CN208021754U - A kind of unmanned plane delivery device - Google Patents
A kind of unmanned plane delivery device Download PDFInfo
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- CN208021754U CN208021754U CN201820390498.0U CN201820390498U CN208021754U CN 208021754 U CN208021754 U CN 208021754U CN 201820390498 U CN201820390498 U CN 201820390498U CN 208021754 U CN208021754 U CN 208021754U
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- card slot
- unmanned plane
- rope body
- balance weight
- release device
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Abstract
The utility model is related to a kind of unmanned plane delivery devices, including release device, rope body, balance weight mechanism and remote controler, release device is set on the downside of unmanned plane, it is internally provided with ring electromagnet, rope body one end is equipped with the adsorption piece being connect with ring electromagnet magnetism, other end connection needs to be thrown goods and materials, rope body is divided to two sections, it is connected by connector, connector includes connected first, second card slot, first card slot is arranged close to release device, the width of first card slot is more than the second card slot, balance weight mechanism outer surface is equipped with protrusion, ledge width is more than the width of the second card slot, and less than the width of the first card slot, after balance weight mechanism passes through the first card slot by protrusion, sliding is set in the second card slot, the distance between balance weight mechanism and release device are less than release altitude, remote controler respectively with unmanned plane, release device control connection.The utility model product can automatically disengage, and meet and launched to electrification article.
Description
Technical field
The utility model is related to a kind of technical field of unmanned plane more particularly to a kind of unmanned plane delivery devices.
Background technology
With the continuous maturation of unmanned air vehicle technique, it can quickly be gone up to the air, hovering and can be carried certain negative according to unmanned plane
The regional air-dropped material of the characteristics of load, the arrival that can be used for earthward having inconvenient traffic generally require to realize air-drop at nobody
Setting is for carrying the plug-in delivery device for launching goods and materials on machine, and in unmanned plane row to specified delivery point, goods and materials to be put are de-
From plug-in delivery device, complete to launch.
In the prior art, for unmanned plane when launching, goods and materials to be put generally can directly completely disengage unmanned plane, make in gravity
With lower rapid landing, it is damaged when contacting ground since the impact force of ground generation is very easy, especially for object to be put
Occasion heavier, that dispensing ground is harder is provided, it is possible that the case where thoroughly damaging goods and materials.In addition, existing unmanned plane is launched
There is also can not launch electrification article to device.
Utility model content
Technical problem to be solved in the utility model is how to provide a kind of dispensing goods and materials, realization can be facilitated to automatically disengage
Unmanned plane delivery device, and can meet to charge article dispensing, greatly improve working efficiency and reduce labor intensity, avoid
It is artificial to carry out hazardous environment operation.
The technical solution that the utility model solves above-mentioned technical problem is as follows：
A kind of unmanned plane delivery device, including release device, rope body, balance weight mechanism and remote controler, the release dress
It sets and is fixed on the downside of unmanned aerial vehicle body, and be internally provided with ring electromagnet, described rope body one end is equipped with adsorption piece, described
The outer diameter of adsorption piece is connect with the internal diameter of ring electromagnet matching magnetism, and the other end connection of the rope body needs to be thrown
Goods and materials, the rope body are therefrom partly two sections, and two sections of rope bodies are connected by connector, inside the connector
It is hollow, and outside is equipped with and is connected with inside the first card slot and the second card slot, first card slot and second card slot one end
It is connected, first card slot is arranged close to the release device, and second card slot is located at first card slot to be released far from described
The side of device is put, and the width of first card slot is more than the width of second card slot, the balance weight mechanism outer surface is set
There are protrusion, the width of the protrusion to be more than the width of second card slot, and less than the width of first card slot, the counterweight
Mechanism by it is described protrusion pass through first card slot after, sliding be set to second card slot in, and the balance weight mechanism with
The distance between described release device is less than release altitude, and the remote controler connects with unmanned plane, release device control respectively
It connects.
Compared with prior art, the utility model has the beneficial effects that：The utility model product passes through rope body both ends
It is separately connected release device and goods and materials to be put, release device is arranged on unmanned plane, and counter weight machine is provided on rope body
Structure, balance weight mechanism pass through the first card slot on connector particular by protrusion, are then slid into the second card slot and position, due to
The width of protrusion is more than the width of the second card slot, and therefore, balance weight mechanism will not be pulled out out of second card slot.It should be noted that
Winding is set in release device in the middle part of one section of rope body above balance weight mechanism, between balance weight mechanism and release device
Distance is less than release altitude, and specifically, the distance between balance weight mechanism and goods and materials to be thrown can be 2m to 3m, can thus make
Release device is obtained when discharging rope body, goods and materials to be put can first be fallen, and balance weight mechanism is now in the air, is waited for
It launches after goods and materials land without departing from rope body, under the gravity of balance weight mechanism, the adsorption piece of rope body one end is just
It can be detached from out of release device ring electromagnet, complete the dispensing of goods and materials, do not interfere with the normal flight of unmanned plane.In addition,
Very easily unmanned plane and release device can be manipulated by remote controler, realize across high-altitude and launch messenger operation.This
Utility model unmanned plane delivery device can facilitate dispensing goods and materials, realization to automatically disengage, and can meet the dispensing to charging article, greatly
It is big to improve working efficiency and reduce labor intensity, it avoids manually carrying out hazardous environment operation.
Based on the above technical solution, the utility model can also do following improvement：
Further, the shape of second card slot is in strip, and is arranged along the length direction of the rope body, institute
It states rope body inner wall and corresponds to the position of second card slot and be equipped at intervals with multiple fixed parts along its length, set in the protrusion
There is the mounting portion with the fixed part Matching installation.
Advantageous effect using above-mentioned further scheme is：It can very easily realize that the installation for adjusting balance weight mechanism is high
Degree meets different release altitude requirements.
Further, the fixed part is the fixed seat inlayed on the rope body inner wall, is equipped in the fixed seat
Internal thread, the mounting portion outer surface are equipped with external screw thread, and the mounting portion is threadedly coupled with the fixed seat.
Advantageous effect using above-mentioned further scheme is：Realization balance weight mechanism easily and effectively is in the second card slot difference position
The installation set is fixed.
Further, the release device includes shell and coiling roller bearing, and the enclosure interior is hollow, and is set to unmanned plane
On the downside of fuselage, the ring electromagnet is set to the housing bottom, and the coiling roller bearing rotation is disposed in the housing portion, institute
It states and is set around in the middle part of rope body on the coiling roller bearing.
Advantageous effect using above-mentioned further scheme is：It can effectively realize be located at by setting coiling roller bearing and match
Rope body when needing to launch, is discharged by coiling roller bearing and is detached from by winding storage in the middle part of one section of rope body above heavy-duty machine structure.
Further, further include insulation sleeve, the insulation sleeve package is on the outside of the shell.
Advantageous effect using above-mentioned further scheme is：It effectively prevent, when launching conductive articles, being connected, making with shell
The damage of article is launched in electrification in pairs.
Further, the rope body internal diameter is 4~8cm, and outer diameter is 8~16cm.
Advantageous effect using above-mentioned further scheme is：To adapt to the article to be put of different weight, meet required
Bearing capacity.
Further, the balance weight mechanism is steel weight or lead flake.
Advantageous effect using above-mentioned further scheme is：Gravity can be effectively provided, realize automatically disengaging for rope body.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model product preferred embodiment；
Fig. 2 is the structural schematic diagram of the utility model release device preferred embodiment；
Fig. 3 is the structural schematic diagram of the utility model rope body preferred embodiment；
Fig. 4 is the structural schematic diagram of the utility model balance weight mechanism preferred embodiment.
In attached drawing, parts list represented by the reference numerals are as follows：
1, release device, 2, rope body, 3, balance weight mechanism, 4, unmanned plane, 5, ring electromagnet, 6, adsorption piece, 7, even
Fitting, the 8, first card slot, the 9, second card slot, 10, protrusion, 11, fixed part, 12, mounting portion, 13, shell, 14, coiling roller bearing.
Specific implementation mode
The principles of the present invention and feature are described below in conjunction with attached drawing, example is served only for explaining this practicality
It is novel, it is not intended to limit the scope of the utility model.
As shown in Figures 1 to 3, a kind of unmanned plane delivery device, including release device 1, rope body 2, balance weight mechanism 3 and distant
Device is controlled, the release device 1 is fixed on the downside of 4 fuselage of unmanned plane, and is internally provided with ring electromagnet 5, the rope body 2
One end is equipped with adsorption piece 6, and the outer diameter of the adsorption piece 6 is connect with the internal diameter of the ring electromagnet 5 matching magnetism, the rope
The other end connection of ontology 2 needs to be thrown goods and materials, and therefrom part is two sections to the rope body 2, and two sections of rope bodies 2 pass through
Connector 7 is connected, 7 inner hollow of the connector, and outside is equipped with and is connected with inside the first card slot 8 and the second card slot 9, institute
The first card slot 8 to be stated with described second card slot, 9 one end to be connected, first card slot 8 is arranged close to the release device 1, and described the
Two draw-in groove 9 is located at first card slot, 8 side far from the release device 1, and the width of first card slot 8 is more than described
The width of second card slot 9,3 outer surface of the balance weight mechanism are equipped with protrusion 10, and raised 10 width is more than described second and blocks
The width of slot 9, and less than the width of first card slot 8, the balance weight mechanism 3 passes through described first to block by described raised 10
After slot 8, sliding is set in second card slot 9, and the distance between the balance weight mechanism 3 and the release device 1 are less than
Release altitude, the remote controler are connected with unmanned plane 4, the control of the release device 1 respectively.The utility model product passes through rope
2 both ends of ontology are separately connected release device 1 and goods and materials to be put, and release device 1 is arranged on unmanned plane 4, on rope body 2
It is provided with balance weight mechanism 3, balance weight mechanism 3 passes through the first card slot 8 on connector 7 particular by protrusion 10, is then slid into
Positioning in second card slot 9, since the width of protrusion 10 is more than the width of the second card slot 9, balance weight mechanism 3 will not be from second
It is pulled out in card slot 9.It should be noted that the middle part winding positioned at one section of rope body 2 of 3 top of balance weight mechanism is set to release dress
Set in 1, the distance between balance weight mechanism 3 and release device 1 are less than release altitude, specifically, balance weight mechanism 3 and goods and materials to be thrown it
Between distance can be 2m to 3m, thus release device 1 can be made when discharging rope body 2, goods and materials to be put can be with
It is first fallen, balance weight mechanism 3 is now in the air, without departing from rope body 2 after goods and materials landing to be put, in counter weight machine
Under the gravity of structure 3, the adsorption piece 6 of 2 one end of rope body will be detached from out of release device 1 ring electromagnet 5, be completed
The dispensing of goods and materials does not interfere with the normal flight of unmanned plane.In addition, can very easily to unmanned plane 4 and be released by remote controler
It puts device 1 to be manipulated, realizes across high-altitude and launch messenger operation.The utility model unmanned plane delivery device can facilitate missile
Money, realization automatically disengage, and can meet the dispensing to charging article, greatly improve working efficiency and reduce labor intensity, avoid
It is artificial to carry out hazardous environment operation.
As shown in Figures 3 and 4, consider to realize the mounting height for adjusting balance weight mechanism 3, meet different release altitude requirements,
Preferably, the shape of second card slot 9 is in strip, and is arranged along the length direction of the rope body 2, the rope sheet
The position that 2 inner wall of body corresponds to second card slot 9 is equipped at intervals with multiple fixed parts 11 along its length, and described raised 10 are equipped with
With the mounting portion 12 of 11 Matching installation of the fixed part.
Further, effective for convenience to realize that balance weight mechanism 3 is fixed in the installation of 9 different location of the second card slot, institute
It is the fixed seat inlayed on 2 inner wall of the rope body to state fixed part 11, and internal thread, the mounting portion are equipped in the fixed seat
12 outer surfaces are equipped with external screw thread, and the mounting portion 12 is threadedly coupled with the fixed seat.Specifically, mounting portion 12 can be arranged to
Plastic part, fixed seat can be arranged to plastic seat or mounting portion 12 can be arranged to metalwork, and fixed seat can be arranged to gold
Belong to seat.
As shown in Fig. 2, the release device 1 includes shell 13 and coiling roller bearing 14,13 inner hollow of the shell, and set
On the downside of 4 fuselage of unmanned plane, the ring electromagnet 5 is set to 13 bottom of the shell, and what the coiling roller bearing 14 rotated is set to
Inside the shell 13, the middle part of the rope body 2 is set around on the coiling roller bearing 14.It can by the way that coiling roller bearing 14 is arranged
Effectively to realize by one section of rope body, the 2 middle part winding storage above balance weight mechanism 3, when needing to launch, by coiling
Roller bearing 14, which discharges rope body 2, to be detached from.
Preferably, further include insulation sleeve, the insulation sleeve package is on the outside of the shell 13.It effectively prevent throwing
It when putting conductive articles, is connected with shell 13, causes the damage for launching article to electrification.
In order to adapt to the article to be put of different weight, meeting required bearing capacity, 2 internal diameter of the rope body is 4~
8cm, outer diameter are 8~16cm.Preferably, the balance weight mechanism 3 is steel weight or lead flake, can effectively provide gravity, is realized
Rope body 2 automatically disengages.
In the description of the present invention, it should be understood that term "center", " longitudinal direction ", " transverse direction ", " length ", " width
Degree ", " thickness ", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom" "inner", "outside", " suitable
The orientation or positional relationship of the instructions such as hour hands ", " counterclockwise ", " axial direction ", " radial direction ", " circumferential direction " is orientation based on ... shown in the drawings
Or position relationship, be merely for convenience of describing the present invention and simplifying the description, do not indicate or imply the indicated device or
Element must have a particular orientation, with specific azimuth configuration and operation, therefore should not be understood as the limit to the utility model
System.
In addition, term " first ", " second " are used for description purposes only, it is not understood to indicate or imply relative importance
Or implicitly indicate the quantity of indicated technical characteristic.Define " first " as a result, the feature of " second " can be expressed or
Implicitly include at least one this feature.The meaning of " plurality " is at least two, such as two in the description of the present invention,
It is a, three etc., unless otherwise specifically defined.
In the present invention unless specifically defined or limited otherwise, term " installation ", " connected ", " connection ", " Gu
It is fixed " etc. terms shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integral；Can be
Mechanical connection can also be electrical connection；It can be directly connected, can also can be indirectly connected through an intermediary two
The interaction relationship of connection or two elements inside element, unless otherwise restricted clearly.For the common skill of this field
For art personnel, the concrete meaning of above-mentioned term in the present invention can be understood as the case may be.
In the present invention unless specifically defined or limited otherwise, fisrt feature is "above" or "below" second feature
Can be that the first and second features are in direct contact or the first and second features pass through intermediary mediate contact.Moreover, first is special
Sign second feature " on ", " top " and " above " can be fisrt feature and be directly above or diagonally above the second feature, or only
Indicate that fisrt feature level height is higher than second feature.Fisrt feature second feature " under ", " lower section " and " below " can be with
It is that fisrt feature is directly under or diagonally below the second feature, or is merely representative of fisrt feature level height and is less than second feature.
In the description of this specification, reference term " one embodiment ", " some embodiments ", " example ", " specifically show
The description of example " or " some examples " etc. means specific features, structure, material or spy described in conjunction with this embodiment or example
Point is contained at least one embodiment or example of the utility model.In the present specification, to the schematic table of above-mentioned term
It states and is necessarily directed to identical embodiment or example.Moreover, particular features, structures, materials, or characteristics described can be with
It can be combined in any suitable manner in any one or more of the embodiments or examples.In addition, without conflicting with each other, this field
Technical staff can by the feature of different embodiments or examples described in this specification and different embodiments or examples into
Row combines and combination.
Although the embodiments of the present invention have been shown and described above, it is to be understood that above-described embodiment is
Illustratively, it should not be understood as limiting the present invention, those skilled in the art are in the scope of the utility model
Inside it can make changes, modifications, alterations, and variations to the above described embodiments.
Claims (7)
1. a kind of unmanned plane delivery device, which is characterized in that including release device (1), rope body (2), balance weight mechanism (3) and
Remote controler, the release device (1) is fixed on the downside of unmanned plane (4) fuselage, and is internally provided with ring electromagnet (5), described
Rope body (2) one end is equipped with adsorption piece (6), and the outer diameter of the adsorption piece (6) is matched with the internal diameter of the ring electromagnet (5)
Magnetism connection, the other end connection of the rope body (2) need to be thrown goods and materials, and therefrom part is two sections to the rope body (2),
Two sections of rope bodies (2) are connected by connector (7), connector (7) inner hollow, and outside is equipped with and connects with inside
Logical the first card slot (8) and the second card slot (9), first card slot (8) are connected with described second card slot (9) one end, and described
One card slot (8) is arranged close to the release device (1), and second card slot (9) is located at first card slot (8) and is released far from described
The side of device (1) is put, and the width of first card slot (8) is more than the width of second card slot (9), the balance weight mechanism
(3) outer surface is equipped with raised (10), and the width of the protrusion (10) is more than the width of second card slot (9), and less than described
The width of first card slot (8), after the balance weight mechanism (3) passes through first card slot (8) by described raised (10), sliding
In second card slot (9), and the distance between the balance weight mechanism (3) and the release device (1) are less than dispensing height
Degree, the remote controler are connected with unmanned plane (4), the release device (1) control respectively.
2. unmanned plane delivery device according to claim 1, which is characterized in that the shape of second card slot (9) is in length
Strip, and be arranged along the length direction of the rope body (2), rope body (2) inner wall corresponds to second card slot (9)
Position be equipped at intervals with multiple fixed parts (11) along its length, the protrusion (10) is equipped with to be matched with the fixed part (11)
The mounting portion (12) of installation.
3. unmanned plane delivery device according to claim 2, which is characterized in that the fixed part (11) is the rope sheet
The fixed seat inlayed on body (2) inner wall, the fixed seat is interior to be equipped with internal thread, and mounting portion (12) outer surface is equipped with outer spiral shell
Line, the mounting portion (12) are threadedly coupled with the fixed seat.
4. unmanned plane delivery device according to claim 1, which is characterized in that the release device (1) includes shell
(13) and coiling roller bearing (14), shell (13) inner hollow, and on the downside of unmanned plane (4) fuselage, the annular electromagnetism
Iron (5) is set to the shell (13) bottom, and coiling roller bearing (14) rotation is set to the shell (13) inside, the rope
It is set around in the middle part of ontology (2) on the coiling roller bearing (14).
5. unmanned plane delivery device according to claim 4, which is characterized in that further include insulation sleeve, the insulation sleeve packet
It wraps up on the outside of the shell (13).
6. unmanned plane delivery device according to claim 1, which is characterized in that rope body (2) internal diameter be 4~
8cm, outer diameter are 8~16cm.
7. unmanned plane delivery device according to any one of claims 1 to 6, which is characterized in that the balance weight mechanism (3) is
Steel weight or lead flake.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820390498.0U CN208021754U (en) | 2018-03-21 | 2018-03-21 | A kind of unmanned plane delivery device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820390498.0U CN208021754U (en) | 2018-03-21 | 2018-03-21 | A kind of unmanned plane delivery device |
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| Publication Number | Publication Date |
|---|---|
| CN208021754U true CN208021754U (en) | 2018-10-30 |
Family
ID=63907929
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820390498.0U Active CN208021754U (en) | 2018-03-21 | 2018-03-21 | A kind of unmanned plane delivery device |
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| Country | Link |
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| CN (1) | CN208021754U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110615095A (en) * | 2018-09-28 | 2019-12-27 | 杭州零零科技有限公司 | Hand-held remote control device and flight system set |
-
2018
- 2018-03-21 CN CN201820390498.0U patent/CN208021754U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110615095A (en) * | 2018-09-28 | 2019-12-27 | 杭州零零科技有限公司 | Hand-held remote control device and flight system set |
| CN110615095B (en) * | 2018-09-28 | 2021-04-13 | 杭州零零科技有限公司 | Hand-held remote control device and flight system set |
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