CN209617524U - A kind of unmanned machine head quick-disassembly structure - Google Patents

A kind of unmanned machine head quick-disassembly structure Download PDF

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Publication number
CN209617524U
CN209617524U CN201821887692.6U CN201821887692U CN209617524U CN 209617524 U CN209617524 U CN 209617524U CN 201821887692 U CN201821887692 U CN 201821887692U CN 209617524 U CN209617524 U CN 209617524U
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CN
China
Prior art keywords
threaded hole
sliding block
dovetail groove
machine head
disassembly structure
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CN201821887692.6U
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Chinese (zh)
Inventor
付万龙
周腾俊
杜健
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Nanjing Xian Aircraft Robot Technology Co Ltd
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Nanjing Xian Aircraft Robot Technology Co Ltd
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Priority to CN201821887692.6U priority Critical patent/CN209617524U/en
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Abstract

The utility model belongs to unmanned plane field.The utility model provides a kind of unmanned machine head quick-disassembly structure, including unmanned plane fixing end and holder plate end, aircraft fixing end and holder plate end match, upper hanging plate two sides are respectively provided with dovetail groove, the distance between dovetail groove is greater than the width of lower plugboard in holder plate end, lower plugboard is inserted into after dovetail groove and the lower end in contact of dovetail groove, a movable sliding block is equipped on the outside of the dovetail groove of lock tongue upper hanging plate wherein side, there is sliding block lid package on the outside of sliding block, sliding block lid is fixed on upper hanging plate, the first threaded hole is equipped with inside sliding block lid, screw rod is equipped in first threaded hole, screw rod and shoe contact, screw rod is directly connect with lock handle.Unmanned machine head quick-disassembly structure provided by the utility model realizes holder Fast Installation and disassembly, and safety is good, convenient to use.Fast by speed, not easy to make mistakes, fixed tight prioritization scheme, it is time-consuming and laborious to solve the problems, such as that user of service installs.

Description

A kind of unmanned machine head quick-disassembly structure
Technical field
The utility model belongs to unmanned plane field, is related to a kind of unmanned machine head quick-disassembly structure.
Background technique
In unmanned plane application process, it is often necessary to carry task device, to realize aerial task, such as high-definition camera Head, megaphone, searchlight.In the prior art, the connection type of task device and unmanned plane is carried out mostly with screw and carbon plate It assembles, needs tool to assist in assembling process, process is cumbersome laborious.And during unmanned plane execution task, it is often necessary to tear open Equipment is unloaded, and is had high requirements to the fastness of installation.The prior art is difficult to meet these demands.
Summary of the invention
1, technical problem to be solved:
The holder of existing unmanned plane assembles and needs tool to assist on dismantling, and process is cumbersome laborious.
2, technical solution:
In order to solve problem above, the utility model provides a kind of unmanned machine head quick-disassembly structure, including unmanned plane is consolidated Fixed end and holder plate end, the unmanned plane fixing end and holder plate end match, and unmanned plane fixing end includes upper hanging plate, The upper hanging plate two sides are respectively provided with dovetail groove, and the distance between described dovetail groove is greater than the width of lower plugboard in holder plate end Degree, the lower plugboard is inserted into after dovetail groove and the lower end in contact of the dovetail groove, the swallow of lock tongue upper hanging plate wherein side It is equipped with a movable sliding block on the outside of stern notch, there is sliding block lid package on the outside of the sliding block, the sliding block lid is fixed on upper hanging plate On, the first threaded hole is equipped with inside the described sliding block lid, is equipped with screw rod in first threaded hole, the screw rod and The shoe contact, the screw rod are directly connect with lock handle.
The outer rim of the dovetail groove is equipped with bevel edge.
The lower plugboard outer rim is equipped with chamfering and bevel edge matches.
The second threaded hole and third threaded hole, second threaded hole, third threaded hole, first are additionally provided in sliding block lid Threaded hole is located at same height, and the second threaded hole, third threaded hole are symmetrical relative to the first threaded hole, and described second A spring is both provided in threaded hole and third threaded hole, spring fixed screw passes through spring and fixation, the spring and institute The shoe contact stated, as screw rod moves inward, the spring is compressed.
The rear end of the lower plugboard is equipped with inverse plugging step.
3, the utility model has the advantages that
Unmanned machine head quick-disassembly structure provided by the utility model realizes holder Fast Installation and disassembly, and safety is good, makes With convenient and efficient.Fast by speed, not easy to make mistakes, fixed tight prioritization scheme, solves user of service and installs time-consuming and laborious ask Topic.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model.
Fig. 2 is the structural schematic diagram of unmanned plane fixing end.
Fig. 3 is the structural schematic diagram at holder plate end.
Fig. 4 is the top view after the utility model assembly.
Fig. 5 is the sectional view along A-A of top view after assembly.
Fig. 6 is the B-B direction cross-sectional view of top view after assembly
Specific embodiment
The utility model is described in detail with reference to the accompanying drawing.
As shown in Fig. 2, unmanned plane fixing end includes upper hanging plate 1, sliding block lid 2, sliding block lid screw 3, the fixed spiral shell of lock handle Silk 4, lock handle 5, spring fixed screw 6, sliding block 10, sliding block screw rod 11, spring 12.
As shown in figure 3, holder plate end includes holder mounting base 7, lower plugboard 8, lower plugboard fixed screw 9.
As shown in Figure 1, unmanned plane fixing end is fixed in the installation site of unmanned plane.Holder plate end can connect nothing Man-machine task holder.1 two sides of upper hanging plate are respectively provided with dovetail groove, and connection type is that lower plugboard 8 is inserted into dovetail groove. The distance between described dovetail groove is greater than the width of lower plugboard 8 in holder plate end, so that plate is smooth when being inserted into not to have resistance, The lower plugboard 8 is inserted into after dovetail groove and the lower end in contact of the dovetail groove, after guaranteeing insertion, lower plugboard and upper hanging plate Inclined-plane contact with each other load, will not fall off.
As shown in Figure 4 and Figure 5, it in order to can be fastened while guaranteeing plate smooth insertion again, is set in the side of dovetail groove Movable sliding block 10 is set.Have on the outside of sliding block 10 sliding block lid 2 package, ensure that sliding block 10 can be moved in sliding block lid 2 without It falls off.There is the first threaded hole inside the sliding block lid 2 being fixed on upper hanging plate 1, the movement of sliding block 10 in the first threaded hole by transporting Dynamic screw rod 11 pushes.And screw rod 11 is directly connected with lock handle 5.When assembly, can directly it be adjusted according to locking force The position of whole good lock handle 5, and it is fixed by lock handle fixed screw 4, so that can complete to clamp in a semi-circumference With loosen.In this way, then screwing unmanned plane and fixing in use, only unmanned plane fixing end need to be inserted into along dovetail groove in holder plate end Installation can be completed in the handle that screws at end.Rotation angle is semi-circumference.
As shown in fig. 6, the second threaded hole and third threaded hole are additionally provided in sliding block lid, second threaded hole, third Threaded hole, the first threaded hole are located at same height, and the second threaded hole, third threaded hole are relative to the first threaded hole pair Claim, a spring 12 is both provided in second threaded hole and third threaded hole, spring fixed screw 6 passes through spring 12 and divides It is not fixed in the second threaded hole and third threaded hole, the spring 12 and the sliding block 10 contact, with screw rod 11 It moves inward, the spring 12 is compressed, and after assembly, spring 12 is in compressive state, can provide bullet when sliding block backhaul Power avoids rubbing so that sliding block 10 may be located remotely from lower plugboard 8 when 11 backhaul of screw rod, so that lower plugboard 8 is smoothly extracted.
Holder mounting base 7 can connect different task tripod head equipments.There are chamfering in the front end two sides of lower plugboard 8, it is ensured that It is smoothly inserted into the case where being inconvenient to observe.The rear end of lower plugboard is equipped with inverse plugging step 13, can influence to make to avoid anti-plug With.
Unmanned machine head quick-disassembly structure provided by the utility model is inserted into nothing when in use, by the lower plugboard 8 with holder In the dovetail groove of man-machine fixing end, it can be inserted on earth along sliding rail.After on earth, quick-detachment locking handle 5 is screwed on earth, it can be complete At assembling process.After the completion of use, quick-detachment locking handle 5 is reversely rotated, tripod head equipment can be extracted, completes disassembly.
Although the utility model has been described by way of example and in terms of the preferred embodiments, they are not for limiting the utility model , it is any to be familiar with this those skilled in the art, in the spirit and scope for not departing from the utility model, it can make various changes or retouch from working as, Therefore the protection scope of the utility model should be subject to what claims hereof protection scope was defined.

Claims (6)

1. a kind of unmanned machine head quick-disassembly structure, including unmanned plane fixing end and holder plate end, the unmanned plane fixing end It is matched with holder plate end, it is characterised in that: unmanned plane fixing end includes upper hanging plate (1), and the upper hanging plate (1) two sides are each Equipped with dovetail groove, the distance between described dovetail groove is greater than the width of lower plugboard (8) in holder plate end, the lower plugboard (8) it is inserted into after dovetail groove and the lower end in contact of the dovetail groove, lock tongue upper hanging plate (1) is wherein set on the outside of the dovetail groove of side There is a movable sliding block (10), there is sliding block lid (2) package on the outside of the sliding block (10), the sliding block lid (2) is fixed on On hanging plate (1), it is equipped with the first threaded hole inside the sliding block lid (2), is equipped with screw rod (11) in first threaded hole, The screw rod (11) and the sliding block (10) contact, the screw rod (11) are directly connect with lock handle (5).
2. unmanned machine head quick-disassembly structure as described in claim 1, it is characterised in that: the outer rim of the dovetail groove is equipped with oblique Side.
3. unmanned machine head quick-disassembly structure as described in claim 1, it is characterised in that: described lower plugboard (8) front end is equipped with Chamfering.
4. the unmanned machine head quick-disassembly structure as described in claims 1 or 2 or 3, it is characterised in that: be additionally provided in sliding block lid (2) Second threaded hole and third threaded hole, second threaded hole, third threaded hole, the first threaded hole are located at same height, And the second threaded hole, third threaded hole are symmetrical relative to the first threaded hole, in second threaded hole and third threaded hole It is both provided with a spring (12), spring fixed screw (6) passes through spring (12) and fixed, the spring (12) and the cunning Block (10) contact, as screw rod (11) moves inward, the spring (12) is compressed.
5. the unmanned machine head quick-disassembly structure as described in claims 1 or 2 or 3, it is characterised in that: after the lower plugboard (8) End is equipped with inverse plugging step (13).
6. unmanned machine head quick-disassembly structure as claimed in claim 4, it is characterised in that: the rear end of the lower plugboard (8) is equipped with Inverse plugging step (13).
CN201821887692.6U 2018-11-16 2018-11-16 A kind of unmanned machine head quick-disassembly structure Active CN209617524U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821887692.6U CN209617524U (en) 2018-11-16 2018-11-16 A kind of unmanned machine head quick-disassembly structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821887692.6U CN209617524U (en) 2018-11-16 2018-11-16 A kind of unmanned machine head quick-disassembly structure

Publications (1)

Publication Number Publication Date
CN209617524U true CN209617524U (en) 2019-11-12

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Application Number Title Priority Date Filing Date
CN201821887692.6U Active CN209617524U (en) 2018-11-16 2018-11-16 A kind of unmanned machine head quick-disassembly structure

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114572409A (en) * 2022-05-07 2022-06-03 北京卓翼智能科技有限公司 A installation device and unmanned aerial vehicle for unmanned aerial vehicle load

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114572409A (en) * 2022-05-07 2022-06-03 北京卓翼智能科技有限公司 A installation device and unmanned aerial vehicle for unmanned aerial vehicle load
CN114572409B (en) * 2022-05-07 2022-07-29 北京卓翼智能科技有限公司 A installation device and unmanned aerial vehicle for unmanned aerial vehicle load

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