CN110525654A - A kind of delivery device of unmanned plane - Google Patents
A kind of delivery device of unmanned plane Download PDFInfo
- Publication number
- CN110525654A CN110525654A CN201910961682.5A CN201910961682A CN110525654A CN 110525654 A CN110525654 A CN 110525654A CN 201910961682 A CN201910961682 A CN 201910961682A CN 110525654 A CN110525654 A CN 110525654A
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- China
- Prior art keywords
- loading attachment
- lead screw
- upper box
- servo motor
- bracket
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- 230000005611 electricity Effects 0.000 claims description 4
- 238000000034 method Methods 0.000 abstract description 6
- 230000005540 biological transmission Effects 0.000 abstract description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power-Operated Mechanisms For Wings (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses a kind of delivery devices of unmanned plane, it is related to air vehicle technique field, first servo motor including bracket and on bracket, the bracket is equipped with fixed link and lead screw, the lead screw is rotationally connected on bracket, one end of the lead screw is connected to the output shaft of first servo motor, loading attachment one and loading attachment two are slidably connected in the fixed link, the loading attachment one and loading attachment two all cooperate with threads of lead screw, the loading attachment one is opposite with the hand of spiral of loading attachment two, the loading attachment one and loading attachment two are symmetrically set in fixed link, the configuration of the present invention is simple, it is convenient to operate, pass through setting lead screw transmission and loading attachment, the quick dispensing to article may be implemented, the height of the easily controllable dispensing of the device, and launch process is relatively stable.
Description
Technical field
The present invention relates to air vehicle technique fields, and in particular to a kind of delivery device of unmanned plane.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
Machine tool remote control station personnel track it, are positioned, are remotely controlled, telemetering and Digital Transmission by the equipment such as radar.It can be in radio
It takes off as conventional airplane under remote control or is launched with booster rocket, aerial launch can also be taken to by machine tool and flown.Recycling
When, the mode automatic Landing as conventional airplane landing mission can be used, can also be recycled by remote control parachute or block.It can
It is reused several times.It is widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..
With the development of technology, the application of unmanned plane is more next wide, and it is also emerging at one to launch express delivery using unmanned plane
Industry, but current throwing device be mostly mount point hang a rope be fixed so that weight is to unmanned plane
It takes off and causes large effect with flight attitude, and be unfavorable for the stability that control is launched.
Chinese patent application is that CN201620079514.5 discloses a kind of delivery device of load-carrying air-drop unmanned plane, is equipped with
Two C-shaped-rods, limit carbon pipe, set square, elastic string, fixed rope；Two C-shaped-rods can be rotated around respective axis of rotation, two C
The upper end of shape bar is respectively equipped with pin hole, and the middle-end of two C-shaped-rods connects elastic string, and the lower end of two C-shaped-rods passes through fixed rope
Connect missile；The upper end closed position of two C-shaped-rods be located at limit carbon pipe and for the set square of fixed main body at.Utilize bullet
The combination of the mechanical structure of the elastic force and device of power rope achievees the purpose that automatically reset after launching；Simply, light reliable, C-shaped-rod,
Stretch cord achievees the purpose that carrying weight, stretch cord achieve the purpose that automatically reset in conjunction with bolt, reduces the matter of delivery device
Amount reduces the difficulty of delivery device production and manipulation.The design and fabrication for launching hatch door can be removed from, artificially control cabin door lock, benefit
It is launched with weight gravity itself, completes to automatically restore to the preceding state of dispensing after launching using elastic string.But this kind of equipment is still
The unstable defect of rope carry is not solved.
Summary of the invention
The purpose of the present invention is to provide a kind of delivery devices of unmanned plane, caused by the prior art above-mentioned more to solve
Item defect.
A kind of delivery device of unmanned plane, the first servo motor including bracket and on bracket are set on the bracket
There are fixed link and lead screw, the lead screw is rotationally connected on bracket, and one end of the lead screw is connected to the defeated of first servo motor
Shaft slidably connects loading attachment one and loading attachment two, the loading attachment one and loading attachment two in the fixed link
All cooperate with threads of lead screw, the hand of spiral of the loading attachment one and loading attachment two is on the contrary, the loading attachment one and dress
It carries and sets two and be symmetrically set in fixed link.
Preferably, the loading attachment one includes upper box one, lower box one, chamber door one and the second servo motor, described
Upper box one is slidably connected in fixed link, and shaft one is rotatably connected on the upper box one, and second servo motor is set
In on upper box one, the shaft one is connected to the output shaft of the second servo motor, and the lower box one is fixed in shaft one,
The chamber door one is articulated with lower box one, and the upper box one is equipped with the first card slot, and the chamber door one is equipped with and the first card
The first buckle that slot matches, the upper box one cooperate with threads of lead screw.
Preferably, the loading attachment two includes upper box two, lower box two, chamber door two and third servo motor, described
Upper box two is slidably connected in fixed link, and shaft two is rotatably connected on the upper box two, and the third servo motor is set
In on upper box two, the shaft two is connected to the output shaft of third servo motor, and the lower box two is fixed in shaft two,
The chamber door two is articulated with lower box two, and the upper box two is equipped with the second card slot, and the chamber door two is equipped with and the second card
The second buckle that slot matches, the upper box two cooperate with threads of lead screw.
Preferably, the bracket is equipped with baffle.
Preferably, the baffle section is L-type.
The present invention has the advantages that structure is simple, it is convenient to operate, and passes through setting lead screw transmission and loading attachment, Ke Yishi
Now to the quick dispensing of article, the height of the easily controllable dispensing of the device, and launch process is relatively stable.
Detailed description of the invention:
Fig. 1 is the structural diagram of the present invention.
Fig. 2 is main view of the invention.
Fig. 3 is side view of the invention.
Fig. 4 is rearview of the invention.
Wherein, 1- bracket, 2- fixed link, 3- lead screw, 4- loading attachment one, 401- upper box one, 402- lower box one,
403- chamber door one, the second servo motor of 404-, 405- shaft one, the first card slot of 406-, 407- first are buckled, 5- the first servo electricity
Machine, 6- loading attachment two, 601- upper box two, 602- lower box two, 603- chamber door two, 604- third servo motor, 605- turn
Axis two, the second card slot of 606-, 607- second are buckled, 7- baffle.
Specific embodiment
To be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, below with reference to
Specific embodiment, the present invention is further explained.
As shown in Figures 1 to 4, a kind of delivery device of unmanned plane, the first servo including bracket 1 and on bracket 1
Motor 5, the bracket 1 are equipped with fixed link 2 and lead screw 3, and the lead screw 3 is rotationally connected on bracket 1, and the one of the lead screw 3
End is connected to the output shaft of first servo motor 5, slidably connects loading attachment 1 and loading attachment two in the fixed link 2
6, the loading attachment 1 and loading attachment 26 are all threadedly engaged with lead screw 3, the loading attachment 1 and loading attachment 26
Hand of spiral on the contrary, the loading attachment 1 and loading attachment 26 are symmetrically set in fixed link 2.
In the present embodiment, the loading attachment 1 includes upper box 1, lower box 1, chamber door 1 and the
Two servo motors 404, the upper box 1 are slidably connected in fixed link 2, are rotatably connected on the upper box 1
Shaft 1, second servo motor 404 are set on upper box 1, and the shaft 1 is connected to the second servo electricity
The output shaft of machine 404, the lower box 1 are fixed in shaft 1, and the chamber door 1 is articulated with lower box one
402, the upper box 1 is equipped with the first card slot 406, and the chamber door 1 is equipped with and matches with the first card slot 406
First buckle 407, the upper box 1 is threadedly engaged with lead screw 3, the loading attachment 26 including upper box 2 601, under
Cabinet 2 602, chamber door 2 603 and third servo motor 604, the upper box 2 601 is slidably connected in fixed link 2, described
Shaft 2 605 is rotatably connected on upper box 2 601, the third servo motor 604 is set on upper box 2 601, and described turn
Axis 2 605 is connected to the output shaft of third servo motor 604, and the lower box 2 602 is fixed in shaft 2 605, the case
Door 2 603 is articulated with lower box 2 602, and the upper box 2 601 is equipped with the second card slot 606, and the chamber door 2 603 is equipped with
The second buckle 607 matched with the second card slot 606, the upper box 2 601 is threadedly engaged with lead screw 3, one 4 He of loading attachment
Loading attachment 26 can be used for loading cargo, and loading attachment 1 and loading attachment 26 are further reinforced in the design of buckle and card slot
Leakproofness.
In the present embodiment, the bracket 1 is equipped with baffle 7, and 7 section of baffle is L-type, reinforces loading attachment 1
With the tightness of the bottom of loading attachment 26.
The present apparatus: being fixed on the bottom of unmanned plane by the course of work and principle first, when need to freight object when, by first card
Button 407 and the second buckle 607 are extracted from the first card slot 406 and the second card slot 607 respectively, by chamber door 1 and chamber door 2 603
It opens, cargo is put into loading attachment 1 and loading attachment 26, chamber door 1 and chamber door 2 603 are closed, by the first card
Button 407 and the second buckle 607 are inserted into the first card slot 406 and the second card slot 607 respectively, complete to load, when cargo needs to launch,
Fly to unmanned plane to target location, start first servo motor 5, drives lead screw 3 to rotate, make loading attachment 1 and loading attachment
26 backwards to movement, while starting the second servo motor 404 and the second servo motor 604, makes lower box 1 and lower box two
602 rotate down, and complete the dispensing of object, to be put to finish, and drive the second servo motor 404 and the second servo motor 604, make
Lower box 1 and lower box 2 602 are rotated up, until lower box 1, lower box 2 602 respectively with upper box one
601, lower box 2 602 is closed, and starts first servo motor 5, is driven lead screw 3 to rotate, is made loading attachment 1 and loading attachment two
6 move toward one another, until loading attachment 1 and loading attachment 26 are combined, complete to launch work.
Based on above-mentioned, the configuration of the present invention is simple, it is convenient to operate, and by setting lead screw transmission and loading attachment, may be implemented
Quick dispensing to article, the height of the easily controllable dispensing of the device, and launch process is relatively stable.
As known by the technical knowledge, the present invention can pass through the embodiment party of other essence without departing from its spirit or essential feature
Case is realized.Therefore, embodiment disclosed above, in all respects are merely illustrative, not the only.Institute
Have within the scope of the present invention or is included in the invention in the change being equal in the scope of the present invention.
Claims (5)
1. a kind of delivery device of unmanned plane, which is characterized in that including bracket (1) and the first servo being set on bracket (1) electricity
Machine (5), the bracket (1) are equipped with fixed link (2) and lead screw (3), and the lead screw (3) is rotationally connected on bracket (1), described
One end of lead screw (3) is connected to the output shaft of first servo motor (5), slidably connects loading attachment on the fixed link (2)
One (4) and loading attachment two (6), the loading attachment one (4) and loading attachment two (6) are all threadedly engaged with lead screw (3), described
The hand of spiral of loading attachment one (4) and loading attachment two (6) is on the contrary, the loading attachment one (4) and loading attachment two (6) are right
Claim to be set on fixed link (2).
2. a kind of delivery device of unmanned plane according to claim 1, which is characterized in that loading attachment one (4) packet
Include upper box one (401), lower box one (402), chamber door one (403) and the second servo motor (404), the upper box one
(401) it is slidably connected on fixed link (2), is rotatably connected to shaft one (405) on the upper box one (401), described second
Servo motor (404) is set on upper box one (401), and the shaft one (405) is connected to the output of the second servo motor (404)
Axis, the lower box one (402) are fixed in shaft one (405), and the chamber door one (403) is articulated with lower box one (402), institute
Upper box one (401) is stated equipped with the first card slot (406), the chamber door one (403) is equipped with and matches with the first card slot (406)
The first buckle (407), the upper box one (401) is threadedly engaged with lead screw (3).
3. according to a kind of delivery device for unmanned plane that claim 2 is stated, which is characterized in that the loading attachment two (6) includes
Upper box two (601), lower box two (602), chamber door two (603) and third servo motor (604), the upper box two (601)
It is slidably connected on fixed link (2), shaft two (605), the third servo electricity is rotatably connected on the upper box two (601)
Machine (604) is set on upper box two (601), and the shaft two (605) is connected to the output shaft of third servo motor (604), institute
Lower box two (602) is stated to be fixed in shaft two (605), the chamber door two (603) is articulated with lower box two (602), it is described on
Cabinet two (601) is equipped with the second card slot (606), and the chamber door two (603) is equipped with the matched with the second card slot (606)
Two buckles (607), the upper box two (601) are threadedly engaged with lead screw (3).
4. a kind of delivery device of unmanned plane according to claim 1, which is characterized in that the bracket (1) is equipped with gear
Plate (7).
5. a kind of delivery device of unmanned plane according to claim 4, which is characterized in that baffle (7) section is L
Type.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910961682.5A CN110525654B (en) | 2019-10-11 | 2019-10-11 | Unmanned aerial vehicle's input device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910961682.5A CN110525654B (en) | 2019-10-11 | 2019-10-11 | Unmanned aerial vehicle's input device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110525654A true CN110525654A (en) | 2019-12-03 |
| CN110525654B CN110525654B (en) | 2020-11-27 |
Family
ID=68671620
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910961682.5A Active CN110525654B (en) | 2019-10-11 | 2019-10-11 | Unmanned aerial vehicle's input device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110525654B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114590405A (en) * | 2022-03-22 | 2022-06-07 | 南京信息工程大学 | Unmanned aerial vehicle for insect throwing |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN207997985U (en) * | 2018-03-12 | 2018-10-23 | 重庆市亿飞智联科技有限公司 | A kind of air-drop unmanned plane |
| CN108791899A (en) * | 2018-07-01 | 2018-11-13 | 陈爱霞 | The equipment launched for unmanned plane |
| US20190066032A1 (en) * | 2017-08-22 | 2019-02-28 | Qualcomm Incorporated | Robotic Vehicle Item Delivery Security System |
| CN109941432A (en) * | 2019-03-06 | 2019-06-28 | 深圳市律远汇智科技有限公司 | A kind of logistics distribution unmanned plane with regulatory function having a smooth flight |
-
2019
- 2019-10-11 CN CN201910961682.5A patent/CN110525654B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20190066032A1 (en) * | 2017-08-22 | 2019-02-28 | Qualcomm Incorporated | Robotic Vehicle Item Delivery Security System |
| CN207997985U (en) * | 2018-03-12 | 2018-10-23 | 重庆市亿飞智联科技有限公司 | A kind of air-drop unmanned plane |
| CN108791899A (en) * | 2018-07-01 | 2018-11-13 | 陈爱霞 | The equipment launched for unmanned plane |
| CN109941432A (en) * | 2019-03-06 | 2019-06-28 | 深圳市律远汇智科技有限公司 | A kind of logistics distribution unmanned plane with regulatory function having a smooth flight |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114590405A (en) * | 2022-03-22 | 2022-06-07 | 南京信息工程大学 | Unmanned aerial vehicle for insect throwing |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110525654B (en) | 2020-11-27 |
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