CN208979105U - A kind of unmanned plane cargo hold handler - Google Patents

A kind of unmanned plane cargo hold handler Download PDF

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Publication number
CN208979105U
CN208979105U CN201821541695.4U CN201821541695U CN208979105U CN 208979105 U CN208979105 U CN 208979105U CN 201821541695 U CN201821541695 U CN 201821541695U CN 208979105 U CN208979105 U CN 208979105U
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CN
China
Prior art keywords
latch
main body
cargo hold
unmanned plane
lock chamber
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
CN201821541695.4U
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Chinese (zh)
Inventor
张志明
杨杰
李蓉
梁凯
王丽丽
陈秋露
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Guangdong University of Technology
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Guangdong University of Technology
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Priority to CN201821541695.4U priority Critical patent/CN208979105U/en
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Publication of CN208979105U publication Critical patent/CN208979105U/en
Expired - Fee Related legal-status Critical Current
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Abstract

The utility model provides a kind of unmanned plane cargo hold handler.A kind of unmanned plane cargo hold handler, wherein including the first latch being located on unmanned plane and the second latch being located on cargo hold, first latch can cooperate with second latch, and unmanned plane is made to link together with cargo hold;First latch includes the first fixed plate and the first locking block main body in first fixed plate, second latch includes the second fixed plate and the second locking block main body in second fixed plate, the second locking block main body is equipped with the second lock chamber for matching with the first locking block main body, and the first locking block main body is equipped with for by pop-up/position-limit mechanism of first latch and the second latch locking.The utility model is able to solve prior art middle hold and is loaded and unloaded in the horizontal plane, and sliding slot gap is small in sliding rail length, sliding rail flexible type, sliding rail leads to problems such as the cargo hold efficiency of loading and unloading low.

Description

A kind of unmanned plane cargo hold handler
Technical field
The utility model relates to unmanned plane logistics and transportation technical fields, load and unload more particularly, to a kind of unmanned plane cargo hold Device.
Background technique
Application No. is CN106114866.A, the Chinese utility model patent of the entitled unmanned plane cargo hold of patent provides one kind Unmanned plane cargo hold, the unmanned plane cargo hold include: one group of first connecting plate being parallel to each other and one group of second connection being parallel to each other Plate, the second bottom won in succession described in the first connecting plate described in one group and one group are closed by bottom plate, adjacent first connecting plate It is connected in corner by column with second connecting plate;At least one described first connecting plate is in the turning position at one The first latch is installed, the top of the latch is equipped with the second latch, and second latch may be provided at unmanned plane On the sliding rail of ontology, the unmanned plane cargo hold can move horizontally along the sliding rail and pass through first latch and described second Latch locking.The above-mentioned prior art is to achieve the purpose that quick despatch and self-locking, uses unmanned plane sliding rail and the first locking The cooperation of block, is loaded and unloaded, and is cooperated using the first latch and the second latch, is carried out self-locking.
In the above prior art, when cargo hold loads, unmanned plane needs to be supported on ground, has support frame, due to support The height limitation of frame, the design length, width and height of cargo hold, the size of length and width is greater than high size, and the prior art is using horizontal sliding Rail, so the length of device sliding rail is longer, for cargo hold in the process of handling, the required time is long, and the cargo hold efficiency of loading and unloading is low.The dress of cargo hold It carries and unloading, the first latch needs moves on the slide rail, cargo hold is mobile, i.e. gravity motion, and the first latch may be made to cunning The pressure of rail is concentrated on one point, along with access times are frequent, sliding rail may be promoted to be deformed, to influence the dress of cargo hold Unload efficiency.Sliding rail sliding slot is matched with the first latch, due to on vertical direction, limit to the first latch, sliding slot The size that gap should be adapted with the thickness of the first latch, since the size of sliding slot and the first latch is adapted, so making It is not easy to be aligned with sliding rail at the first latch, to cause efficiency of loading low.
Summary of the invention
The utility model in order to overcome at least one of the drawbacks of the prior art described above, provides a kind of unmanned plane cargo hold handling Device.The utility model is able to solve prior art middle hold and is loaded and unloaded in the horizontal plane, sliding rail length, sliding rail flexible type, cunning Sliding slot gap is small in rail leads to problems such as the cargo hold efficiency of loading and unloading low.
In order to solve the above technical problems, the technical solution adopted in the utility model is: a kind of unmanned plane cargo hold handler, Wherein, including the first latch being located on unmanned plane and the second latch being located on cargo hold, first latch can It cooperates with second latch, unmanned plane is made to link together with cargo hold;First latch includes first fixed Plate and the first locking block main body in first fixed plate, second latch is including the second fixed plate and is set to institute The second locking block main body in the second fixed plate is stated, the second locking block main body is equipped with and the first locking block main body phase Second lock chamber of cooperation, the first locking block main body is equipped with locks for realizing first latch and the second latch Only and unlock pop-up/position-limit mechanism.
Further, the pop-up/position-limit mechanism includes the button bit being located in the first latch main body wall, and It is located at the flip-over type fastening structure matched on the second locking cavity wall with the button bit;It is of course also possible to set in turn It sets, i.e., button bit is arranged on the second locking cavity wall, and flip-over type fastening structure is arranged in the first latch main body side On wall.The flip-over type fastening structure can clasp the button bit when the first locking block main body once presses down on and realize First latch and the second latch locking, can unclamp the button bit when the first locking block main body presses down on again Realize the first latch and the unlock of the second latch.
Further, the first locking block main body is equipped with the first lock chamber, is equipped with first in first lock chamber Spring, first spring one end connect the first lock chamber bottom wall, are connected with nested block, the nested block energy on the other end Pop-up/retraction first lock chamber under the mating reaction of external force and the first spring.The size of nested block is less than the first locking The size of block main body, when being aligned with the second latch, nested block is easier to be aligned with the second lock chamber, nested block After the contraposition of the second lock chamber, nested block can play guiding function to the first latch and the contraposition of the second lock chamber, make first Latch is easier to be aligned with the second lock chamber, nested after the first latch with the second lock chamber completely into being locked up Block can be retracted first lock chamber, not take up space.
In the utility model, pop-up/position-limit mechanism working principle is as follows: embedding on the first latch when original state Set block is ejected into outside the first lock chamber, first sharp when the first latch needs are cooperatively connected simultaneously locking with the second latch The first locking block main body and the second lock chamber are aligned with nested block, then pressed along the vertical direction of second latch First latch, the first locking block main body enters the second lock chamber, while first latch moves down compression institute Nested block is stated, so that nested block is retracted into the first lock chamber, while button bit and the second lock in the first latch main body wall Only the flip-over type fastening structure on cavity wall matches, and flip-over type fastening structure clasps the button bit and realizes the first latch and the Two latch lockings.When the first latch and the second latch that cooperate together need to unlock, along second lock The vertical direction of stops presses first latch again, then unclamps, pressing force disappear when, flip-over type fastening structure with The button bit unclamps, and realizes the first latch and the unlock of the second latch, and by described the under the collective effect of the first spring One latch pops up.Certainly, pop-up/position-limit mechanism is a kind of device with flip-over type fastening structure, which, which has, faces When locked and interim pop-up function, such as SD card slot, push type ball pen etc..Therefore, pop-up/position-limit mechanism specific implementation side Formula and this more than above-mentioned one kind, as long as it can be carried out locking by self structure, popped up to change position of the first latch State.
Further, nested block one end opposite with first spring is equipped with the first guiding surface.Described first One end of locking block main body and second lock chamber cooperation is equipped with the second guiding surface, and the opening of second lock chamber is set There is third guiding surface.The effect of third guiding surface is that the original opening made becomes larger and for inclined-plane, be more convenient for nested block and the One locking block main body is aligned with the second lock chamber, can be to the first locking block main body and nested block and due to being inclined-plane Guiding function is played in the contraposition of two lock chambers.First guiding surface and the second guiding surface make the end and first of nested block respectively Latch main body end is opposite respectively to be reduced with nested block main part and the first latch main part bottom end, is convenient for and second Lock chamber contraposition, along with being inclined-plane, contacts with third guiding surface, can be to the first locking block main body and the second lock chamber pair Play good guiding function in position.
Further, first latch is fixed on unmanned machine bottom board or described first by the first fixed plate Latch and the unmanned machine bottom board integrated design.Second latch is fixed on cargo hold by the second fixed plate, or Second latch described in person and the cargo hold integrated design.
The overall work principle of the utility model are as follows: the first step, the first latch are aligned with the second latch: first Nested block is popped up from the first lock chamber, aligns nested block and the first locking block main body with the second latch, Enter nested block and the first locking block main body in the second lock chamber.
Second step, the first latch and the second latch carry out locking: manpower promotes unmanned aerial vehicle body to be pressed downward, the first lock Stops and the second latch locking under the action of pop-up/position-limit mechanism;
Third step, the first latch are unlocked with the second latch: unmanned plane carries cargo hold and reaches specified place, goods Cabin is unloaded, and manpower promotes unmanned aerial vehicle body to be pressed downward, and the first latch and the second latch are in pop-up/position-limit mechanism work With lower unlock.
Compared with prior art, the utility model has the beneficial effects that
For the utility model using unmanned plane and the handling of cargo hold in the vertical direction, the mobile path of the first latch is short, Time required for mobile is short;Using unmanned plane and the handling of cargo hold in the vertical direction, will not occur to generate pressure to sliding rail Effect, promote sliding rail to be deformed, thus the problem of influencing the efficiency of loading and unloading of cargo hold;First latch and the second latch pair Position, the end of the opening of the second lock chamber, the end of the first locking block main body and nested block are equipped with guiding surface, so that The openings of sizes of second lock chamber is greater than the size of the first latch body width, consequently facilitating contraposition, and guiding can be played Effect;Pop-up/position-limit mechanism is provided on first latch, after the first latch and the contraposition of the second latch cooperate, pop-up/limit Position mechanism can lock the first latch and the second latch, so that unmanned plane and cargo hold lock securely, securely and reliably after loading.
Detailed description of the invention
Fig. 1 is the first latch of the utility model and the second latch connect with unmanned plane and cargo hold after structural schematic diagram;
Fig. 2 is the longitudinal profile schematic diagram after the first latch of the utility model and the second latch cooperation locking;
Fig. 3 is the longitudinal profile schematic diagram after the first latch of the utility model and the unlock of the second latch;
Fig. 4 is the structural schematic diagram of the first latch of the utility model;
Fig. 5 is the structural schematic diagram of the second latch of the utility model.
Specific embodiment
The attached figures are only used for illustrative purposes and cannot be understood as limitating the patent;In order to better illustrate this embodiment, attached Scheme certain components to have omission, zoom in or out, does not represent the size of actual product;To those skilled in the art, The omitting of some known structures and their instructions in the attached drawings are understandable.Being given for example only property of positional relationship is described in attached drawing Illustrate, should not be understood as the limitation to this patent.
As shown in Fig. 1 to Fig. 5, a kind of unmanned plane cargo hold handler, wherein including the first locking being located on unmanned plane Block 1 and the second latch 2 being located on cargo hold 6, first latch 1 can cooperate with second latch 2, make Unmanned plane links together with cargo hold 6;First latch 1 is including the first fixed plate 11 and is set to first fixed plate 11 On the first locking block main body 12, second latch 2 include the second fixed plate 21 and be set to second fixed plate 21 on The second locking block main body 22, the second locking block main body 22 is equipped with the matched with the first locking block main body 12 Two lock chambers 221, the first locking block main body 12, which is equipped with, to be used for 2 locking of first latch 1 and the second latch Pop-up/position-limit mechanism.
In the present embodiment, the pop-up/position-limit mechanism includes the button bit being located on 12 side wall of the first locking block main body, And it is located at the flip-over type fastening structure matched on 221 inner wall of the second lock chamber with the button bit.The flip-over type button It closes structure and can clasp the button bit when the first locking block main body 12 once presses down on and realize the first latch 1 and the Two latch, 2 locking can unclamp the button bit when the first locking block main body 12 presses down on again and realize the first lock Stops 1 and the unlock of the second latch 2.
As shown in Fig. 1 to Fig. 5, the first locking block main body 12 is equipped with the first lock chamber 121, first lock chamber The first spring 3 is equipped in 121, described first spring, 3 one end connects 121 bottom wall of the first lock chamber, is connected on the other end Nested block 4, the nested block 4 can under the mating reaction of external force and the first spring 3 pop-up/retraction first lock chamber 121. The size of nested block 4 is less than the size of the first locking block main body 12, and when being aligned with the second latch 2, nested block 4 is easier to Aligned in the second lock chamber 221, after nested block 4 and the contraposition of the second lock chamber 221, nested block 4 to the first latch 1 with The contraposition of second lock chamber 221 can play guiding function, and the first latch 1 is made to be easier to be aligned with the second lock chamber 221, After first latch 1 with the second lock chamber 221 completely into being locked up, nested block 4 can be retracted first lock chamber 121, It does not take up space.
In the present embodiment, pop-up/position-limit mechanism working principle is as follows: nesting when original state, on the first latch 1 Block 4 is ejected into outside the first lock chamber 121, when the first latch 1 needs to be cooperatively connected simultaneously locking with the second latch 2, First locking block main body 12 and the second lock chamber 221 are aligned first with nested block 4, then along second latch 2 Vertical direction presses first latch 1, and the first locking block main body 12 enters the second lock chamber 221, while first lock Stops 1 moves down the compression nested block 4, so that nested block 4 is retracted into the first lock chamber 121, while the first latch Button bit on 12 side wall of main body is matched with the flip-over type fastening structure on 221 inner wall of the second lock chamber, flip-over type fastening structure It clasps the button bit and realizes the first latch 1 and 2 locking of the second latch.When the first latch 1 to cooperate together with When second latch 2 needs to unlock, first latch 1 is pressed again along the vertical direction of second latch 2, then It unclamps, when pressing force disappears, flip-over type fastening structure and the button bit unclamp, and realize the first latch 1 and the second latch 2 Unlock, and pop up first latch 1 under the collective effect of the first spring 3.Certainly, pop-up/position-limit mechanism is A kind of device with flip-over type fastening structure, the structure have interim locked and interim pop-up function, such as SD card slot, push type Ball pen etc..Therefore, pop-up/position-limit mechanism specific implementation and this more than above-mentioned one kind, as long as it can pass through itself Structure carries out locking, pops up to change the location status of the first latch.
As shown in Fig. 1 to Fig. 5, the nested block 4 one end opposite with first spring 3 is equipped with the first guiding surface 41.One end of the first locking block main body 12 and second lock chamber 221 cooperation is equipped with the second guiding surface 122, described The opening of second lock chamber 221 is equipped with third guiding surface 222.The effect of third guiding surface 222 is the original opening made Become larger and for inclined-plane, is more convenient for nested block 4 and the first locking block main body 12 is aligned with the second lock chamber 221, due to being oblique Face can play guiding function to the first locking block main body 12 and nested block 4 and the contraposition of the second lock chamber 221.First guiding is oblique Face 41 and the second guiding surface 122 make respectively nested block 4 end and 12 end of the first locking block main body respectively it is opposite with it is embedding It covers 4 main part of block and 12 member base end of the first locking block main body to reduce, convenient for aligning with the second lock chamber 221, along with being Inclined-plane is contacted with third guiding surface 222, can be played very well to the first locking block main body 12 and the contraposition of the second lock chamber 221 Guiding function.
In the present embodiment, first latch 1 is fixed on unmanned machine bottom board 5 by the first fixed plate 11, Huo Zhesuo State the first latch 1 and unmanned 5 integrated design of machine bottom board.Second latch 2 is fixed by the second fixed plate 21 On cargo hold 6 or second latch 2 and 6 integrated design of cargo hold.
The overall work principle of the present embodiment are as follows: the first step, the first latch 1 are aligned with the second latch 2: first Nested block 4 is popped up from the first lock chamber 121, then make nested block 4 and the first locking block main body 12 and the second latch 2 into Row contraposition, then enter nested block 4 and the first locking block main body 12 in second lock chamber 221.
Second step, the first latch 1 and the second latch 2 carry out locking: manpower promotes unmanned aerial vehicle body to be pressed downward, and first Latch 1 and the second latch 2 locking under the action of pop-up/position-limit mechanism;
Third step, the first latch 1 are unlocked with the second latch 2: unmanned plane carries cargo hold 6 and reaches specified ground Point, cargo hold 6 are unloaded, and manpower promotes unmanned aerial vehicle body to be pressed downward, and the first latch 1 and the second latch 2 are in pop-up/limit It is unlocked under the action of mechanism.
Obviously, the above embodiments of the present invention is used for the purpose of clearly demonstrating examples for clearly illustrating the present invention, And it is not limitations of the embodiments of the present invention.For those of ordinary skill in the art, it is stated upper It can also be made other variations or changes in different ways on the basis of bright.There is no need and unable to give all embodiments With exhaustion.Any modifications, equivalent replacements, and improvements made within the spirit and principle of the present invention etc. should all include Within the protection scope of the utility model claims.

Claims (7)

1. a kind of unmanned plane cargo hold handler, which is characterized in that including the first latch (1) being located on unmanned plane and be located at The second latch (2) on cargo hold (6), first latch (1) can cooperate with second latch (2), make Unmanned plane links together with cargo hold (6);First latch (1) includes the first fixed plate (11) and consolidates set on described first The first locking block main body (12) on fixed board (11), second latch (2) include the second fixed plate (21) and are set to described The second locking block main body (22) in second fixed plate (21), the second locking block main body (22) are equipped with and first lock The second lock chamber (221) that stops main body (12) matches, the first locking block main body (12) and the second lock chamber (221) it Between be equipped with for realizing first latch (1) and the second latch (2) locking and unlock pop-up/position-limit mechanism.
2. a kind of unmanned plane cargo hold handler according to claim 1, which is characterized in that the pop-up/position-limit mechanism Including the button bit being located on the first locking block main body (12) side wall, and it is located on the second lock chamber (221) inner wall The flip-over type fastening structure matched with the button bit, the flip-over type fastening structure is in the first locking block main body (12) one The button bit can be clasped when secondary downward push and realizes the first latch (1) and the second latch (2) locking, in first lock Stops main body (12) can unclamp the button bit and realize the first latch (1) and the second latch (2) solution when pressing down on again Lock.
3. a kind of unmanned plane cargo hold handler according to claim 1, which is characterized in that the first locking block main body (12) the first lock chamber (121) are equipped with, are equipped with the first spring (3) in first lock chamber (121), first spring (3) one end connects the first lock chamber (121) bottom wall, is connected with nested block (4) on the other end, and the nested block (4) can be Pop-up/retraction first lock chamber (121) under the mating reaction of external force and the first spring (3).
4. a kind of unmanned plane cargo hold handler according to claim 3, which is characterized in that the nested block (4) and institute The opposite one end of the first spring (3) is stated equipped with the first guiding surface (41).
5. a kind of unmanned plane cargo hold handler according to claim 1, which is characterized in that the first locking block main body (12) one end with second lock chamber (221) cooperation is equipped with the second guiding surface (122), second lock chamber (221) Opening be equipped with third guiding surface (222).
6. a kind of unmanned plane cargo hold handler according to claim 1, which is characterized in that first latch (1) It is fixed on unmanned machine bottom board (5) by the first fixed plate (11) or first latch (1) and the unmanned machine bottom board (5) integrated design.
7. a kind of unmanned plane cargo hold handler according to claim 1, which is characterized in that second latch (2) It is fixed on cargo hold (6) by the second fixed plate (21) or second latch (2) is integrated with the cargo hold (6) sets Meter.
CN201821541695.4U 2018-09-20 2018-09-20 A kind of unmanned plane cargo hold handler Expired - Fee Related CN208979105U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821541695.4U CN208979105U (en) 2018-09-20 2018-09-20 A kind of unmanned plane cargo hold handler

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821541695.4U CN208979105U (en) 2018-09-20 2018-09-20 A kind of unmanned plane cargo hold handler

Publications (1)

Publication Number Publication Date
CN208979105U true CN208979105U (en) 2019-06-14

Family

ID=66784924

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821541695.4U Expired - Fee Related CN208979105U (en) 2018-09-20 2018-09-20 A kind of unmanned plane cargo hold handler

Country Status (1)

Country Link
CN (1) CN208979105U (en)

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

Granted publication date: 20190614

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