CN106477046B - A kind of unmanned plane hose loading single-shot delivery device - Google Patents
A kind of unmanned plane hose loading single-shot delivery device Download PDFInfo
- Publication number
- CN106477046B CN106477046B CN201611057299.XA CN201611057299A CN106477046B CN 106477046 B CN106477046 B CN 106477046B CN 201611057299 A CN201611057299 A CN 201611057299A CN 106477046 B CN106477046 B CN 106477046B
- Authority
- CN
- China
- Prior art keywords
- storage organization
- unmanned plane
- delivery device
- support
- bowl
- 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
Links
- 230000008520 organization Effects 0.000 claims abstract description 26
- 238000010276 construction Methods 0.000 claims abstract description 16
- 230000007246 mechanism Effects 0.000 claims abstract description 11
- 230000008878 coupling Effects 0.000 claims description 7
- 238000010168 coupling process Methods 0.000 claims description 7
- 238000005859 coupling reaction Methods 0.000 claims description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- 244000309464 bull Species 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000005484 gravity Effects 0.000 description 2
- 230000000386 athletic effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000006467 substitution reaction 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Catching Or Destruction (AREA)
- Road Signs Or Road Markings (AREA)
Abstract
The invention discloses a kind of unmanned plane hoses to load single-shot delivery device, including launching structure, storage organization and support construction, the storage organization inclination is fixed on the support structure, the dispensing structure setting falls for controlling the sphere in storage organization from exit one by one in the exit of the storage organization.The storage organization includes flexible hose；The support construction includes several columns of upper plate, lower plate, setting between the upper and lower plates, the pipe support for fixing and supporting the storage organization.The dispensing structure includes guide pipe (5), Bo Wan mechanism, power device.The present invention drives the rotation for dialling bowl by steering engine, realizes that sphere is fallen one by one, in conjunction with the incline structure of corrugated flexible hose, so that sphere orderly slides.
Description
Technical field
The present invention relates to a kind of delivery devices more particularly to a kind of unmanned plane hose to load single-shot delivery device, mainly
The dispensing of the delivery device in field, especially athletic competition and goods and materials transport is launched for unmanned plane.
Background technique
Currently, existing delivery device, typically inclination allow spherical object by self gravity downslide dispensing or round
In the same plane, be then open body dispensing one by one.It is unable to ensure the precision fallen in this way, while delivery device
Running is complicated, so that spherical object is fallen one by one in the same position.
Summary of the invention
It is an object of the invention to solve the problems, such as how in the short time spherical object to be fallen in the same position one by one,
The efficiency launched and precision are improved, a kind of unmanned plane hose loading single-shot delivery device is provided.
It solves the problems, such as that spherical object is quickly fallen in the same position one by one.
The purpose of the present invention is achieved through the following technical solutions:
A kind of unmanned plane hose loading single-shot delivery device, including structure, storage organization and support construction are launched, it is described
Storage organization inclination is fixed on the support structure, and the dispensing structure setting is in the exit of the storage organization, for controlling
Sphere in storage organization falls one by one from exit.
Further, the storage organization includes flexible hose.
Further, the flexible hose includes corrugated flexible hose, is fixed in the shape of a spiral on the support structure.
Further, the support construction include upper plate, lower plate, setting several columns between the upper and lower plates,
Pipe for fixing and supporting the storage organization supports.
Further, the mounting hole and many places hollow-out part of pipe support are provided on the column.
Further, aluminum strip is selected in the pipe support, and intermediate portion is arranged with the mounting hole of mounting screw, by tightening spiral shell
Nail is fixed on column.
Further, the dispensing structure includes guide pipe, Bo Wan mechanism, power device, and the guide pipe setting exists
The support construction bottom and the outlet of connection storage organization, the Bo Wan mechanism is rotatably arranged at the outlet of the guide pipe
Place, the power device are located at the support construction bottom and are drivingly connected with the Bo Wan mechanism.
Further, the Bo Wan mechanism includes group bowl that can be rotated in guiding tube cavity, described group of bowl both ends
It is oppositely extended the swingle having across guiding tube wall, described dials the bowl structure that bowl is arc, the swingle
Free end be arranged in the support construction bottom and be located at guide pipe two sides bearing block by bearing rotation connection.
Further, the power device includes steering engine, the steering engine is horizontally fixed on the support construction bottom
Multi-purpose stand, shaft coupling, the output shaft of the steering engine is drivingly connected by shaft coupling and any swingle.
Further, the bearing is deep groove ball bearing.
Compared with the existing technology, the invention has the advantages that and technical effect:
1) present invention can accurately realize that single-shot is launched.
2) present invention is cleverly stored and is ranked up with corrugated flexible hose structure.
3) present invention innovatively realizes single-shot effect using group bowl structure.
4) present invention neatly in conjunction with the center of gravity of aircraft and is designed the lightweight of structure.
Detailed description of the invention
Fig. 1 is overall structure diagram of the embodiment of the present invention.
Fig. 2 is that the embodiment of the present invention launches structural schematic diagram.
Fig. 3 is to send out at A schematic diagram big in Fig. 2.
Fig. 4 is that the embodiment of the present invention launches detailed schematic of the structure in the state of dispensing.
Fig. 5 is that the embodiment of the present invention builds schematic diagram on board the aircraft.
It is as shown in the figure: the support of 1- pipe；2- upper plate；3- corrugated flexible hose；4- lower plate；5- guide pipe；6- column；7- round
Body；8- steering engine；9- multi-purpose stand；10- shaft coupling；11- bearing block；12- bearing；13- dials bowl.
Specific embodiment
For a better understanding of the invention, specific implementation of the invention is described further with reference to the accompanying drawing.
As depicted in figs. 1 and 2, a kind of unmanned plane hose loads single-shot delivery device, including launch structure, storage organization and
Support construction, the storage organization inclination is fixed on the support structure, and the dispensing structure setting is in the storage organization
Exit falls for controlling the sphere in storage organization from exit one by one.
Specifically, the support construction include upper plate 2, lower plate 4, be arranged between upper plate 2 and lower plate 4 four it is vertical
Column 6, the pipe for fixing and supporting the storage organization support 1.Be provided on the column 6 pipe support 1 mounting hole and
Many places hollow-out part mitigates self weight.
Aluminum strip is selected in the pipe support 1, and intermediate portion is arranged with the mounting hole of mounting screw, is fixed on by tightening screw
On column 6, the density of aluminum strip is small, light-weight.
The storage organization uses corrugated flexible hose 3, is fixed in the shape of a spiral on the support structure, for storing spherical object
7, it is located between upper plate 2 and lower plate 4, is supported and is fixed by pipe support 1.Wherein, the tail end of corrugated flexible hose 3 and guide pipe 5
It is attached.
The dispensing structure includes guide pipe 5, Bo Wan mechanism, power device, and the guide pipe 5 is arranged in the lower plate
4 bottoms and connection corrugated flexible hose 3 exports, the Bo Wan mechanism is rotatably arranged at the exit of the guide pipe 5, the power
Device is located at 4 bottom of lower plate and is drivingly connected with the Bo Wan mechanism.The Bo Wan mechanism includes can be in guide pipe 5
What is rotated in inner cavity dials bowl 13, and described group of bowl both ends, which are oppositely extended, the swingle across 5 tube wall of guide pipe, described
The bowl structure that bowl is arc is dialled, the free end of the swingle and setting in 4 bottom of lower plate and are located at 5 two sides of guide pipe
Bearing block 11 be rotatablely connected by bearing 12, the bearing 12 is deep groove ball bearing.The distance between bearing block 11 basis
The size for dialling bowl 13 carries out the selection of position.It is equipped with to meet in the guide pipe 5 and dials bowl 13 around the rotation of rotation rod axis rotation
Cavity makes when fall of ball to be in free falling body state.
As shown in Figures 2 and 3, the power device includes steering engine 8, the steering engine 8 is horizontally fixed on 4 bottom of lower plate
Multi-purpose stand 9, shaft coupling 10, the output shaft of the steering engine 8 is drivingly connected by shaft coupling 10 and any swingle, passed through
The given PWM of control terminal carries out the control of respective angles, so that steering engine 8 rotates.The multi-purpose stand 9 is fixed on lower plate 4
Bottom.
It is built on board the aircraft as shown in figure 5, the unmanned plane hose of the present embodiment can be loaded single-shot delivery device, it can
To facilitate the ball single-shot for realizing anywhere to launch, maneuverability, easy to operate, efficient quick.
As shown in figure 4, the unmanned plane hose of the present embodiment loads single-shot delivery device, when launching, steering engine 8 carries out 180 degree
Rotation realize and dial the rim of a bowl by being changed into vertically upward vertically upward, realize that a spherical object falls, next spherical object
It rests at the bottom of bowl for dialling bowl 13, group the rim of a bowl is waited to go back to.
The unmanned plane hose loads single-shot delivery device, and support construction part has hollow-out part, it can be achieved that entirety
Light weight effect.
The unmanned plane hose, which loads single-shot delivery device, makes the row that spherical object is orderly by using corrugated flexible hose 3
It is listed in hose, in a manner of first in first out, carries out the whereabouts of spherical object, realize that the single-shot one by one of spherical object is launched.
Embodiment of the present invention are not limited by the above embodiments, other any real without departing from spirit of the invention
The changes, modifications, substitutions, combinations, simplifications done under matter and principle, should be equivalent substitute mode, are included in the present invention
Protection scope within.
Claims (8)
1. a kind of unmanned plane hose loads single-shot delivery device, it is characterised in that: including launching structure, storage organization and support knot
Structure, the described storage organization inclination is fixed on the support structure, the dispensing structure setting in the exit of the storage organization,
It falls one by one for controlling the sphere in storage organization from exit；The dispensing structure includes guide pipe (5), dials bowl machine
Structure, power device, guide pipe (5) setting is in the support construction bottom and the outlet of connection storage organization, described group of bowl machine
Structure is rotatably arranged at the exit of the guide pipe (5), the power device be located at the support construction bottom and with it is described
Bo Wan mechanism is drivingly connected；The Bo Wan mechanism includes group bowl that can be rotated in guide pipe (5) inner cavity, described group of bowl two
End, which is oppositely extended, the swingle across guide pipe (5) tube wall, and described dials the bowl structure that bowl is arc, the rotation
The free end of bull stick and the bearing block (11) being arranged in the support construction bottom and positioned at guide pipe (5) two sides pass through bearing
(12) it is rotatablely connected.
2. unmanned plane hose according to claim 1 loads single-shot delivery device, it is characterised in that: the storage organization
Including flexible hose.
3. unmanned plane hose according to claim 2 loads single-shot delivery device, it is characterised in that: the flexible hose
Including corrugated flexible hose (3), fix in the shape of a spiral on the support structure.
4. unmanned plane hose according to claim 1 loads single-shot delivery device, it is characterised in that: the support construction
Including upper plate (2), lower plate (4), several columns (6) between upper plate (2) and lower plate (4) are set, for fixing and supporting
State the pipe support (1) of storage organization.
5. unmanned plane hose according to claim 4 loads single-shot delivery device, it is characterised in that: the column (6)
On be provided with pipe support (1) mounting hole and many places hollow-out part.
6. unmanned plane hose according to claim 5 loads single-shot delivery device, it is characterised in that: the pipe supports (1)
Aluminum strip is selected, intermediate portion is arranged with the mounting hole of mounting screw, is fixed on column (6) by tightening screw.
7. unmanned plane hose according to claim 1 loads single-shot delivery device, it is characterised in that: the power device
Multi-purpose stand (9), the shaft coupling of the support construction bottom are horizontally fixed on including steering engine (8), by the steering engine (8)
(10), the output shaft of the steering engine (8) is drivingly connected by shaft coupling (10) and any swingle.
8. unmanned plane hose according to claim 1 loads single-shot delivery device, it is characterised in that: the bearing (12)
For deep groove ball bearing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611057299.XA CN106477046B (en) | 2016-11-26 | 2016-11-26 | A kind of unmanned plane hose loading single-shot delivery device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611057299.XA CN106477046B (en) | 2016-11-26 | 2016-11-26 | A kind of unmanned plane hose loading single-shot delivery device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106477046A CN106477046A (en) | 2017-03-08 |
| CN106477046B true CN106477046B (en) | 2019-01-15 |
Family
ID=58274381
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611057299.XA Expired - Fee Related CN106477046B (en) | 2016-11-26 | 2016-11-26 | A kind of unmanned plane hose loading single-shot delivery device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106477046B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112693611B (en) * | 2020-12-31 | 2021-07-27 | 中国海洋大学 | Aerial mask putting machine capable of being carried by epidemic-resistant emergency unmanned aerial vehicle |
| CN112793784B (en) * | 2020-12-31 | 2022-05-17 | 中国海洋大学 | Can carry on multiple unmanned aerial vehicle platform of equipping combination execution difference duty |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5267501A (en) * | 1992-12-14 | 1993-12-07 | Shillig Vance R | R/C paint ball drop system |
| CN1569294A (en) * | 2004-03-29 | 2005-01-26 | 刘宝堂 | Football emitter |
| CN203556120U (en) * | 2013-11-29 | 2014-04-23 | 哈尔滨体育学院 | Automatic tennis ball serving machine |
| CH707436A1 (en) * | 2013-01-09 | 2014-07-15 | Fenaco Genossenschaft | Ball launcher. |
| CN105197244A (en) * | 2015-09-21 | 2015-12-30 | 江苏大学 | Biological control ball releasing device matched with airplane |
| CN105394025A (en) * | 2015-09-21 | 2016-03-16 | 江苏大学 | Degradable ball automatic dropping device used for unmanned plane |
| FR3027284A1 (en) * | 2014-10-17 | 2016-04-22 | Skeyelabs | AERIAL SPREADING DEVICE AND ASSOCIATED STEERING METHOD |
| CN206265310U (en) * | 2016-11-26 | 2017-06-20 | 华南理工大学 | A kind of unmanned plane flexible pipe loads single-shot delivery device |
-
2016
- 2016-11-26 CN CN201611057299.XA patent/CN106477046B/en not_active Expired - Fee Related
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5267501A (en) * | 1992-12-14 | 1993-12-07 | Shillig Vance R | R/C paint ball drop system |
| CN1569294A (en) * | 2004-03-29 | 2005-01-26 | 刘宝堂 | Football emitter |
| CH707436A1 (en) * | 2013-01-09 | 2014-07-15 | Fenaco Genossenschaft | Ball launcher. |
| CN203556120U (en) * | 2013-11-29 | 2014-04-23 | 哈尔滨体育学院 | Automatic tennis ball serving machine |
| FR3027284A1 (en) * | 2014-10-17 | 2016-04-22 | Skeyelabs | AERIAL SPREADING DEVICE AND ASSOCIATED STEERING METHOD |
| CN105197244A (en) * | 2015-09-21 | 2015-12-30 | 江苏大学 | Biological control ball releasing device matched with airplane |
| CN105394025A (en) * | 2015-09-21 | 2016-03-16 | 江苏大学 | Degradable ball automatic dropping device used for unmanned plane |
| CN206265310U (en) * | 2016-11-26 | 2017-06-20 | 华南理工大学 | A kind of unmanned plane flexible pipe loads single-shot delivery device |
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| Publication number | Publication date |
|---|---|
| CN106477046A (en) | 2017-03-08 |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190115 Termination date: 20211126 |
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| CF01 | Termination of patent right due to non-payment of annual fee |