CN207956084U - A kind of open adjustable carry platform applied on unmanned plane - Google Patents

A kind of open adjustable carry platform applied on unmanned plane Download PDF

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Publication number
CN207956084U
CN207956084U CN201820136835.3U CN201820136835U CN207956084U CN 207956084 U CN207956084 U CN 207956084U CN 201820136835 U CN201820136835 U CN 201820136835U CN 207956084 U CN207956084 U CN 207956084U
Authority
CN
China
Prior art keywords
cross
arm
carry
unmanned plane
slide bar
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201820136835.3U
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Chinese (zh)
Inventor
黄永明
梁生智
邓坤南
卢洪涛
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Guangzhou Guanghong Aviation Science And Technology Co Ltd
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Guangzhou Guanghong Aviation Science And Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Priority to CN201820136835.3U priority Critical patent/CN207956084U/en
Application granted granted Critical
Publication of CN207956084U publication Critical patent/CN207956084U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model is related to a kind of open adjustable carry platforms applied on unmanned plane, including:Cross-arm and two identical and placed side by side slide bars;Vertically fixed intersection, described slide bar one end are detachably provided with the cross-arm of the first quantity for the slide bar and the horizontal segment on unmanned aerial vehicle rack top, and the detachable other end of the slide bar is provided with the cross-arm of the second quantity;It is provided on the cross-arm for the fixed mounting hole for waiting for carry equipment.Cross-arm and the sliding rail on the open adjustable carry platform of the utility model are detachably connected.When cross-arm and sliding rail are releasing orientation, position of the cross-arm on sliding rail can be moved.When cross-arm and sliding rail are locking state, the position of cross-arm is fixed, in this way will be after carry hanging equipment is loaded on the cross-arm at slide bar both ends, the weight of carry equipment can be waited for both ends, cross-arm is moved in the position of sliding rail, adjusts the center of gravity of unmanned plane, unmanned plane is made to balance.

Description

A kind of open adjustable carry platform applied on unmanned plane
Technical field
The utility model is related to air vehicle technique field, more particularly to it is a kind of apply it is open adjustable on unmanned plane Carry platform.
Background technology
Application of the technical grade multi-rotor unmanned aerial vehicle in emergency communication industry is more and more extensive, logical by carry broadband wireless Letter access system, wireless environment analysis system, system of scouting in the air, is propagandaed directed to communicate and lighting system at mobile data services access system Equipment, provides various types of communication service for emergency communication scene, provides all kinds of the condition of a disasters and place for related command scheduling and administrative department It sets information, provide environment of working at night for emergency communication scene emergency communication disposition.However, weight and the physics rule of above-mentioned equipment Lattice size differs, and to be such as mounted on unmanned aerial vehicle platform, needs for each equipment, using 10-30 days, custom fitting was each other Carry space and tightening platform, to ensure that unmanned plane does not print and distribute safety accident in lifting because of additional increased equipment.This Result in application cost of investment and time cost of the unmanned plane in emergency communication excessively high, and cannot meet in 30 minutes and set out, 1 The quick emergency communication requirements of support of emergency service are opened in hour.
Technical grade multi-rotor unmanned aerial vehicle is without for the proprietary carry platform of all kinds of load designs.There is related extension in such as applying Carrying platform requirement is all often to be customized production according to the physical specification characteristic of specific a certain given load.Customize the period 10-30 days.Major technique the disadvantage is that:
1. customization increases the barrier for promoting and applying technical grade unmanned plane.It is negative that technical grade unmanned plane does not configure lift-off generally The carry platform of load, user will such as be utilized technical grade unmanned plane carry equipment or facility, be taken off based on unmanned plane required on demand Gravity balance needs equipment or facility by unmanned plane and required carry, and unmanned plane genuine is sent to carry out Integrated design and installation, Integrated expense and time cost are higher, and are easy initiation user and the important carry equipment or facility generation that send factory are divulged a secret or lost It loses, the sense of insecurity of damage.
2. the production cycle is relatively long, it is not easy to quickly put into application.Customized production and integrated carry platform, generally require 10-30 days, user can not quickly be come into operation.
3. technical grade unmanned plane is easy by Two-level ensemble wprks structure.User is if you need to need carry to equip according to using Or facility, if being only the theory based on customization, can exist user selection be different from for the first time integrate carry equipment or When facility, second-order correction is carried out to first time integrated platform, structure is more easily damaged to be easy to cause technical grade unmanned plane, draws Send out safety accident.
It is badly in need of solving for disadvantages mentioned above, in industry under the premise of not destroying technical grade unmanned plane original platform mechanism, Manufacture can compatible subscribers difference carry equipment or facility, and convenient for the open carry platform of machine gravity is adjusted flexibly.
Utility model content
In order to overcome industry grade multi-rotor unmanned aerial vehicle of the existing technology not to be directed to all kinds of loads, proprietary carry is designed The deficiency of platform, the utility model provide a kind of open adjustable carry platform applied on unmanned plane.
Technical solution adopted by the utility model to solve its technical problems is:
A kind of open adjustable carry platform applied on unmanned plane, including:Cross-arm and two it is identical and side by side The slide bar of placement;The slide bar and the vertically fixed intersection of the horizontal segment on unmanned aerial vehicle rack top, described slide bar one end is detachably set It is equipped with the cross-arm of the first quantity, the detachable other end of the slide bar is provided with the cross-arm of the second quantity;It is arranged on the cross-arm It is useful for the fixed mounting hole for waiting for carry equipment.
Preferably, the cross-arm and the sliding rail intersect vertically.
Preferably, the cross-arm and the sliding rail are detachably connected by connecting clamping block.
Preferably, including:The slide bar fixes intersection by sliding rail connector and the horizontal segment on unmanned aerial vehicle rack top.
Preferably, more than one mounting hole is provided on the cross-arm, the mounting hole is a word hole.
Preferably, further include:Carry component;The top of the carry component is fixed on by mounting hole on the cross-arm, The lower part of the carry component is fixed and waits for carry equipment.
Preferably, the carry component is suspending assembly, and one end of the suspending assembly is fixed on cross-arm across mounting hole On, the other end of the suspending assembly is tightened against the mounting hole for waiting for carry equipment.
Preferably, the carry component is Quick-dismantle component, and the lower part of the Quick-dismantle component is provided with supporting plate;The Quick Release group The peripheral word hole of cross-arm is inserted on the head of part, is rotated by 90 ° and is fixed on cross-arm, and the supporting plate of the Quick-dismantle component hooks support and waits for that carry is set It is standby.
Preferably, first quantity is identical with the second quantity.
Preferably, first quantity and the second quantity are 2.
The utility model has the beneficial effects that:Cross-arm on the open adjustable carry platform of the utility model and the cunning Rail is detachably connected.When cross-arm and sliding rail are releasing orientation, position of the cross-arm on sliding rail can be moved.When cross-arm and sliding rail For locking state when, the position of cross-arm is fixed, can be with two in this way by after carry hanging equipment is loaded on the cross-arm at slide bar both ends Wait for that the weight of carry equipment adjusts the center of gravity of unmanned plane, unmanned plane is made to balance to move cross-arm in the position of sliding rail in end.
Description of the drawings
The utility model is further illustrated with reference to the accompanying drawings and examples.
Fig. 1 is the schematic flow chart for applying the open adjustable carry platform on unmanned plane of first embodiment.
Fig. 2 is upward view of the open adjustable carry platform application of first embodiment on unmanned plane.
Fig. 3 is the vertical view of the cross-arm of first embodiment.
Fig. 4 carries for the open adjustable carry platform of first embodiment applied on unmanned plane waits carrying the vertical of load Body figure.
Fig. 5 is that the front plan view for needing carrying equipment is carried on the cross-arm of first embodiment.
Fig. 6 is the front plan view of the Quick-dismantle component of second embodiment.
Fig. 7 is that the front plan view for needing carrying equipment is carried on the cross-arm of second embodiment.
Specific implementation mode
The utility model is described in further detail presently in connection with attached drawing.These attached drawings are simplified schematic diagram, Only illustrate the basic structure of the utility model in a schematic way, therefore it only shows composition related with the utility model.
Embodiment 1
Referring to Fig. 1-5, a kind of open adjustable carry platform applied on unmanned plane, including:Cross-arm 2 and two are completely Identical and placed side by side slide bar 1;The vertically fixed intersection of the horizontal segment on 3 top of the slide bar 1 and unmanned aerial vehicle rack, the slide bar 1 one end is detachably provided with the cross-arm 2 of the first quantity, and the other end of the slide bar 1 is detachably provided with the cross-arm of the second quantity 2;It is provided on the cross-arm 2 for the fixed mounting hole 21 for waiting for carry equipment 4.
It should be noted that the cross-arm 2 and slide bar 1 are intensity height and light-weight carbon fiber, it is ensured that do not increase excessive Load, meet requirement of the user to complete machine carry load.
In the present embodiment, the cross-arm 2 and the sliding rail intersect vertically.Closer, the cross-arm 2 and the sliding rail It is detachably connected by connecting clamping block 22.
In the horizontal segment stationary phase that the present embodiment, the slide bar 1 pass through 3 top of sliding rail connector 11 and unmanned aerial vehicle rack It hands over.
More than one mounting hole 21 is provided on the present embodiment, the cross-arm 2, the mounting hole 21 is a word hole.This The outer mounting hole 21 can also be various sizes of hole or strip hole, can be adapted to 21 size of mounting hole of distinct device, realize The requirement of Quick universal.Open adjustable carry platform of this application on unmanned plane has open well.Compatible carry Any equipment or facility of following physical specification size:Long x wide x high(mm):(10-315)x(10-300)x(10-300).It is not required to It is loaded for every sample, carries out the personalized customization of carry platform.
First quantity is identical with the second quantity.In the present embodiment, first quantity and the second quantity are 2. Two cross-arms 2 of the slide bar 1 per one end respectively select four mounting holes 21, connect a carry equipment, form one group moveable group The assembly of zoarium, 1 both ends of slide bar can be adjusted around, and position of centre of gravity before and after unmanned plane is adjusted flexibly in support.
In the present embodiment, further include:Carry component;The top of the carry component is fixed on the cross by mounting hole 21 In load 2, the lower part of the carry component, which is fixed, waits for carry equipment 4.A more progressive ground, the carry component are suspending assembly 51, One end of the suspending assembly 51 passes through mounting hole 21, plugs traverse latch and is fixed on cross-arm 2, the other end of the suspending assembly 51 It is tightened against the mounting hole 21 for waiting for carry equipment 4.Referring to Fig. 5, suspending assembly lower part is fixed by screw in the peace for waiting for carry equipment Hole is filled, is dottle pin layer in the middle part of suspending assembly, a cross-drilled hole is arranged at suspending assembly top, after above wearing the mounting hole of cross-arm, in cross-drilled hole A split pin i.e. suspended is plugged to complete.Split pin is pulled up when dismounting can unload equipment.User is supported to be operated without tool-type;It waits for Carry equipment 4 can horizontal carry on cross bar, also can vertical carry, vertical carry also 0-45 ° of inclined angle-adjustable is specific to participate in figure 4。
Embodiment 2
Referring to Figures 5 and 6, difference lies in the carry component is Quick-dismantle component 52, described fast for embodiment 1 and embodiment 2 The lower part for tearing component 52 open is provided with supporting plate;The peripheral word hole of cross-arm 2 is inserted on the head of the Quick-dismantle component 52, is rotated by 90 ° fixation In on cross-arm 2, the supporting plate of the Quick-dismantle component 52 hooks support and waits for carry equipment 4.
Cross-arm 2 and the sliding rail on the open adjustable carry platform of the utility model are detachably connected.When 2 He of cross-arm When sliding rail is releasing orientation, position of the cross-arm 2 on sliding rail can be moved.When cross-arm 2 and sliding rail are locking state, cross-arm 2 Position fix, in this way by after 4 carry of carry equipment on the cross-arm 2 at 1 both ends of slide bar after, carry equipment 4 can be waited for both ends Weight adjust the center of gravity of unmanned plane to move cross-arm 2 in the position of sliding rail, unmanned plane made to balance.And using using pull fastening type Fastener does not need tool-type installation and fixes, and is particularly suitable for wild environment installation application.
It is enlightenment, through the above description, related work people with the above-mentioned desirable embodiment according to the utility model Member can carry out various changes and amendments in the range of without departing from this item utility model technological thought completely.This item is real It is not limited to the contents of the specification with novel technical scope, it is necessary to which its technology is determined according to right Property range.

Claims (10)

1. a kind of open adjustable carry platform applied on unmanned plane, which is characterized in that including:Cross-arm and two complete phases Same and slide bar placed side by side;
The slide bar and the vertically fixed intersection of the horizontal segment on unmanned aerial vehicle rack top, described slide bar one end is detachably provided with first The cross-arm of quantity, the other end of the slide bar are detachably provided with the cross-arm of the second quantity;It is provided on the cross-arm for solid Surely the mounting hole of carry equipment is waited for.
2. the open adjustable carry platform according to claim 1 applied on unmanned plane, which is characterized in that the cross Load and the slide bar intersect vertically.
3. the open adjustable carry platform according to claim 2 applied on unmanned plane, which is characterized in that the cross Load and the sliding rail are detachably connected by connecting clamping block.
4. the open adjustable carry platform according to claim 1 applied on unmanned plane, which is characterized in that including: The slide bar fixes intersection by sliding rail connector and the horizontal segment on unmanned aerial vehicle rack top.
5. the open adjustable carry platform according to claim 1 applied on unmanned plane, which is characterized in that the cross More than one mounting hole is provided in load, the mounting hole is a word hole.
6. the open adjustable carry platform according to claim 5 applied on unmanned plane, which is characterized in that also wrap It includes:Carry component;
The top of the carry component is fixed on by mounting hole on the cross-arm, and the lower part of the carry component, which is fixed, waits for carry Equipment.
7. the open adjustable carry platform according to claim 6 applied on unmanned plane, which is characterized in that the extension Load component is suspending assembly, and one end of the suspending assembly is fixed on across mounting hole on cross-arm, the suspending assembly it is another End is tightened against the mounting hole for waiting for carry equipment.
8. the open adjustable carry platform according to claim 6 applied on unmanned plane, which is characterized in that the extension Load component is Quick-dismantle component, and the lower part of the Quick-dismantle component is provided with supporting plate;
The peripheral word hole of cross-arm is inserted on the head of the Quick-dismantle component, is rotated by 90 ° and is fixed on cross-arm, the support of the Quick-dismantle component Plate hooks support and waits for carry equipment.
9. the open adjustable carry platform according to claim 1 applied on unmanned plane, which is characterized in that described One quantity is identical with the second quantity.
10. the open adjustable carry platform according to claim 9 applied on unmanned plane, which is characterized in that described First quantity and the second quantity are 2.
CN201820136835.3U 2018-01-26 2018-01-26 A kind of open adjustable carry platform applied on unmanned plane Expired - Fee Related CN207956084U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820136835.3U CN207956084U (en) 2018-01-26 2018-01-26 A kind of open adjustable carry platform applied on unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820136835.3U CN207956084U (en) 2018-01-26 2018-01-26 A kind of open adjustable carry platform applied on unmanned plane

Publications (1)

Publication Number Publication Date
CN207956084U true CN207956084U (en) 2018-10-12

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ID=63735343

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820136835.3U Expired - Fee Related CN207956084U (en) 2018-01-26 2018-01-26 A kind of open adjustable carry platform applied on unmanned plane

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110667867A (en) * 2019-08-30 2020-01-10 南京精微迅智能科技有限公司 Agricultural unmanned aerial vehicle mounting device
CN111288275A (en) * 2018-12-07 2020-06-16 中航贵州飞机有限责任公司 Adjustable aircraft task equipment stores pylon
WO2020253622A1 (en) * 2019-06-18 2020-12-24 深圳高度创新技术有限公司 Fire-fighting and disaster relief unmanned aerial vehicle

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111288275A (en) * 2018-12-07 2020-06-16 中航贵州飞机有限责任公司 Adjustable aircraft task equipment stores pylon
WO2020253622A1 (en) * 2019-06-18 2020-12-24 深圳高度创新技术有限公司 Fire-fighting and disaster relief unmanned aerial vehicle
CN110667867A (en) * 2019-08-30 2020-01-10 南京精微迅智能科技有限公司 Agricultural unmanned aerial vehicle mounting device

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CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20181012

Termination date: 20220126