fixedly arranged on the synchronous belt, a guide shaft is arranged on the sliding block, the direction of the guide shaft is identical to the setting direction of the synchronous belt and is positioned under the synchronous belt, and the limiting block is fixedly arranged on the sliding block.

Preferably, the track grooves are arranged in a 'well' -shaped manner, the synchronous belt is positioned in the track grooves, and the synchronous belt is designed in an up-down dislocation manner at the crossing of the track grooves.

Preferably, the inner wall both sides of synthesizing unmanned aerial vehicle application platform all are provided with the unipolar manipulator, synthesize unmanned aerial vehicle application platform's inner chamber bottom and be provided with battery package and battery controller, battery package and battery controller set up side by side and the top is provided with the protection apron, the top fixed mounting of protection apron has the horn locating part.

Preferably, the horn limiting part comprises four vertical rods fixedly installed on the protection cover plate and a charging pile, wherein a clamping groove for clamping the remote control unmanned aerial vehicle is formed in the top of the vertical rods, and elastic cards are arranged on two sides of the clamping groove.

Preferably, the bottom of remote control unmanned aerial vehicle is provided with the supporting legs, the supporting legs comprises two "T" type poles that the symmetry set up, has all cup jointed the podotheca at the bottom both ends of "T" type pole, and two mutual symmetrical supporting legs pass through fixed connection's carbon tube interconnect on the podotheca.

Preferably, the single-shaft manipulator mainly comprises a single-shaft driver and a manipulator, wherein one end of the manipulator far away from the single-shaft driver is bifurcated into a Y-shaped structure.

The platform fixing method of the fixed storage device of the unmanned aerial vehicle is characterized by comprising the following specific steps:

S1: when the remote control unmanned aerial vehicle falls in the stopping platform, the driving device moving in the front-back direction pushes the unmanned remote control to the middle position, so that the limiting block in the front-back direction can realize front-back fixation;

S2: after the previous step is finished, the driving device moving in the left-right direction pushes the remote control unmanned aerial vehicle to the middle position of the stopping platform, so that the limiting blocks at the left side and the right side realize the fixation in the left-right direction;

S3: after the remote control unmanned aerial vehicle is fixed on the shutdown platform, the shutdown platform starts to descend through the single-shaft manipulator, and when the shutdown platform descends to a preset height, the horn limiting parts can extend through the shutdown platform to fix four horns of the remote control unmanned aerial vehicle, so that the whole aircraft is fixed.

The platform fixing method of the fixed storage device of the unmanned aerial vehicle is characterized by comprising the following specific steps:

the first step: when the remote control unmanned aerial vehicle falls in the stopping platform, the driving device moving in the front-back direction pushes the unmanned remote control to the middle position, so that the limiting block in the front-back direction can realize front-back fixation;

And a second step of: after the previous step is finished, the driving device moving in the left-right direction pushes the remote control unmanned aerial vehicle to the middle position of the stopping platform, so that the limiting blocks at the left side and the right side realize the fixation in the left-right direction;

and a third step of: when the remote control unmanned aerial vehicle is fixed on the shutdown platform, the shutdown platform starts to descend through the single-shaft manipulator, and when the shutdown platform descends to a preset height, the left side and the right side of the remote control unmanned aerial vehicle respectively extend out of one manipulator through the single-shaft driver to grasp four arms of the aircraft.

Compared with the prior art, the invention has the beneficial effects that: the unmanned aerial vehicle can be in a state of taking off at any time, the operation flow is simplified, and meanwhile, the space of the comprehensive unmanned aerial vehicle platform can be reduced.

Drawings

FIG. 1 is a schematic diagram of the structure of the present invention;

FIG. 2 is a schematic view of a shutdown platform according to the present invention;

FIG. 3 is a schematic diagram of a driving apparatus according to the present invention;

FIG. 4 is a schematic view of the internal structure of the present invention;

FIG. 5 is a schematic view of the arm stop of the present invention;

FIG. 6 is a schematic view of the structure of the elastic card at the top of the arm limiter of the present invention;

FIG. 7 is a schematic view of the structure of the unmanned aerial vehicle of the present invention;

FIG. 8 is a schematic view of a remote unmanned aerial vehicle securing means of the present invention;

Fig. 9 is a schematic diagram of a stopper structure according to the present invention.

Reference numerals in the drawings: 1 comprehensive unmanned aerial vehicle application platform, 2 switch door, 3 skylight, 4 remote control unmanned aerial vehicle, 401 podotheca, 402 carbon tube, 5 platform, 501 track groove, 6 drive arrangement, 601 servo motor, 602 rotation axis, 603 synchronous belt, 604 slider, 605 guiding axle, 7 stopper, 8 unipolar manipulator, 801 unipolar driver, 802 manipulator, 9 battery package, 10 battery controller, 11 horn locating part, 12 protection apron, 13 fills electric pile, 14 elasticity cards.

Detailed Description

The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.

Referring to fig. 1-8, the present invention provides a technical solution: the utility model provides a fixed strorage device of unmanned aerial vehicle, includes synthesizes unmanned aerial vehicle application platform 1, synthesize and be provided with the switch door 2 of double-open on the unmanned aerial vehicle application platform 1, synthesize the top movable mounting of unmanned aerial vehicle application platform 1 and have skylight 3, skylight 3 is bilateral symmetry setting, synthesize the top of unmanned aerial vehicle application platform 1 and be shut down platform 5, it is notable that remote control unmanned aerial vehicle 4 has been parked on shut down platform 5, the bottom of remote control unmanned aerial vehicle 4 is provided with the supporting legs, the supporting legs comprises two symmetrical "T" type poles that set up, has cup jointed foot cover 401 at the bottom both ends of "T" type pole, and two mutually symmetrical supporting legs pass through the carbon tube 402 interconnect of fixed connection on the foot cover 401, and notably, shut down platform 5 includes track groove 501, the track groove 501 penetrates through the upper bottom and the lower bottom of the shutdown platform 5, the bottom of the shutdown platform 5 is fixedly provided with a servo driving device 6, the driving device 6 is fixedly provided with a limiting block 7, the limiting block 7 is movably clamped with the remote control unmanned aerial vehicle 4, the limiting block 7 is positioned at the top of the shutdown platform 5, it is worth noting that both sides of the inner wall of the comprehensive unmanned aerial vehicle application platform 1 are provided with single-shaft manipulators 8, wherein the single-shaft manipulators 8 mainly comprise single-shaft drivers 801 and manipulators 802, one ends of the manipulators 802 far away from the single-shaft drivers 801 are branched into a Y-shaped structure, the bottom of the inner cavity of the comprehensive unmanned aerial vehicle application platform 1 is provided with a battery pack 9 and a battery controller 10, the battery pack 9 and the battery controller 10 are arranged side by side, the top is provided with a protection cover plate 12, the top of the protective cover plate 12 is fixedly provided with an organic arm limiting part 11.

It is noted that the driving device 6 includes a servo motor 601, a power output end of the servo motor 601 is fixedly connected with a rotating shaft 602, two ends of the rotating shaft 602 are vertically and drivingly connected with a synchronous belt 603, a sliding block 604 is fixedly installed on the synchronous belt 603, a guide shaft 605 is configured on the sliding block 604, the direction of the guide shaft 605 is the same as the setting direction of the synchronous belt 603 and is located under the synchronous belt 603, a limiting block 7 is fixedly installed on the sliding block 604, the track grooves 501 are arranged in a 'well' -shaped manner, the synchronous belt 603 is located in the track grooves 501, and the synchronous belt 603 is designed in an up-down staggered manner at the crossing position of the track grooves 501.

It should be noted that the arm limiting member 11 comprises four vertical rods fixedly installed on the protective cover 12 and a charging pile 13, wherein a clamping groove for clamping the remote control unmanned aerial vehicle 4 is formed in the top of the vertical rods, and elastic cards 14 are arranged on two sides of the clamping groove.

For a platform fixing method of a fixed storage device of an unmanned aerial vehicle, the method comprises the following specific steps:

embodiment one:

S1: when the remote control unmanned aerial vehicle 4 falls in the stopping platform 5, the driving device 6 moving in the front-back direction pushes the unmanned remote control 4 to the middle position, so that the limiting block 7 in the front-back direction can realize front-back fixation;

S2: after the previous step is finished, the driving device 6 moving in the left-right direction pushes the remote control unmanned aerial vehicle 4 to the middle position of the stopping platform 5, so that the limiting blocks 7 at the left side and the right side realize the fixation in the left-right direction;

S3: after the remote control unmanned aerial vehicle 4 is fixed on the shutdown platform 5, the shutdown platform 5 starts to descend through the single-shaft manipulator 8, and when the shutdown platform falls to a preset height, the horn limiting pieces 11 can extend through the shutdown platform 5 to fix the four horns of the remote control unmanned aerial vehicle 4, so that the whole airplane is fixed.

Embodiment two:

The first step: when the remote control unmanned aerial vehicle 4 falls in the stopping platform 5, the driving device 6 moving in the front-back direction pushes the unmanned remote control 4 to the middle position, so that the limiting block 7 in the front-back direction can realize front-back fixation;

and a second step of: after the previous step is finished, the driving device 6 moving in the left-right direction pushes the remote control unmanned aerial vehicle 4 to the middle position of the stopping platform 5, so that the limiting blocks 7 at the left side and the right side realize the fixation in the left-right direction;

And a third step of: when the remote control unmanned aerial vehicle 4 is fixed on the shutdown platform 5, the shutdown platform 5 starts to descend through the single-shaft manipulator 8, and when the shutdown platform descends to a preset height, the left side and the right side of the remote control unmanned aerial vehicle 4 extend out of one manipulator 802 respectively through the single-shaft driver 801 to grasp four arms of the aircraft.

Principle of operation

The unmanned aerial vehicle is fixed in four different directions by the parking platform 5 through the servo motor 601 and the synchronous belt 603, and is pushed to the middle part of the parking platform 5 through the servo motor 601, and after the pushing process is finished, the limiting block 7 on the synchronous belt 603 just can buckle two supporting legs of the unmanned aerial vehicle; after the fixation is completed, the whole parking platform 5 and the unmanned aerial vehicle can be lowered together through the single-shaft manipulator 8, the whole parking platform can be fixed through the horn limiting part 11 after the whole parking platform is lowered, the whole parking platform can be fixed through the manipulator 802, and then the unmanned aerial vehicle can be charged by matching with the charging pile 13.

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

Claims (8)

1.一种无人机的固定存放装置的平台固定方法,所述固定存放装置包括综合无人机应用平台(1),其特征在于:所述综合无人机应用平台(1)上设置有双开的开关门(2),所述综合无人机应用平台(1)的顶部活动安装有天窗(3),所述天窗(3)为左右对称设置,所述综合无人机应用平台(1)的顶端为停机平台(5),所述停机平台(5)上停放有遥控无人飞机(4);所述停机平台(5) 包括轨道槽(501),所述轨道槽(501)贯穿停机平台(5)的上下底,所述停机平台(5)的底部还固定安装有驱动装置(6),所述驱动装置(6)上固定安装有限位块(7),所述限位块(7)活动卡接遥控无人飞机(4),所述限位块(7)位于停机平台(5)的顶部;所述综合无人机应用平台(1)的内壁两侧均设置有单轴机械手(8),所述综合无人机应用平台(1)的内腔底部设置有电池包(9)和电池控制器(10),所述电池包(9)和电池控制器(10)并排设置且顶部设置有保护盖板(12),所述保护盖板(12)的顶部固定安装有机臂限位件(11);所述机臂限位件(11)具有由四根固定安装在保护盖板(12)的竖杆和充电桩(13)组成,其中所述竖杆的顶部开设有用于卡接遥控无人飞机(4)的卡槽,在卡槽的两侧设置有弹性卡片(14);1. A platform fixing method for a fixed storage device of an unmanned aerial vehicle, the fixed storage device comprising an integrated unmanned aerial vehicle application platform (1), characterized in that: the integrated unmanned aerial vehicle application platform (1) is provided with a double-opening switch door (2), the top of the integrated unmanned aerial vehicle application platform (1) is movably provided with a skylight (3), the skylight (3) is symmetrically arranged, the top of the integrated unmanned aerial vehicle application platform (1) is a parking platform (5), a remote-controlled unmanned aircraft (4) is parked on the parking platform (5); the parking platform (5) The invention comprises a track groove (501), wherein the track groove (501) passes through the upper and lower bottoms of a parking platform (5), a driving device (6) is fixedly installed on the bottom of the parking platform (5), a limit block (7) is fixedly installed on the driving device (6), the limit block (7) is movably connected to a remote-controlled unmanned aircraft (4), and the limit block (7) is located at the top of the parking platform (5); single-axis manipulators (8) are arranged on both sides of the inner wall of the integrated unmanned aircraft application platform (1), and the inner cavity bottom of the integrated unmanned aircraft application platform (1) is provided with a plurality of mechanical arms (8). A battery pack (9) and a battery controller (10) are provided on the top of the battery pack (9) and the battery controller (10), the battery pack (9) and the battery controller (10) are arranged side by side and a protective cover (12) is provided on the top of the protective cover (12), an arm stopper (11) is fixedly installed on the top of the protective cover (12); the arm stopper (11) comprises four vertical rods fixedly installed on the protective cover (12) and a charging pile (13), wherein a card slot for clamping a remote-controlled unmanned aircraft (4) is provided on the top of the vertical rod, and elastic cards (14) are provided on both sides of the card slot; 所述平台固定方法,包括具体步骤如下:The platform fixing method comprises the following specific steps: S1:当遥控无人飞机(4)降落在停机平台(5)内时,前后方向运动的驱动装置(6)将遥控无人飞机(4)推至中间位置,这样前后方向上的限位块(7)就可以实现前后的固定;S1: When the remote-controlled unmanned aircraft (4) lands on the parking platform (5), the driving device (6) moving in the front-to-back direction pushes the remote-controlled unmanned aircraft (4) to the middle position, so that the limit blocks (7) in the front-to-back direction can achieve front-to-back fixation; S2:当上个步骤完成后,左右方向移动的驱动装置(6)将遥控无人飞机(4)推送至停机平台(5)的中间位置,这样左右两侧的限位块(7)就实现了左右方向的固定;S2: After the previous step is completed, the driving device (6) that moves in the left and right directions pushes the remote-controlled unmanned aircraft (4) to the middle position of the parking platform (5), so that the limit blocks (7) on the left and right sides can achieve left and right fixation; S3:当遥控无人飞机(4)固定在停机平台(5)上后,停机平台(5)通过单轴机械手(8)开始下降,当下降到预定的高度时,机臂限位件(11)会伸过停机平台(5)将遥控无人飞机(4)的四个机臂固定住,这样整个飞机就得到固定。S3: After the remote-controlled unmanned aircraft (4) is fixed on the parking platform (5), the parking platform (5) begins to descend through the single-axis manipulator (8). When it descends to a predetermined height, the arm limiter (11) extends over the parking platform (5) to fix the four arms of the remote-controlled unmanned aircraft (4), so that the entire aircraft is fixed. 2.根据权利要求1所述的一种无人机的固定存放装置的平台固定方法,其特征在于:所述驱动装置(6)包括伺服电机(601),所述伺服电机(601)的动力输出端固定连接旋转轴(602),所述旋转轴(602)的两端均垂直传动连接有同步皮带(603),所述同步皮带(603)上固定安装有滑块(604),所述滑块(604)上配置有导向轴(605),所述导向轴(605)的方向与同步皮带(603)的设置方向相同且位于同步皮带(603)的正下方,所述限位块(7)固定安装于滑块(604)上。2. A platform fixing method for a fixed storage device of an unmanned aerial vehicle according to claim 1, characterized in that: the driving device (6) comprises a servo motor (601), the power output end of the servo motor (601) is fixedly connected to a rotating shaft (602), both ends of the rotating shaft (602) are vertically connected to a synchronous belt (603), a slider (604) is fixedly installed on the synchronous belt (603), a guide shaft (605) is arranged on the slider (604), the direction of the guide shaft (605) is the same as the setting direction of the synchronous belt (603) and is located directly below the synchronous belt (603), and the limit block (7) is fixedly installed on the slider (604). 3.根据权利要求2所述的一种无人机的固定存放装置的平台固定方法,其特征在于:所述轨道槽(501)呈“井”字型排列设置,所述同步皮带(603)则位于轨道槽(501)内,在轨道槽(501)的交叉处,所述同步皮带(603)采用上下错位的方式进行设计。3. A platform fixing method for a fixed storage device of an unmanned aerial vehicle according to claim 2, characterized in that: the track groove (501) is arranged in a "well" shape, and the synchronous belt (603) is located in the track groove (501), and at the intersection of the track groove (501), the synchronous belt (603) is designed in an up-down staggered manner. 4.根据权利要求1所述的一种无人机的固定存放装置的平台固定方法,其特征在于:所述遥控无人飞机(4)的底部设置有支撑脚,所述支撑脚由两个对称设置的“T”型杆组成,在“T”型杆的底部两端均套接有脚套(401),两个相互对称的支撑脚通过脚套(401)上固定连接的碳管(402)相互连接。4. The platform fixing method of a fixed storage device for an unmanned aerial vehicle according to claim 1 is characterized in that: a supporting foot is arranged at the bottom of the remote-controlled unmanned aircraft (4), and the supporting foot is composed of two symmetrically arranged "T"-shaped rods, and foot sleeves (401) are sleeved at both ends of the bottom of the "T"-shaped rods, and the two mutually symmetrical supporting feet are connected to each other through a carbon tube (402) fixedly connected to the foot sleeve (401). 5.一种无人机的固定存放装置的平台固定方法,所述固定存放装置包括综合无人机应用平台(1),其特征在于:所述综合无人机应用平台(1)上设置有双开的开关门(2),所述综合无人机应用平台(1)的顶部活动安装有天窗(3),所述天窗(3)为左右对称设置,所述综合无人机应用平台(1)的顶端为停机平台(5),所述停机平台(5)上停放有遥控无人飞机(4);所述停机平台(5) 包括轨道槽(501),所述轨道槽(501)贯穿停机平台(5)的上下底,所述停机平台(5)的底部还固定安装有驱动装置(6),所述驱动装置(6)上固定安装有限位块(7),所述限位块(7)活动卡接遥控无人飞机(4),所述限位块(7)位于停机平台(5)的顶部;所述综合无人机应用平台(1)的内壁两侧均设置有单轴机械手(8),所述综合无人机应用平台(1)的内腔底部设置有电池包(9)和电池控制器(10),所述电池包(9)和电池控制器(10)并排设置且顶部设置有保护盖板(12),所述保护盖板(12)的顶部固定安装有机臂限位件(11);所述单轴机械手 (8)主要由单轴驱动器(801)和机械手(802)组成,其中所述机械手(802)远离单轴驱动器 (801)的一端分叉呈“Y”字型结构;所述平台固定方法,包括具体步骤如下:5. A platform fixing method for a fixed storage device of an unmanned aerial vehicle, the fixed storage device comprising an integrated unmanned aerial vehicle application platform (1), characterized in that: the integrated unmanned aerial vehicle application platform (1) is provided with a double-opening switch door (2), the top of the integrated unmanned aerial vehicle application platform (1) is movably provided with a skylight (3), the skylight (3) is symmetrically arranged, the top of the integrated unmanned aerial vehicle application platform (1) is a parking platform (5), a remote-controlled unmanned aircraft (4) is parked on the parking platform (5); the parking platform (5) The invention comprises a track groove (501), wherein the track groove (501) passes through the upper and lower bottoms of a parking platform (5), and a driving device (6) is fixedly installed at the bottom of the parking platform (5), and a limit block (7) is fixedly installed on the driving device (6), and the limit block (7) is movably connected to a remote-controlled unmanned aircraft (4), and the limit block (7) is located at the top of the parking platform (5); single-axis manipulators (8) are arranged on both sides of the inner wall of the integrated unmanned aerial vehicle application platform (1), and a battery pack (9) and a battery controller (10) are arranged at the bottom of the inner cavity of the integrated unmanned aerial vehicle application platform (1), and the battery pack (9) and the battery controller (10) are arranged side by side and a protective cover plate (12) is arranged on the top, and an arm limiter (11) is fixedly installed on the top of the protective cover plate (12); the single-axis manipulator (8) is mainly composed of a single-axis driver (801) and a manipulator (802), wherein the manipulator (802) is far away from the single-axis driver. One end of (801) is bifurcated into a "Y"-shaped structure; the platform fixing method includes the following specific steps: 第一步:当遥控无人飞机(4)降落在停机平台(5)内时,前后方向运动的驱动装置(6)将遥控无人飞机(4)推至中间位置,这样前后方向上的限位块(7)就可以实现前后的固定;Step 1: When the remote-controlled unmanned aircraft (4) lands on the parking platform (5), the driving device (6) that moves in the front-to-back direction pushes the remote-controlled unmanned aircraft (4) to the middle position, so that the limit blocks (7) in the front-to-back direction can achieve front-to-back fixation; 第二步:当上个步骤完成后,左右方向移动的驱动装置(6)将遥控无人飞机(4)推送至停机平台(5)的中间位置,这样左右两侧的限位块(7)就实现了左右方向的固定;Step 2: After the previous step is completed, the driving device (6) that moves in the left and right directions pushes the remote-controlled unmanned aircraft (4) to the middle position of the parking platform (5), so that the limit blocks (7) on the left and right sides can achieve left and right fixation; 第三步:当遥控无人飞机(4)固定在停机平台(5)上时,停机平台(5)通过单轴机械手(8)开始下降,当下降到预定的高度时,遥控无人飞机(4)的左右两侧均通过单轴驱动器(801)各伸出一个机械手(802)将飞机的四个机臂抓住。Step 3: When the remote-controlled unmanned aircraft (4) is fixed on the parking platform (5), the parking platform (5) begins to descend through the single-axis manipulator (8). When it descends to a predetermined height, a manipulator (802) is extended from each of the left and right sides of the remote-controlled unmanned aircraft (4) through the single-axis driver (801) to grab the four arms of the aircraft. 6.根据权利要求5所述的一种无人机的固定存放装置的平台固定方法,其特征在于:所述驱动装置(6)包括伺服电机(601),所述伺服电机(601)的动力输出端固定连接旋转轴(602),所述旋转轴(602)的两端均垂直传动连接有同步皮带(603),所述同步皮带(603)上固定安装有滑块(604),所述滑块(604)上配置有导向轴(605),所述导向轴(605)的方向与同步皮带(603)的设置方向相同且位于同步皮带(603)的正下方,所述限位块(7)固定安装于滑块(604)上。6. A platform fixing method for a fixed storage device of an unmanned aerial vehicle according to claim 5, characterized in that: the driving device (6) comprises a servo motor (601), the power output end of the servo motor (601) is fixedly connected to a rotating shaft (602), both ends of the rotating shaft (602) are vertically connected to a synchronous belt (603), a slider (604) is fixedly installed on the synchronous belt (603), a guide shaft (605) is arranged on the slider (604), the direction of the guide shaft (605) is the same as the setting direction of the synchronous belt (603) and is located directly below the synchronous belt (603), and the limit block (7) is fixedly installed on the slider (604). 7.根据权利要求6所述的一种无人机的固定存放装置的平台固定方法,其特征在于:所述轨道槽(501)呈“井”字型排列设置,所述同步皮带(603)则位于轨道槽(501)内,在轨道槽(501)的交叉处,所述同步皮带(603)采用上下错位的方式进行设计。7. A platform fixing method for a fixed storage device of an unmanned aerial vehicle according to claim 6, characterized in that: the track grooves (501) are arranged in a "well" shape, and the synchronous belt (603) is located in the track grooves (501), and at the intersection of the track grooves (501), the synchronous belt (603) is designed in an up-down staggered manner. 8.根据权利要求5所述的一种无人机的固定存放装置的平台固定方法,其特征在于:所述遥控无人飞机(4)的底部设置有支撑脚,所述支撑脚由两个对称设置的“T”型杆组成,在“T”型杆的底部两端均套接有脚套(401),两个相互对称的支撑脚通过脚套(401)上固定连接的碳管(402)相互连接。8. The platform fixing method of a fixed storage device for an unmanned aerial vehicle according to claim 5, characterized in that: a supporting foot is arranged at the bottom of the remote-controlled unmanned aircraft (4), and the supporting foot is composed of two symmetrically arranged "T"-shaped rods, and foot sleeves (401) are sleeved at both ends of the bottom of the "T"-shaped rods, and the two mutually symmetrical supporting feet are connected to each other through a carbon tube (402) fixedly connected to the foot sleeve (401).

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