CN106114861A - A kind of unmanned vehicle transports mechanism of jettisoninging - Google Patents
A kind of unmanned vehicle transports mechanism of jettisoninging Download PDFInfo
- Publication number
- CN106114861A CN106114861A CN201610703500.0A CN201610703500A CN106114861A CN 106114861 A CN106114861 A CN 106114861A CN 201610703500 A CN201610703500 A CN 201610703500A CN 106114861 A CN106114861 A CN 106114861A
- Authority
- CN
- China
- Prior art keywords
- telescopic shaft
- housing
- unmanned vehicle
- jettisoninging
- retention device
- 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.)
- Pending
Links
- 230000032258 transport Effects 0.000 title claims description 16
- 230000007246 mechanism Effects 0.000 title claims description 14
- 230000014759 maintenance of location Effects 0.000 claims abstract description 20
- 230000007723 transport mechanism Effects 0.000 claims abstract description 3
- 230000002708 enhancing effect Effects 0.000 claims description 8
- 230000015572 biosynthetic process Effects 0.000 claims description 4
- 238000010586 diagram Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 230000005484 gravity Effects 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000003187 abdominal effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 239000011435 rock Substances 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of unmanned vehicle and transport mechanism of jettisoninging, including the mounting bracket being fixed on below unmanned vehicle, mounting bracket is arranged with housing, the telescope motor being provided with telescopic shaft it is equipped with in mounting bracket, retention device it is further fixedly arranged in mounting bracket, grasping part is formed between telescopic shaft and retention device, described housing is by above-mentioned telescope motor, retention device is located at wherein, housing offers the mouth of stepping down communicated with grasping part, it is provided with for controlling telescope motor and receiving the electrical control gear of control signal in housing, it is provided with below housing for controlling electrical control gear energising or the power switch of power-off.It is unrestricted that the present invention has transport thing volume profiles, simple and reasonable, and stability is high, and manipulation is simple, it is simple to install, and lightweight size is little, it is simple to the advantage that aircraft carries, and applied range is practical.
Description
Technical field
The present invention relates to a kind of unmanned vehicle and transport mechanism of jettisoninging.
Background technology
Chinese patent CN201310715672 discloses " a kind of goods delivery device for depopulated helicopter ", and it passes through
Hang under unmanned plane abdominal part and fix a support, connected by rotary shaft between support and a loop bracket, loop bracket is placed
Have a spherical container, between the two, do not have fixed connection structure, spherical container loop bracket keep angle placed in the middle time due to
Gravity abuts against and realizes on loop bracket fixing, and rotates certain angle when needs are jettisoninged by rotary shaft Spin Control loop bracket
Degree, and then realize bracket and separate with spherical container, thus realize transporting thing and jettisoning.This similar means needs one standardized
Bracket and spherical container, the size and shape therefore transporting object is limited, and needs mechanism's integral-rotation, occupies camera head
Deng the space of other carry things, when aircraft throw in destination indefinite time because lacking the target recognition of video camera thus nothing
Method realizes remotely controlling and automatically controlling, and range of application limitation is bigger.
Summary of the invention
It is an object of the invention to provide a kind of simple and reasonable, stability is high, manipulation is simple, be easily installed, and weight
The light unmanned vehicle that size is little, be easy to aircraft carries transports mechanism of jettisoninging, and its transport thing volume profiles is unrestricted, applies model
Enclose wide, practical.
The technical scheme realizing the object of the invention is as follows:
A kind of unmanned vehicle transports mechanism of jettisoninging, and including the mounting bracket being fixed on below unmanned vehicle, installs and props up
Frame is arranged with housing, and mounting bracket is equipped with the telescope motor being provided with telescopic shaft, and mounting bracket is further fixedly arranged on resistance
Blocking means, forms grasping part between telescopic shaft and retention device, and above-mentioned telescope motor, retention device cover are set by described housing
Wherein, housing offers the mouth of stepping down communicated with grasping part, be provided with in housing for controlling telescope motor and connecing
Receive the electrical control gear of control signal, be provided with below housing for controlling electrical control gear energising or the power supply of power-off
Switch.
Further, described retention device stretching out in stroke at telescopic shaft.
Further, described telescopic shaft front end is fixedly installed an enhancing axle sleeve.
Further, the described axial line of enhancing axle sleeve overlaps with the axial line of telescopic shaft.
Further, described retention device includes disengaging plate, top board, forms above-mentioned clamping empty between disengaging plate and top board
Between, described telescopic shaft stretches in grasping part through disengaging plate.
Further, described disengaging plate offers the resigning hole passed for telescopic shaft.
Further, described top board is provided with the end for telescopic shaft and stretches into the spacing hole that formation is spacing.
Further, the fairlead extended in oriented housing being set at the stepping down mouthful of described housing or outside housing.
Have employed technique scheme, telescope motor and telescopic shaft fitted shaft realize hook loading with come off, motion
Stroke is short, and overall dimensions is little and activity space is little, does not affect the carry of camera head.Telescopic shaft stretches out travel position and is in stop
The side of device and form grasping part between, contacts clamping carry thing by telescopic shaft with the cooperation of retention device,
Realize the disengaging of telescopic shaft and retention device when telescopic shaft is retracted, carry thing drops under gravity because of unsettled.This
It is unrestricted that invention has transport thing volume profiles, simple and reasonable, and stability is high, and manipulation is simple, it is simple to installs, and lightweight
Size is little, it is simple to the advantage that aircraft carries, and applied range is practical.
Accompanying drawing explanation
Fig. 1 is the assembling schematic diagram of the present invention；
Fig. 2 is the schematic diagram that the present invention is assembled on unmanned plane during flying device；
Fig. 3 is the cut-away view of the present invention；
Fig. 4 is the telescopic shaft of the present invention structural representation through carry principle condition；
Fig. 5 is partial enlarged drawing at B in Fig. 4；
Fig. 6 is that telescopic shaft of the present invention stretches out the structural representation withstanding carry thing formation carry；
Fig. 7 is that telescopic shaft retraction carry thing of the present invention drops the schematic diagram of situation；
In accompanying drawing, 1 is mounting bracket, and 2 is housing, and 3 is telescope motor, and 4 is retention device, and 5 is grasping part, and 6 for allowing
Position mouth, 7 is electrical control gear, and 8 is power switch, and 9 is disengaging plate, and 10 is top board, and 11 is carry thing, and 12 for strengthening axle sleeve,
13 is resigning hole, and 14 is spacing hole, and 15 is fairlead, and 16 is cover plate, and 17 is telescopic shaft, and 18 is connecting plate, and 19 open for carry thing
Hole；
100 is unmanned vehicle.
Detailed description of the invention
For making the purpose of the embodiment of the present invention, technical scheme and advantage clearer, below in conjunction with the embodiment of the present invention
Accompanying drawing, the technical scheme of the embodiment of the present invention is clearly and completely described.Obviously, described embodiment is this
Bright a part of embodiment rather than whole embodiments.Based on described embodiments of the invention, ordinary skill
The every other embodiment that personnel are obtained on the premise of without creative work, broadly falls into the scope of protection of the invention.
Seeing Fig. 1,2,3, a kind of unmanned vehicle transports mechanism of jettisoninging, including being fixed on below unmanned vehicle 100
Mounting bracket 1, mounting bracket is arranged with housing 2, and mounting bracket is equipped with the Miniature retractable motor 3 being provided with telescopic shaft 17,
Large and middle size motor can certainly be selected, mounting bracket is further fixedly arranged on retention device 4, telescopic shaft and retention device it
Between formed grasping part 5, above-mentioned telescope motor, retention device are located at wherein, offer and clamp sky on housing by housing
Between the mouth 6 of stepping down that communicates, be provided with for controlling telescope motor and receiving the electrical control gear 7 of control signal in housing,
It is provided with below housing for controlling electrical control gear energising or the power switch 8 of power-off.Retention device stretching at telescopic shaft
Going out in stroke, retention device includes disengaging plate 9, top board 10, and the parts of one can be used between disengaging plate and top board to constitute or adopt
With connecting plate 18, both upper ends are attached integral, between disengaging plate and top board, form above-mentioned grasping part 5 for extension
The insertion of loading 11, carry thing can be gondola or transport pod etc. can object in partial insertion grasping part, telescopic shaft is worn
Cross disengaging plate to stretch in grasping part.Owing to Miniature retractable motor size is little, telescopic shaft is meticulous, for preventing carry thing overweight, leads
Causing telescopic shaft deform under a stretching force or rock, telescopic shaft front end is fixedly installed an enhancing axle sleeve 12, and strengthening axle sleeve can
With as desired to carry out choosing whether to use.In order to ensure the stability of transmission more accurately carry thing is clamped,
The axial line strengthening axle sleeve overlaps with the axial line of telescopic shaft.The resigning hole 13 passed for telescopic shaft is offered on disengaging plate.
It is provided with the end for telescopic shaft on top board and stretches into the spacing hole 14 that formation is spacing.It is provided with at the stepping down mouthful of housing
The fairlead 15 extended in housing or outside housing.This fairlead can withstand on disengaging plate and top board in upper end when being arranged in housing
Lower section, forms supporting, so can realize the guide effect that carry thing inserts, it is also possible to top board, disengaging plate is formed supporting,
Stability during ensureing clamping or departing from.In enforcement, it is provided above the lid that it is covered at Miniature retractable motor
Plate 16.
See Fig. 4,5, wherein, Fig. 4 showing, telescopic shaft extends through the situation of carry thing perforate 19, on telescopic shaft 17
Enhancing axle sleeve 12 contact through resigning hole 13, grasping part 5 and spacing hole 14 with top board 10, telescopic shaft 17 and enhancing axle sleeve 12
Compressing top board 10 under the thrust of micromachine 3, carry thing 11 is suspended on enhancing axle sleeve and telescopic shaft, disengaging plate and top
The effect rocked before and after clamping carry thing limits is played between plate.Disengaging plate stops carry thing to follow flexible when telescopic shaft is retracted
Axle is retracted.
Seeing Fig. 6, non-perforate on the carry thing in Fig. 6, telescopic shaft 17 stretches out the situation of clamping carry thing and is: strengthen axle sleeve
12 wear resigning hole 13, stretch into carry thing 11 is formed top clip shape by grasping part 5, telescopic shaft and strengthen axle sleeve and make at micromachine
Compressing top board 10 with lower promotion carry thing, when telescopic shaft runs into certain resistance, telescopic shaft stops stretching out, and carry thing presss from both sides in both sides
Realize under compaction forces effect hanging fixing.
Fig. 7 is the schematic diagram of telescopic shaft retracted mode, the situation that carry thing drops voluntarily, specifies sheet to throw when aircraft arrives
When throwing position, telescopic shaft 17 is retracted under micromachine 3 acts on automatically, and disengaging plate stops carry thing to be followed when telescopic shaft is retracted
Telescopic shaft is retracted, and carry thing drops under gravity.
Claims (8)
1. unmanned vehicle transport is jettisoninged mechanism, it is characterised in that this transport mechanism of jettisoninging includes being fixed on unmanned flight
Mounting bracket below device, mounting bracket is arranged with housing, and mounting bracket is equipped with the telescope motor being provided with telescopic shaft, peace
Being further fixedly arranged on retention device on dress support, form grasping part between telescopic shaft and retention device, described housing is by upper
State telescope motor, retention device is located at wherein, offers the mouth of stepping down communicated with grasping part on housing, arranges in housing
Have for controlling telescope motor and receiving the electrical control gear of control signal, be provided with below housing for controlling electric-controlled
Device processed energising or the power switch of power-off.
A kind of unmanned vehicle the most according to claim 1 transports mechanism of jettisoninging, it is characterised in that described retention device exists
Stretching out in stroke of telescopic shaft.
A kind of unmanned vehicle the most according to claim 1 and 2 transports mechanism of jettisoninging, it is characterised in that described telescopic shaft
Front end is fixedly installed an enhancing axle sleeve.
A kind of unmanned vehicle the most according to claim 3 transports mechanism of jettisoninging, it is characterised in that described enhancing axle sleeve
Axial line overlaps with the axial line of telescopic shaft.
A kind of unmanned vehicle the most according to claim 1 transports mechanism of jettisoninging, it is characterised in that described retention device bag
Including disengaging plate, top board, form above-mentioned grasping part between disengaging plate and top board, described telescopic shaft stretches into clamping through disengaging plate
In space.
A kind of unmanned vehicle the most according to claim 5 transports mechanism of jettisoninging, it is characterised in that open on described disengaging plate
It is provided with the resigning hole passed for telescopic shaft.
7. transport, according to a kind of unmanned vehicle described in claim 5-6, mechanism of jettisoninging, it is characterised in that preferably, described
It is provided with the end for telescopic shaft on top board and stretches into the spacing hole that formation is spacing.
8. transport, according to a kind of unmanned vehicle described in claim 1 or 2 or 5 or 6, mechanism of jettisoninging, it is characterised in that described
The fairlead extended in oriented housing is set at the stepping down mouthful of housing or outside housing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610703500.0A CN106114861A (en) | 2016-08-22 | 2016-08-22 | A kind of unmanned vehicle transports mechanism of jettisoninging |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610703500.0A CN106114861A (en) | 2016-08-22 | 2016-08-22 | A kind of unmanned vehicle transports mechanism of jettisoninging |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106114861A true CN106114861A (en) | 2016-11-16 |
Family
ID=57273632
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610703500.0A Pending CN106114861A (en) | 2016-08-22 | 2016-08-22 | A kind of unmanned vehicle transports mechanism of jettisoninging |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106114861A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107434041A (en) * | 2017-08-08 | 2017-12-05 | 深圳市科卫泰实业发展有限公司 | A kind of more carry throwing devices |
| CN108382597A (en) * | 2018-04-18 | 2018-08-10 | 上海唯成电子科技有限公司 | Universal unmanned plane article delivery device |
| CN109987227A (en) * | 2017-12-30 | 2019-07-09 | 广州刀锋智能科技有限公司 | A kind of goods and materials jettison system based on unmanned plane |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4399968A (en) * | 1980-05-16 | 1983-08-23 | Rockwell International Corporation | Controlled output force actuator |
| US6666351B1 (en) * | 2002-01-03 | 2003-12-23 | Raytheon Company | Dispenser structure for chaff countermeasures |
| CN104097773A (en) * | 2014-06-13 | 2014-10-15 | 芜湖特源鑫复合材料科技有限公司 | Multi-rotor-wing aircraft for dropping goods and materials |
| CN105644786A (en) * | 2015-12-30 | 2016-06-08 | 北京航空航天大学 | Micro unmanned plane throwing device |
| CN206050078U (en) * | 2016-08-22 | 2017-03-29 | 北京朗森基科技发展有限公司 | A kind of unmanned vehicle transports mechanism of jettisoninging |
-
2016
- 2016-08-22 CN CN201610703500.0A patent/CN106114861A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4399968A (en) * | 1980-05-16 | 1983-08-23 | Rockwell International Corporation | Controlled output force actuator |
| US6666351B1 (en) * | 2002-01-03 | 2003-12-23 | Raytheon Company | Dispenser structure for chaff countermeasures |
| CN104097773A (en) * | 2014-06-13 | 2014-10-15 | 芜湖特源鑫复合材料科技有限公司 | Multi-rotor-wing aircraft for dropping goods and materials |
| CN105644786A (en) * | 2015-12-30 | 2016-06-08 | 北京航空航天大学 | Micro unmanned plane throwing device |
| CN206050078U (en) * | 2016-08-22 | 2017-03-29 | 北京朗森基科技发展有限公司 | A kind of unmanned vehicle transports mechanism of jettisoninging |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107434041A (en) * | 2017-08-08 | 2017-12-05 | 深圳市科卫泰实业发展有限公司 | A kind of more carry throwing devices |
| CN109987227A (en) * | 2017-12-30 | 2019-07-09 | 广州刀锋智能科技有限公司 | A kind of goods and materials jettison system based on unmanned plane |
| CN108382597A (en) * | 2018-04-18 | 2018-08-10 | 上海唯成电子科技有限公司 | Universal unmanned plane article delivery device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106114861A (en) | A kind of unmanned vehicle transports mechanism of jettisoninging | |
| KR101947335B1 (en) | Coaxial double propeller double-motor aircraft | |
| CN203793657U (en) | Take-off assisting device for fixed-wing unmanned aerial vehicle | |
| CN207045661U (en) | Eight rotor plant protection unmanned planes and its flying wing arm knob are disassembled | |
| CN107792348B (en) | Auxiliary device rises and falls based on wireless battery charging outfit of unmanned aerial vehicle | |
| CN207157451U (en) | A kind of water life-saving unmanned plane | |
| CN110901913B (en) | Unmanned aerial vehicle control system based on intelligent device is controlled | |
| CA3137585C (en) | Aircraft retrieval system and method | |
| CN206050078U (en) | A kind of unmanned vehicle transports mechanism of jettisoninging | |
| CN201108745Y (en) | Power kite | |
| CN208760913U (en) | A kind of camera fixing device for unmanned plane | |
| CN210882549U (en) | Rescue unmanned aerial vehicle on water | |
| CN108408038A (en) | It is capable mechanical to sending the magnetic spring operation for connecing article suspension to float in the air | |
| CN206501993U (en) | A kind of lifebuoy is jettisoninged carry and unmanned plane | |
| CN207173966U (en) | Hovering and flight instruments | |
| CN211468795U (en) | Unmanned aerial vehicle with couple | |
| CN213502887U (en) | Unmanned aerial vehicle flight platform capable of accurately throwing aerial materials | |
| CN208325613U (en) | A kind of aerial photography aircraft can be improved landing safety | |
| CN206059621U (en) | A kind of unmanned plane gps antenna can folding and unfolding mounting structure | |
| US2778611A (en) | System for aerial pick-up from surface vessels | |
| CN213620225U (en) | Air capture net throwing type unmanned aerial vehicle | |
| CN216035130U (en) | Unmanned aerial vehicle pickup attachment | |
| CN110271670B (en) | Water area rescue unmanned aerial vehicle and life buoy carrying device thereof | |
| CN210707900U (en) | A goods and materials air transportation device for animal husbandry | |
| CN202093303U (en) | Camera suspension device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161116 |
|
| RJ01 | Rejection of invention patent application after publication |