CN106477046A - A kind of unmanned plane flexible pipe loads single-shot delivery device - Google Patents
A kind of unmanned plane flexible pipe loads single-shot delivery device Download PDFInfo
- Publication number
- CN106477046A CN106477046A CN201611057299.XA CN201611057299A CN106477046A CN 106477046 A CN106477046 A CN 106477046A CN 201611057299 A CN201611057299 A CN 201611057299A CN 106477046 A CN106477046 A CN 106477046A
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- CN
- China
- Prior art keywords
- delivery device
- unmanned plane
- storage organization
- flexible pipe
- shot delivery
- 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.)
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Links
- 230000008520 organization Effects 0.000 claims abstract description 23
- 238000010276 construction Methods 0.000 claims abstract description 14
- 230000007246 mechanism Effects 0.000 claims abstract description 13
- 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
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000000386 athletic effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 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
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
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- 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 flexible pipe loads single-shot delivery device, including input structure, storage organization and supporting construction, described storage organization tilts to be fixed on the support structure, described input structure setting in the exit of described storage organization, for controlling the spheroid in storage organization to fall one by one from exit.Described storage organization includes flexible hose；Described supporting construction include upper plate, lower plate, setting some columns between the upper and lower plates, for fixing and supporting the pipe of described storage organization to support.Described input structure includes guide pipe (5), Bo Wan mechanism, power set.The present invention drives, by steering wheel, the rotation dialling bowl, realizes spheroid and falls one by one, and the incline structure in conjunction with corrugated flexible hose is so that the orderly landing of spheroid.
Description
Technical field
The present invention relates to a kind of delivery device, more particularly, to a kind of unmanned plane flexible pipe loading single-shot delivery device, mainly
Throw in the input that the delivery device in field, especially athletic competition and goods and materials transport for unmanned plane.
Background technology
At present, existing delivery device, typically all tilts to allow spherical object to lean on self gravitation to glide and throws in or round
Body at grade, then carries out opening one by one and throws in.The precision dropping so cannot be guaranteed, simultaneously delivery device
Running complexity is it is impossible to quickly make spherical object be dropped one by one in same position.
Content of the invention
It is an object of the invention to solve the problems, such as how the short time one by one by round body drop in same position,
Improve the efficiency thrown in and precision, provide a kind of unmanned plane flexible pipe to load single-shot delivery device.
Solve the problems, such as quickly spherical object to fall one by one in same position.
The purpose of the present invention is achieved through the following technical solutions：
A kind of unmanned plane flexible pipe loads single-shot delivery device, includes input structure, storage organization and supporting construction, described storage
Structures slope is fixing on the support structure, and described input structure setting, in the exit of described storage organization, stores for controlling
Spheroid in structure falls one by one from exit.
Further, described storage organization includes flexible hose.
Further, described flexible hose includes corrugated flexible hose, fixes on the support structure in the shape of a spiral.
Further, described supporting construction include upper plate, lower plate, setting some columns between the upper and lower plates,
Pipe for fixing and supporting described storage organization supports.
Further, described column is provided with installing hole and the many places openwork part of pipe support.
Further, described pipe supports and selects aluminum strip, and intermediate portion is arranged with the installing hole of mounting screw, by tightening spiral shell
Nail is fixed on column.
Further, described input structure includes guide pipe, Bo Wan mechanism, power set, and described guide pipe is arranged on
Described supporting construction bottom and connection storage organization outlet, described Bo Wan mechanism is rotatably arranged at the outlet of described guide pipe
Place, described power set be located at described supporting construction bottom and with described Bo Wan mechanism drive connection.
Further, described Bo Wan mechanism includes group bowl that can rotate in guiding tube cavity, described group of bowl two ends
Oppositely it is extended the swingle having through guiding tube wall, described dials the bowl structure that bowl is arc, described swingle
Free end be arranged on described supporting construction bottom and be located at guide pipe both sides bearing block pass through bearing rotation be connected.
Further, described power set include steering wheel, described steering wheel are horizontally fixed on described supporting construction bottom
Multiple bay, shaft coupling, the output shaft of described steering wheel passes through shaft coupling and arbitrary swingle drive connection.
Further, described bearing is deep groove ball bearing.
With respect to prior art, the invention has the advantages that and technique effect：
1）The present invention can accurately realize single-shot and throw in.
2）The present invention is cleverly stored with corrugated flexible hose structure and is ranked up.
3）The present invention innovatively realizes single-shot effect using group bowl structure.
4）Neatly the center of gravity with reference to aircraft and the lightweight to structure are designed the present invention.
Brief description
Fig. 1 is embodiment of the present invention overall structure diagram.
Fig. 2 throws in structural representation for the embodiment of the present invention.
Fig. 3 is to send out at A in Fig. 2 schematic diagram big.
Fig. 4 throws in the detailed schematic in the state of input for the structure for the embodiment of the present invention.
Fig. 5 builds schematic diagram on board the aircraft for the embodiment of the present invention.
Shown in figure：1- pipe supports；2- upper plate；3- corrugated flexible hose；4- lower plate；5- guide pipe；6- column；7- round
Body；8- steering wheel；9- multiple bay；10- shaft coupling；11- bearing block；12- bearing；13- dials bowl.
Specific embodiment
For more fully understanding the present invention, below in conjunction with the accompanying drawings to the present invention be embodied as be described further.
As depicted in figs. 1 and 2, a kind of unmanned plane flexible pipe loads single-shot delivery device, include input structure, storage organization and
Supporting construction, described storage organization tilts to be fixed on the support structure, and described input structure setting is in described storage organization
Exit, for controlling the spheroid in storage organization to fall one by one from exit.
Specifically, described supporting construction include upper plate 2, lower plate 4, be arranged between upper plate 2 and lower plate 4 four stand
Post 6, the pipe support 1 for fixing and supporting described storage organization.Be provided with described column 6 pipe support 1 installing hole and
Many places openwork part, mitigates deadweight.
Described pipe supports 1 to select aluminum strip, and intermediate portion is arranged with the installing hole of mounting screw, is fixed on by tightening screw
On column 6, the density of aluminum strip is little, lightweight.
Described storage organization adopts corrugated flexible hose 3, fixes on the support structure in the shape of a spiral, for storing spherical object
7, it is located between upper plate 2 and lower plate 4, supported 1 to be supported and fixed by pipe.Wherein, the tail end of corrugated flexible hose 3 and guide pipe 5
It is attached.
Described input structure includes guide pipe 5, Bo Wan mechanism, power set, and described guide pipe 5 is arranged on described lower plate
4 bottoms and connect corrugated flexible hose 3 export, described Bo Wan mechanism is rotatably arranged at the exit of described guide pipe 5, described power
Device be located at described lower plate 4 bottom and with described Bo Wan mechanism drive connection.Described Bo Wan mechanism includes can be in guide pipe 5
Group bowl 13 of rotation in inner chamber, described group of bowl two ends are oppositely extended the swingle having through guide pipe 5 tube wall, described
Dial bowl be arc bowl structure, the free end of described swingle be arranged on described lower plate 4 bottom and be located at guide pipe 5 both sides
Bearing block 11 pass through bearing 12 and rotate to connect, described bearing 12 is deep groove ball bearing.The distance between bearing block 11 basis
The size dialling bowl 13 carries out the selection of position.It is provided with described guide pipe 5 and meet the rotation dialling bowl 13 around rotation rod axis rotation
Cavity, makes to be in free falling body state during fall of ball.
As shown in Figures 2 and 3, described power set include steering wheel 8, described steering wheel 8 are horizontally fixed on lower plate 4 bottom
Multiple bay 9, shaft coupling 10, the output shaft of described steering wheel 8 passes through shaft coupling 10 and arbitrary swingle drive connection, passes through
The PWM that control end gives carries out the control of respective angles so that steering wheel 8 rotates.Described multiple bay 9 is fixed on lower plate 4
Bottom.
As shown in figure 5, the unmanned plane flexible pipe of the present embodiment can be loaded single-shot delivery device building on board the aircraft, can
To facilitate the ball single-shot realizing anywhere to throw in, maneuverability, easy to operate, efficient quick.
As shown in figure 4, the unmanned plane flexible pipe of the present embodiment loads single-shot delivery device, when throwing in, steering wheel 8 carries out 180 degree
Rotation realize dialling the rim of a bowl by being changed into vertically upward vertically upward, realize spherical object, next spherical object
Rest on the bowl bottom dialling bowl 13, wait group the rim of a bowl to go back to.
Described unmanned plane flexible pipe loads single-shot delivery device, and supporting construction partly all has openwork part, can achieve overall
Light weight effect.
Described unmanned plane flexible pipe loads single-shot delivery device, by using corrugated flexible hose 3, making the row that spherical object is orderly
It is listed in flexible pipe, in the way of first in first out, carries out the whereabouts of spherical object, the single-shot one by one realizing spherical object is thrown in.
Embodiments of the present invention are simultaneously not restricted to the described embodiments, and other any spirit without departing from the present invention are real
Matter and the change made under principle, modification, replacement, combine, simplify, all should be equivalent substitute mode, be included in the present invention
Protection domain within.
Claims (10)
1. a kind of unmanned plane flexible pipe load single-shot delivery device it is characterised in that：Tie including throwing in structure, storage organization and support
Structure, described storage organization tilt fixing on the support structure, described input structure setting in the exit of described storage organization,
For controlling the spheroid in storage organization to fall one by one from exit.
2. unmanned plane flexible pipe according to claim 1 load single-shot delivery device it is characterised in that：Described storage organization
Including flexible hose.
3. unmanned plane flexible pipe according to claim 2 load single-shot delivery device it is characterised in that：Described flexible hose
Including corrugated flexible hose (3), fix in the shape of a spiral on the support structure.
4. unmanned plane flexible pipe according to claim 1 load single-shot delivery device it is characterised in that：Described supporting construction
Including upper plate (2), lower plate (4), some columns (6) being arranged between upper plate (2) and lower plate (4), it is used for fixing and support institute
The pipe stating storage organization supports (1).
5. unmanned plane flexible pipe according to claim 4 load single-shot delivery device it is characterised in that：Described column (6)
On be provided with pipe and support the installing hole of (1) and many places openwork part.
6. unmanned plane flexible pipe according to claim 5 load single-shot delivery device it is characterised in that：Described pipe supports (1)
From aluminum strip, intermediate portion is arranged with the installing hole of mounting screw, is fixed on column (6) by tightening screw.
7. unmanned plane flexible pipe according to claim 1 load single-shot delivery device it is characterised in that：Described input structure
Including guide pipe (5), Bo Wan mechanism, power set, described guide pipe (5) is arranged on described supporting construction bottom and connects storage
Structure exports, and described Bo Wan mechanism is rotatably arranged at the exit of described guide pipe (5), and described power set are located at described
Support structure bottom and with described Bo Wan mechanism drive connection.
8. unmanned plane flexible pipe according to claim 7 load single-shot delivery device it is characterised in that：Described Bo Wan mechanism
Including the bowl of dialling that can rotate in guide pipe (5) inner chamber, described group of bowl two ends are oppositely extended to be had through guide pipe (5)
The swingle of tube wall, described dials the bowl structure that bowl is arc, and the free end of described swingle is tied with being arranged on described support
Structure bottom and be located at guide pipe (5) both sides bearing block (11) pass through bearing (12) rotate connect.
9. unmanned plane flexible pipe according to claim 8 load single-shot delivery device it is characterised in that：Described power set
It is horizontally fixed on multiple bay (9), the shaft coupling of described supporting construction bottom including steering wheel (8), by described steering wheel (8)
(10), the output shaft of described steering wheel (8) passes through shaft coupling (10) and arbitrary swingle drive connection.
10. unmanned plane flexible pipe according to claim 8 load single-shot delivery device it is characterised in that：Described bearing
(12) it is 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 true CN106477046A (en) | 2017-03-08 |
| CN106477046B 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) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112693611A (en) * | 2020-12-31 | 2021-04-23 | 中国海洋大学 | Aerial mask putting machine capable of being carried by epidemic-resistant emergency unmanned aerial vehicle |
| CN112793784A (en) * | 2020-12-31 | 2021-05-14 | 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 |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112693611A (en) * | 2020-12-31 | 2021-04-23 | 中国海洋大学 | Aerial mask putting machine capable of being carried by epidemic-resistant emergency unmanned aerial vehicle |
| CN112793784A (en) * | 2020-12-31 | 2021-05-14 | 中国海洋大学 | Can carry on multiple unmanned aerial vehicle platform of equipping combination execution difference duty |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106477046B (en) | 2019-01-15 |
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| SE01 | Entry into force of request for substantive examination | ||
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190115 Termination date: 20211126 |