CN208021749U - A kind of unmanned plane delivery device - Google Patents
A kind of unmanned plane delivery device Download PDFInfo
- Publication number
- CN208021749U CN208021749U CN201820374204.5U CN201820374204U CN208021749U CN 208021749 U CN208021749 U CN 208021749U CN 201820374204 U CN201820374204 U CN 201820374204U CN 208021749 U CN208021749 U CN 208021749U
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- unmanned plane
- turntable
- vertical
- inner cylinder
- shell
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Abstract
The utility model is related to a kind of unmanned plane delivery devices,Including shell,Article-holding device,First driving means and the second driving device,Article-holding device includes turntable and is fixedly arranged on the shaft of center of turntable,Shaft is connect across shell top with first driving means,Turntable includes outer ring,Inner ring,It connects multiple connecting shafts of outer ring and inner ring and is fixedly arranged on several baffles on outer ring,The cavity that vertical inner cylinder and vertical outer barrel form several storage missiles with turntable and baffle is equipped at the outer edge of outer ring,Cabochon dispensing port there are one being set on vertical inner cylinder,The driving chamber for being formed and accommodating the second driving device is protruded outward in vertical outer barrel position corresponding with dispensing port,Under first driving means drive,Dispensing object in driven by rotary disc cavity is moved to dispensing port position,Second driving device, which will launch object, to be hauled oneself willingly into and puts mouth and push,To next dispensing place,Continue to launch.The utility model can be launched continuously in different appointed places, and simple in structure, at low cost.
Description
Technical field
The utility model is related to unmanned plane apparatus fields, and in particular to a kind of unmanned plane delivery device.
Background technology
Unmanned plane is the abbreviation of unmanned remote controlled aircraft, at low cost, manipulation is simple, loading capacity is big, to weather, landform
It is required that low advantage, therefore be more and more widely used in fields such as the disaster relief, meteorology, mappings.In such applications, need by
Disaster relief supplies or monitoring instrument etc. are thrown to fixed location, especially in fields such as weather monitorings, need same instrument
Equipment air-drop is monitored in different positions, and the continuous delivery device of current unmanned plane is complicated, of high cost.
Utility model content
The technical problem to be solved by the utility model is to provide one kind continuously launching object and knot in different location
The unmanned plane delivery device of the simple low cost of structure.
The technical solution that the utility model solves above-mentioned technical problem is as follows：A kind of unmanned plane delivery device, including including
Shell, article-holding device, first driving means and the second driving device, the shell include shell bottom, shell top and side wall, the shell top
It is equipped with the fixing device for being fixedly connected with unmanned plane, the article-holding device is located in the shell, including horizontally disposed
Turntable and be fixedly arranged on the shaft of the center of turntable, the shaft passes through the shell top and is rotatablely connected with the shell top, institute
First driving means are stated above the shell top and its output shaft is fixedly connected with the shaft, the turntable include outer ring,
Inner ring, multiple connecting shafts and be fixedly arranged on equally distributed several baffles on the outer ring, the connecting shaft both ends respectively with it is described
Outer ring inner edge is connected with inner ring outer rim, be respectively equipped at the outer ring outer edge bottom end be fixedly connected with the shell bottom it is vertical
Inner cylinder and vertical outer barrel, the vertical inner cylinder and vertical outer barrel are coaxially disposed and form several use together with the turntable and baffle
In the cavity of storage missile, the top of the vertical inner cylinder is described by being fixedly connected at the top of connecting rod and the vertical outer barrel
Turntable can be rotated relative to the vertical inner cylinder and vertical outer barrel, set that there are one cabochon dispensing ports on the vertical inner cylinder, described
The driving chamber for being formed and accommodating second driving device is protruded in vertical outer barrel position corresponding with the dispensing port outward, described
Second driving device includes that sequentially connected actuator, catch bar and movable plate, the actuator are fixed on described from the outside to the core
The side wall centers of driving chamber simultaneously can drive the movable plate to do linear reciprocation along the axial direction of the catch bar by the catch bar
Movement, region corresponding with the vertical inner cylinder is a through-hole on the shell bottom.
The utility model has the beneficial effects that：The object for needing continuously to launch is put into article-holding device, when needing to launch, the
One driving device drives turntable rotation, the cavity that object is launched in accommodate nearest from dispensing port to turn to dispensing port position, open
Dynamic second driving device, movable plate are pushed from dispensing port by object is launched, are thrown in the air by through-hole, then fly to second to throw
Place is put, continues to launch, the utility model can be launched continuously in appointed place, and simple in structure, at low cost.
Based on the above technical solution, the utility model can also do following improvement.
Further, the fixing device includes two symmetrical rectangular fixed frames and is located on the fixed frame upper frame body
Several fasteners, the lower frame body of the fixed frame is fixedly connected with shell top upper surface, and the fastener includes phase interworking
The screw of conjunction and the screw hole on the fixed frame upper frame body.
Advantageous effect using above-mentioned further scheme is that the unmanned plane of the utility model is launched dress by fixing device
It sets and is fixed on unmanned plane, keep whole device more secured, and fixture structure is simple, it is versatile.
Further, the quantity of the baffle is consistent with the connection number of axle and positioned at on Radius, the baffle
Width is less than the width between the outer ring outer edge.
Advantageous effect using above-mentioned further scheme is that barrier width is less than the width between the outer ring outer edge
Degree so that baffle can and turntable rotated between vertical outer barrel and vertical inner cylinder together, when hold launch object cavity reach
When to dispensing port position, two adjacent connecting shafts are placed exactly in the both sides of dispensing port, and the object enable is connected by two
Space between axis is fallen.
Further, the dispensing port width vertical inner cylinder corresponding with a cavity is of same size, is highly the turntable
The distance between described vertical inner cylinder intersection to the vertical inner cylinder top.
The rotation angle that first driving means control turntable is easy for using the advantageous effect of above-mentioned further scheme so that
Dispensing port can be matched with each cavity, and under the thrust of the second driving device, object can smoothly be detached from article-holding device.
Further, the first driving means are servo motor.
Advantageous effect using above-mentioned further scheme is the angle that servo motor can more accurately control turntable rotation, is made
Every time when operating, two side shields of cavity are just concordant with the edge of dispensing port, and stability is high.
Further, the actuator is cylinder or hydraulic cylinder.
Advantageous effect using above-mentioned further scheme is that cylinder or hydraulic cylinder are capable of providing straight reciprocating motion, controlling party
Just.
Further, when the actuator retracted mode, the movable plate is located in the driving chamber.
Advantageous effect using above-mentioned further scheme is in turntable rotation process, not influenced by movable plate, Neng Goushun
Profit rotation.
Further, the shell top is equipped with opening for missile to be put into article-holding device.
Advantageous effect using above-mentioned further scheme is will to launch object before unmanned plane starts to be put into unmanned plane dispensing
Device.
Further, the width of the movable plate is less than or equal to the width of dispensing port.
When advantageous effect using above-mentioned further scheme is that actuator is extended to longest, it can utilize movable plate that will launch
Object is pushed into most marginal position and ensures to launch object to haul oneself willingly into put mouth and fall.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model unmanned plane delivery device；
Fig. 2 is the structural schematic diagram of unmanned plane delivery device shown in FIG. 1, and the shell top of middle casing and side wall are not shown；
Fig. 3 is the vertical view of unmanned plane delivery device shown in Fig. 2.
In attached drawing, parts list represented by the reference numerals are as follows：
1, shell, 2, article-holding device, 3, first driving means, the 4, second driving device, 5, shell bottom, 6, shell top, 7, side wall,
8, fixing device, 9, turntable, 10, shaft, 11, outer ring, 12, inner ring, 13, connecting shaft, 14, baffle, 15, vertical inner cylinder, 16, perpendicular
Straight outer barrel, 17, cavity, 18, dispensing port, 19, driving chamber, 20, actuator, 21, catch bar, 22, movable plate, 23, fixed frame,
24, fastener, 25, screw, 26, screw hole, 27, opening, 28, connecting rod.
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 Figs. 1-2, the utility model provides a kind of unmanned plane delivery device, including shell 1, article-holding device 2,
One driving device 3 and the second driving device 4, the shell 1 include shell bottom 5, shell top 6 and side wall 7, and the shell top 6, which is equipped with, to be used
In the fixing device 8 being fixedly connected with unmanned plane, the article-holding device 2 is located in the shell 1, including horizontally disposed turntable
9 and it is fixedly arranged on the shaft 10 of the center of turntable, the shaft 10 passes through the shell top 6 and is rotatablely connected with the shell top 6, institute
First driving means 3 are stated above the shell top 6 and its output shaft is fixedly connected with the shaft 10, the turntable 9 includes
Outer ring 11, inner ring 12, multiple connecting shafts 13 and it is fixedly arranged on equally distributed several baffles 14, the connecting shaft on the outer ring 11
13 both ends are connect with 11 inner edge of the outer ring and 12 outer rim of inner ring respectively, be respectively equipped at 11 outer edge of the outer ring bottom end with
The vertical inner cylinder 15 and vertical outer barrel 16 that the shell bottom 5 is fixedly connected, the vertical inner cylinder 15 and vertical outer barrel 16 are coaxially disposed
And several cavitys 17 for storing missile, the top of the vertical inner cylinder 15 are formed together with the turntable 9 and baffle 14
It is fixedly connected with 16 top of the vertical outer barrel by connecting rod 28, one or more can be arranged in the connecting rod 28, described turn
Disk 9 can be rotated relative to the vertical inner cylinder 15 and vertical outer barrel 16, set that there are one cabochon dispensing ports on the vertical inner cylinder 15
18, the drive for being formed and accommodating second driving device 4 is protruded in the vertical outer barrel 16 position corresponding with dispensing port 18 outward
Dynamic chamber 19, second driving device 4 include sequentially connected actuator 20, catch bar 21 and movable plate 22 from the outside to the core, institute
Actuator 20 is stated to be fixed on the side wall centers of the driving chamber 19 and 22 edge of the movable plate can be driven by the catch bar 21
The axis of the catch bar 21 does straight reciprocating motion, and region corresponding with the vertical inner cylinder 15 is one logical on the shell bottom 5
Hole.The shell top 6 is equipped with opening 27 for missile to be put into article-holding device 2, and the fixing device 8 includes two symmetrical sides
On several fasteners 24 on shape fixed frame 23 and framework disposed thereon, the lower frame body of the fixed frame 23 and the shell top 6
Surface is fixedly connected, and the fastener 24 includes mutually matched screw 25 and the screw hole on the fixed frame upper frame body
26.The first driving means 3 are servo motor, and the actuator 20 is cylinder or hydraulic cylinder.
It is put into article-holding device 2 by object is launched by the opening on shell top 6, and is launched unmanned plane by fixing device 8
Device is fixed on unmanned plane, when unmanned plane flies to designated position, is rotated turntable 9 admittedly by controlling first driving means 3
Determine angle, the wherein width of baffle 14 is less than the width between 11 outer edge of the outer ring, 18 width of dispensing port and a sky
The corresponding vertical inner cylinder of chamber 17 15 it is of same size so that the cavity 17 that object is launched in accommodate nearest from dispensing port 18 rotates
To 18 position of dispensing port, servo motor can accurately control the angle of the rotation of turntable 9 and the stability of operation is high, and rotation stops
When, two side shields of cavity 17 are just in the marginal position of dispensing port 18.Before second driving device 4 starts, cylinder or hydraulic pressure
Cylinder is in retracted mode, and movable plate 22 is located in the driving chamber so that the missile body in cavity 17 can be revolved with turntable 9
Transfer held stationary.Then start the second driving device 4, cylinder or hydraulic cylinder elongation, movable plate is driven by catch bar 21
22 move to dispensing port 18, the height of dispensing port 18 be the turntable 9 with 15 intersection of vertical inner cylinder to it is described it is vertical in
The distance between 15 top of cylinder, the width of movable plate 22 is less than or equal to the width of the dispensing port 18 so that 22 energy of movable plate
It is moved to the position of 11 inner edge dispensing port 18 of outer ring, baffle 14 is consistent with the quantity of connecting shaft 13 and positioned at on Radius, energy
Enough ensure that missile is pushed to dispensing port 18 and is directly fallen by through-hole.
The above is only the preferred embodiment of the present invention, is not intended to limit the utility model, all in this practicality
Within novel spirit and principle, any modification, equivalent replacement, improvement and so on should be included in the guarantor of the utility model
Within the scope of shield.
Claims (9)
1. a kind of unmanned plane delivery device, which is characterized in that including shell (1), article-holding device (2), first driving means (3) and
Second driving device (4), the shell (1) include shell bottom (5), shell top (6) and side wall (7), and the shell top (6) is equipped with and is used for
The fixing device (8) being fixedly connected with unmanned plane, the article-holding device (2) are located in the shell (1), including horizontally disposed
Turntable (9) and the shaft (10) for being fixedly arranged on the center of turntable, the shaft (10) pass through the shell top (6) and with the shell top
(6) it is rotatablely connected, the first driving means (3) are set to above the shell top (6) and its output shaft and the shaft (10) are solid
Fixed connection, the turntable (9) include outer ring (11), inner ring (12), multiple connecting shafts (13) and are fixedly arranged on the outer ring (11)
Equally distributed several baffles (14), connecting shaft (13) both ends respectively with the outer ring (11) inner edge and inner ring (12) outer rim
Connection, be respectively equipped at outer ring (11) outer edge vertical inner cylinder (15) that bottom end is fixedly connected with the shell bottom (5) and
Vertical outer barrel (16), the vertical inner cylinder (15) and vertical outer barrel (16) be coaxially disposed and with the turntable (9) and baffle (14)
Formed together it is several for storing the cavitys (17) of missile, the top of the vertical inner cylinder (15) by connecting rod (28) with it is described
It being fixedly connected at the top of vertical outer barrel (16), the turntable (9) can rotate relative to the vertical inner cylinder (15) and vertical outer barrel (16),
Cabochon dispensing port (18) there are one being set on the vertical inner cylinder (15), the vertical outer barrel (16) and the dispensing port (18) are right
The driving chamber (19) for being formed and accommodating second driving device (4), second driving device (4) are protruded outward in the position answered
Including sequentially connected actuator (20), catch bar (21) and movable plate (22) from the outside to the core, the actuator (20) is fixed on
The side wall of the driving chamber (19) simultaneously can drive the movable plate (22) along the catch bar (21) by the catch bar (21)
Axial direction do straight reciprocating motion, region corresponding with vertical inner cylinder (15) is a through-hole on the shell bottom (5).
2. a kind of unmanned plane delivery device according to claim 1, which is characterized in that the fixing device (8) includes two
Several fasteners (24) on a symmetrical rectangular fixed frame (23) and framework disposed thereon, the lower frame body of the fixed frame with
Shell top (6) upper surface is fixedly connected, the fastener (24) include mutually matched screw (25) and be located at the fixation
Screw hole (26) on frame upper frame body.
3. a kind of unmanned plane delivery device according to claim 1, which is characterized in that the quantity of the baffle (14) and institute
Connecting shaft (13) quantity is stated unanimously and positioned at on Radius, the width of the baffle (14) is less than outside in the outer ring (11)
Width between edge.
4. a kind of unmanned plane delivery device according to claim 1, which is characterized in that dispensing port (18) width and one
The corresponding vertical inner cylinder (15) of a cavity (17) it is of same size, be highly the turntable (9) and the vertical inner cylinder
(15) the distance between at the top of intersection to the vertical inner cylinder (15).
5. a kind of unmanned plane delivery device according to claim 1, which is characterized in that the first driving means (3) are
Servo motor.
6. a kind of unmanned plane delivery device according to claim 1, which is characterized in that the actuator (20) be cylinder or
Hydraulic cylinder.
7. any one unmanned plane delivery device according to claim 1 and claim 6, which is characterized in that the drive
When moving part (20) retracted mode, the movable plate (22) is located in the driving chamber (19).
8. a kind of unmanned plane delivery device according to claim 1, which is characterized in that the shell top (6) is equipped with opening
(27) it is used to missile being put into the article-holding device (2).
9. a kind of unmanned plane delivery device according to claim 1, which is characterized in that the width of the movable plate (22) is small
In or equal to the dispensing port (18) width.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820374204.5U CN208021749U (en) | 2018-03-19 | 2018-03-19 | A kind of unmanned plane delivery device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820374204.5U CN208021749U (en) | 2018-03-19 | 2018-03-19 | A kind of unmanned plane delivery device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208021749U true CN208021749U (en) | 2018-10-30 |
Family
ID=63908010
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820374204.5U Active CN208021749U (en) | 2018-03-19 | 2018-03-19 | A kind of unmanned plane delivery device |
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| Country | Link |
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| CN (1) | CN208021749U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112607031A (en) * | 2020-12-22 | 2021-04-06 | 西安羚控电子科技有限公司 | Modular unmanned aerial vehicle cluster aerial rapid delivery system |
| CN112638089A (en) * | 2020-12-28 | 2021-04-09 | 同济大学 | Information module releasing device |
-
2018
- 2018-03-19 CN CN201820374204.5U patent/CN208021749U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112607031A (en) * | 2020-12-22 | 2021-04-06 | 西安羚控电子科技有限公司 | Modular unmanned aerial vehicle cluster aerial rapid delivery system |
| CN112638089A (en) * | 2020-12-28 | 2021-04-09 | 同济大学 | Information module releasing device |
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