CN108116690A - Unmanned plane emitter - Google Patents
Unmanned plane emitter Download PDFInfo
- Publication number
- CN108116690A CN108116690A CN201711396706.4A CN201711396706A CN108116690A CN 108116690 A CN108116690 A CN 108116690A CN 201711396706 A CN201711396706 A CN 201711396706A CN 108116690 A CN108116690 A CN 108116690A
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- China
- Prior art keywords
- flat pad
- unmanned plane
- inclined plate
- transmitting
- turntable
- 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.)
- Granted
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 27
- 230000007246 mechanism Effects 0.000 claims abstract description 21
- 230000005540 biological transmission Effects 0.000 claims description 5
- 239000000463 material Substances 0.000 claims description 4
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 claims description 3
- 210000002421 cell wall Anatomy 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims 1
- 238000000034 method Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
Unmanned plane emitter, including flat pad, turntable and transmitting pedestal, the bottom of transmitting pedestal is set there are four traveling wheel, turntable is rotatably connected on transmitting pedestal upper surface by thrust bearing, equipped with hydraulic station and for driving the revolving power mechanism that turntable rotates in transmitting pedestal, the length direction of flat pad is set along the longitudinal direction, the bottom rear of flat pad is hinged on the rear side of turntable, lifting cylinder is hinged between the front side bottom of flat pad and the front side of turntable, flat pad is equipped with transmitting pushing mechanism, the rear side of flat pad is equipped with folded sheet auxiliary body；In conclusion the configuration of the present invention is simple, design are reasonable, at low cost, wherein hydraulic motor provides power source, is driven to drive taking off for unmanned plane by chain structure, and guarantee is provided for smoothly taking off for modern unmanned plane.
Description
Technical field
The invention belongs to unmanned air vehicle technique fields, and in particular to a kind of unmanned plane emitter.
Background technology
Unmanned plane is the abbreviation of " UAV ", relies primarily on wireless remotecontrol or by the side such as automatic pilot
Formula realizes autonomous control flight.It is one of current advanced technological arms, is widely used in battle reconnaissance, electronic countermeasure, sky
Many military operations such as middle strike are known as the " prying eyes " and " trump card " of modern battlefield.At present, China UAV emission systems
Mainly using the modes such as hydraulic pressure, pneumatic, rocket assist, but these types of radiation pattern there is complicated, manufacture use into
The problem of this height, maintenance is difficult.
The content of the invention
The present invention provides a kind of simple in structure, at low cost, operation side of manufacture to solve shortcoming of the prior art
Just unmanned plane emitter.
In order to solve the above technical problems, the present invention adopts the following technical scheme that：Unmanned plane emitter is flat including emitting
Platform, turntable and transmitting pedestal, the bottom for emitting pedestal are set there are four traveling wheel, and turntable is rotatably connected on by thrust bearing
Emit pedestal upper surface, hydraulic station is equipped in transmitting pedestal and for driving the revolving power mechanism that turntable rotates, transmitting is flat
The length direction of platform is set along the longitudinal direction, and the bottom rear of flat pad is hinged on the rear side of turntable, before flat pad
Lifting cylinder is hinged between side bottom and the front side of turntable, flat pad is equipped with transmitting pushing mechanism, flat pad
Rear side is equipped with folded sheet auxiliary body, and hydraulic station is auxiliary by oil pipe and lifting cylinder, transmitting pushing mechanism and folded sheet respectively
Mechanism is helped to connect.
Revolving power mechanism includes the stepper motor being arranged in transmitting pedestal, and the main shaft of stepper motor is equipped with master tape
It takes turns, the column spinner that fixed own centre line is arranged in vertical at the bottom centre of turntable, the lower end of column spinner passes through hair
Pedestal upper surface is penetrated to extend into transmitting pedestal, the lower end of column spinner is equipped with from belt wheel, main pulley by transmission belt with from band
Wheel is sequentially connected.
The upper surface of flat pad offers the pilot hole that takes off along its length, transmitting pushing mechanism include hydraulic motor,
Gearbox and two sprocket wheels, one of sprocket wheel are rotatably connected on the rear interior of flat pad, another sprocket wheel, which rotates, to be connected
The front interior of flat pad is connected on, is connected between two sprocket wheels by chain drive, chain is parallel to be located at the pilot hole that takes off
Underface, the main shaft of hydraulic motor are sequentially connected by gearbox and one of sprocket wheel, and hydraulic station passes through oil pipe and hydraulic pressure horse
Up to connection, traction component is installed on chain；
Two groups of limit switches are additionally provided in flat pad, two groups of limit switches are separately positioned on the front end for the pilot hole that takes off with after
End, two groups of limit switches are connected by circuit with hydraulic motor.
Traction component includes mounting bracket and guiding piece, and mounting bracket is assemblied in the upper half range of chain, and the longitudinal section of guiding piece is
Right angled triangle, the right angle of guiding piece are hinged on the forward upper of mounting bracket by axis pin, and the center line of axis pin is along left and right water
Square to setting, guiding piece, which is upward through, to take off pilot hole and protrudes from flat pad upper surface, and the leading flank of guiding piece is vertical
In flat pad upper surface, the rear lateral portion weight of guiding piece is more than the front side portion weight of guiding piece, and the leading flank of guiding piece opens up
There is groove.
Guiding piece is made of ferrous material, and the rear lateral portion of mounting bracket is equipped with magnet.
Folded sheet auxiliary body includes the first inclined plate and the second inclined plate, and the first inclined plate and the second inclined plate incline in low after preceding height
Tiltedly setting, the front side edge of the first inclined plate is fixed there are two the first hinge sleeve, and the back side edge of flat pad is fixed with the second hinge sleeve, and second
The center line of hinge sleeve and two the first hinge sleeves is set along left and right horizontal direction, the second hinge sleeve be located at two the first hinge sleeves it
Between, it is equipped with the first articulated shaft in the second hinge sleeve and two the first hinge sleeves；The bottom rear of first inclined plate is fixed with the 3rd hinge
The center line of set, the 4th hinge sleeve that there are two the front side edge fixations of the second inclined plate, the 3rd hinge sleeve and two the 4th hinge sleeves is along a left side
Right horizontally arranged, the 3rd hinge sleeve is located between two the 4th hinge sleeves, is equipped in the 3rd hinge sleeve with two the 4th hinge sleeves
Second articulated shaft；The rear lateral portion of first inclined plate is ramp structure.
The bottom surface of second inclined plate is opened up there are two accommodating groove, and two accommodating grooves or so are arranged side by side and the length of each accommodating groove
It is consistent with the length direction of the second inclined plate to spend direction, hydraulic pressure support component is equipped in each accommodating groove, hydraulic pressure support component includes
Support cylinder, the cylinder ends of support cylinder are hinged on the front side of accommodating groove, and the piston rod end of support cylinder is hinged with backing plate.
Mounting groove is offered on the downside of the rear end portion of second inclined plate, shop bolt, one end of shop bolt are equipped in mounting groove
It is hinged on the front side cell wall of mounting groove.
Above-mentioned technical proposal is used, the invention has the advantages that：
（1）, the present invention launch angle and launch azimuth of unmanned plane can be adjusted, to adapt to different transmitting items
Part wherein when adjusting unmanned plane launch azimuth, starts stepper motor, and stepper motor drives main pulley to rotate, and main pulley passes through
Transmission belt is driven from belt wheel, and so as to which column spinner rotates under the drive from belt wheel, turntable starts to rotate, when turntable turns to
During orientation to be launched, stepper motor is stopped；When needing to adjust unmanned plane launch angle, start lifting cylinder, lifting oil
The piston rod of cylinder stretches out and props up the front side portion of flat pad, when flat pad is propped up to launch angle, lifting cylinder
It is stopped；
（2）, the present invention devise a kind of folded sheet auxiliary body, it is flat that unmanned plane need to push to transmitting by folded sheet auxiliary body
The rear side of platform could realize that unmanned plane works in the launch of flat pad, wherein folded sheet auxiliary machine need not used
During structure, folded sheet auxiliary body can fold up and be placed on flat pad upper surface, and due to folded sheet, auxiliary body can
It folds, reduces the volume of whole device, it is easy to use convenient for storage；
（3）, the present invention by emitting pushing mechanism unmanned plane is promoted to take off, wherein hydraulic motor provides enough power and leads to
Cross gearbox speed change, then through chain structure drive unmanned plane start, in addition hydraulic motor can pass through gearbox accelerate so as to
So that the slewing rate of output is faster；
（4）, the second inclined plate rear end portion be equipped with shop bolt, shop bolt is prevented in nothing for being positioned to the second inclined plate
In man-machine emission process, transmitting pedestal moves backward.
In conclusion the configuration of the present invention is simple, design are reasonable, at low cost, wherein hydraulic motor provides power source, by chain
Structure driven provides guarantee so as to drive taking off for unmanned plane, for smoothly taking off for modern unmanned plane.
Description of the drawings
Fig. 1 is the structure diagram of the present invention；
Fig. 2 is the top view of flat pad；
Fig. 3 is the working state figure of traction component；
Fig. 4 is view when folded sheet auxiliary body folds；
Fig. 5 is view when the second inclined plate is opened in Fig. 4；
Fig. 6 is the top view of Fig. 5.
Specific embodiment
As shown in figures 1 to 6, unmanned plane emitter of the invention including flat pad 1, turntable 2 and emits pedestal 3,
The bottom of transmitting pedestal 3 is set there are four traveling wheel 4, and turntable 2 is rotatably connected on 3 upper surface of transmitting pedestal by thrust bearing 5,
Equipped with hydraulic station 6 and for driving the revolving power mechanism that turntable 2 rotates, the length direction of flat pad 1 in transmitting pedestal 3
It sets along the longitudinal direction, the bottom rear of flat pad 1 is hinged on the rear side of turntable 2, front side bottom and the rotation of flat pad 1
Lifting cylinder 7 is hinged between the front side of turntable 2, flat pad 1 is equipped with transmitting pushing mechanism, and the rear side of flat pad 1 is set
There is folded sheet auxiliary body, hydraulic station 6 passes through oil pipe and lifting cylinder 7, transmitting pushing mechanism and folded sheet auxiliary machine respectively
Structure connects.
Revolving power mechanism includes the stepper motor 8 being arranged in transmitting pedestal 3, and the main shaft of stepper motor 8 is equipped with master
Belt wheel, the column spinner 10 that fixed own centre line is arranged in vertical at the bottom centre of turntable 2, the lower end of column spinner 10
It is extend into through 3 upper surface of transmitting pedestal in transmitting pedestal 3, the lower end of column spinner 10 is equipped with from belt wheel 11, and main pulley passes through
Transmission belt 12 from belt wheel 11 with being sequentially connected.
The upper surface of flat pad 1 offers the pilot hole 13 that takes off along its length, and transmitting pushing mechanism includes hydraulic pressure horse
It reaches, gearbox and two sprocket wheels 14, one of sprocket wheel 14 are rotatably connected on the rear interior of flat pad 1, another chain
Wheel 14 is rotatably connected on the front interior of flat pad 1, is sequentially connected between two sprocket wheels 14 by chain 15, chain 15 is parallel
Positioned at the underface for the pilot hole 13 that takes off, the main shaft of hydraulic motor is sequentially connected by gearbox and one of sprocket wheel 14, liquid
Pressure station 6 is connected by oil pipe with hydraulic motor, and traction component is equipped on chain 15；
Be additionally provided with two groups of limit switches in flat pad 1, two groups of limit switches be separately positioned on the pilot hole 13 that takes off front end and
Rear end, two groups of limit switches are connected by circuit with hydraulic motor.
Traction component includes mounting bracket 16 and guiding piece 17, and mounting bracket 16 is assemblied in the upper half range of chain 15, guiding piece 17
Longitudinal section for right angled triangle, the right angle of guiding piece 17 is hinged on the forward upper of mounting bracket 16, axis pin by axis pin 18
18 center line is set along left and right horizontal direction, and guiding piece 17 is upward through to take off and pilot hole 13 and protrude from flat pad 1
Surface, for the leading flank of guiding piece 17 perpendicular to 1 upper surface of flat pad, the rear lateral portion weight of guiding piece 17 is more than guiding piece 17
Front side portion weight, the leading flank of guiding piece 17 offer groove 19.
Guiding piece 17 is made of ferrous material, and the rear lateral portion of mounting bracket 16 is equipped with magnet 20.
Folded sheet auxiliary body includes the first inclined plate 21 and the second inclined plate 22, before the first inclined plate 21 and the second inclined plate 22 are in
Low dip is set after height, and the front side edge of the first inclined plate 21 is fixed there are two the first hinge sleeve 23, and the back side edge of flat pad 1 is fixed with
The center line of second hinge sleeve 24, the second hinge sleeve 24 and two the first hinge sleeves 23 is set along left and right horizontal direction, the second hinge sleeve
24 are located between two the first hinge sleeves 23, and the first articulated shaft 32 is equipped in the second hinge sleeve 24 and two the first hinge sleeves 23；The
The bottom rear of one inclined plate 21 is fixed with the 3rd hinge sleeve 25, and the front side edge of the second inclined plate 22 is fixed there are two the 4th hinge sleeve 26, the
The center line of three hinge sleeves 25 and two the 4th hinge sleeves 26 is set along left and right horizontal direction, and the 3rd hinge sleeve 25 is located at two the 4th
Between hinge sleeve 26, the second articulated shaft 33 is equipped in the 3rd hinge sleeve 25 and two the 4th hinge sleeves 26；The rear side of first inclined plate 21
Portion is ramp structure.
The bottom surface of second inclined plate 22 is opened up there are two accommodating groove 27, and two accommodating grooves 27 or so are arranged side by side and each store
The length direction of slot 27 is consistent with the length direction of the second inclined plate 22, and hydraulic pressure support component, hydraulic pressure are equipped in each accommodating groove 27
Support component includes support cylinder 28, and the cylinder ends of support cylinder 28 are hinged on the front side of accommodating groove 27, support cylinder 28
Piston rod end is hinged with backing plate 29.
Mounting groove is offered on the downside of the rear end portion of second inclined plate 22, shop bolt 30, shop bolt 30 are equipped in mounting groove
One end be hinged on the front side cell wall of mounting groove.
The method that unmanned plane transmitting is carried out using the present invention, is comprised the following steps：
（1）, first will transmitting pedestal 3 by engineering truck roping to launch site, start hydraulic station 6 afterwards, hydraulic station 6 passes through oil
It manages and provides power drive for lifting cylinder 7, transmitting pushing mechanism and folded sheet auxiliary body；
（2）, adjustment unmanned plane launch azimuth：Start stepper motor 8, stepper motor 8 drives main pulley to rotate, and main pulley passes through biography
Dynamic band 12 is driven from belt wheel 11, and so as to which column spinner 10 rotates under the drive from belt wheel 11, turntable 2 starts to rotate, and works as rotation
When platform 2 turns to orientation to be launched, stepper motor 8 is stopped；
（3）, adjustment unmanned plane launch angle：Start lifting cylinder 7, the piston rod of lifting cylinder 7 stretches out and by flat pad 1
Front side portion is propped up, and when flat pad 1 is propped up to launch angle, lifting cylinder 7 is stopped；
（4）, folded sheet auxiliary body from flat pad 1 is put down and is supported on ground：Overturn the second inclined plate 22 forward, second
Inclined plate 22 rotates 180 ° around the second articulated shaft 33, then pulls out two groups of support cylinders 28 out of accommodating groove 27 respectively, turns over backward
Turn the first inclined plate 21 until shop bolt on the ground, is transferred to and inserted out of mounting groove at this time by the lateral support of the second inclined plate 22
If on the ground, then starting support cylinder 28, the piston rod of support cylinder 28 stretches out straight down so that backing plate 29 and ground
Contact；
（5）, unmanned plane is transported to by flat pad 1 by folded sheet auxiliary body：Unmanned plane is transported to the second inclined plate 22
The rack of unmanned plane is connected by rear side by rope with guiding piece 17, and the end of wherein rope is connected to the groove of guiding piece 17
In 19, start hydraulic motor, the positive band movable sprocket 14 of hydraulic motor rotates, and so as to which chain 15 starts to be driven, the drive of chain 15 is led
Draw component to travel forward, guiding piece 17 pulls unmanned plane by rope, and unmanned plane is in 22 He of the second inclined plate of pulling lower edge of rope
First inclined plate 21 is travelled to the rear side of flat pad 1, is closed hydraulic motor, is again started up support cylinder 28, support cylinder afterwards
28 jack up the second inclined plate 22 and the first inclined plate 21, and the first inclined plate 21 is overturn forward around the first articulated shaft 32, until unmanned plane
Afterbody touches the first inclined plate 21, and support cylinder 28 is stopped, and unmanned plane is located at hair under the support of the first inclined plate 21 at this time
The rear side of platform 1 is penetrated, unmanned plane is in battery；
（6）, start transmitting pushing mechanism, carry out transmitting work：The rope connected between unmanned plane rack and guiding piece 17 is taken
Under, then start hydraulic motor, reversely band movable sprocket 14 rotates hydraulic motor, and so as to which chain 15 starts to be driven, chain 15 drives
Traction component moves backward, when guiding piece 17 is moved to 31 lower section of rack of unmanned plane, since the height of guiding piece 17 is more than
The rack 31 of unmanned plane arrives the distance of flat pad 1, so the rack 31 of unmanned plane promotes guiding piece 17, guiding piece 17 is around axis pin
18 rotate forward, and guiding piece 17 passes through the rack 31 of unmanned plane, since the rear lateral portion weight of guiding piece 17 is more than guiding piece
17 front side portion weight, so under the action of the effect of gravity and magnetism, guiding piece 17 resets, the lower surface of guiding piece 17
Again the upper surface with mounting bracket 16 is bonded, and after guiding piece 17 touches the limit switch of rear side, hydraulic motor starts just again
It rotates to band movable sprocket 14, so as to which guiding piece 17 contradicts 31 rear side of rack in unmanned plane under the drive of chain 15, then leads
Draw block 17 to move rapidly forward along the pilot hole 13 that takes off, and guiding piece 17 promotes forward the rack 31 of unmanned plane, and unmanned plane exists
It gives it the gun along flat pad 1 under the promotion of guiding piece 17, and launches forward from the front end of flat pad 1, guiding piece 17
After the limit switch for touching front side, hydraulic motor is stopped, and completes the transmitting work of unmanned plane.
The present embodiment is every according to this hair not to the limitation of works in any form such as shape, material, the structures of the present invention
Any simple modification, equivalent change and modification that bright technical spirit makees above example, belongs to the technology of the present invention side
The protection domain of case.
Claims (8)
1. unmanned plane emitter, it is characterised in that：Including flat pad, turntable and emit pedestal, emit the bottom of pedestal
If there are four traveling wheel, turntable is rotatably connected on transmitting pedestal upper surface by thrust bearing, and hydraulic pressure is equipped in transmitting pedestal
It stands and for driving the revolving power mechanism that turntable rotates, the length direction of flat pad is set along the longitudinal direction, and transmitting is flat
The bottom rear of platform is hinged on the rear side of turntable, and lifting is hinged between the front side bottom of flat pad and the front side of turntable
Oil cylinder, flat pad are equipped with transmitting pushing mechanism, and the rear side of flat pad is equipped with folded sheet auxiliary body, and hydraulic station leads to respectively
Oil pipe is crossed to be connected with lifting cylinder, transmitting pushing mechanism and folded sheet auxiliary body.
2. unmanned plane emitter according to claim 1, it is characterised in that：Revolving power mechanism includes being arranged on transmitting
Stepper motor in pedestal, the main shaft of stepper motor are equipped with main pulley, own centre line edge are fixed at the bottom centre of turntable
The column spinner that vertical direction is set, the lower end of column spinner are extend into through transmitting pedestal upper surface in transmitting pedestal, column spinner
Lower end be equipped with from belt wheel, main pulley is connected by transmission belt with from belt wheel transmission.
3. unmanned plane emitter according to claim 1, it is characterised in that：The upper surface of flat pad is along its length
The pilot hole that takes off is offered, transmitting pushing mechanism includes hydraulic motor, gearbox and two sprocket wheels, and one of sprocket wheel, which rotates, to be connected
The rear interior of flat pad is connected on, another sprocket wheel is rotatably connected on the front interior of flat pad, between two sprocket wheels
It is connected by chain drive, the parallel underface for being located at the pilot hole that takes off of chain, the main shaft of hydraulic motor passes through gearbox and its
In sprocket wheel be sequentially connected, hydraulic station is connected by oil pipe with hydraulic motor, and traction component is equipped on chain；
Two groups of limit switches are additionally provided in flat pad, two groups of limit switches are separately positioned on the front end for the pilot hole that takes off with after
End, two groups of limit switches are connected by circuit with hydraulic motor.
4. unmanned plane emitter according to claim 3, it is characterised in that：Traction component includes mounting bracket and traction
Block, mounting bracket are assemblied in the upper half range of chain, and the longitudinal section of guiding piece is right angled triangle, and the right angle of guiding piece passes through axis pin
The forward upper of mounting bracket is hinged on, the center line of axis pin is set along left and right horizontal direction, and guiding piece is upward through guiding of taking off
Hole simultaneously protrudes from flat pad upper surface, and the leading flank of guiding piece is perpendicular to flat pad upper surface, the rear lateral portion weight of guiding piece
Amount is more than the front side portion weight of guiding piece, and the leading flank of guiding piece offers groove.
5. unmanned plane emitter according to claim 4, it is characterised in that：Guiding piece is made of ferrous material, installation
The rear lateral portion of frame is equipped with magnet.
6. unmanned plane emitter according to claim 1, it is characterised in that：Folded sheet auxiliary body includes the first inclined plate
With the second inclined plate, the first inclined plate and the second inclined plate are set in low dip after preceding height, and there are two the front side edge fixations of the first inclined plate
First hinge sleeve, the back side edge of flat pad are fixed with the second hinge sleeve, the equal edge of center line of the second hinge sleeve and two the first hinge sleeves
Left and right horizontal direction is set, and the second hinge sleeve is located between two the first hinge sleeves, is worn in the second hinge sleeve with two the first hinge sleeves
There is the first articulated shaft；The bottom rear of first inclined plate is fixed with the 3rd hinge sleeve, and there are two the 4th for the front side edge fixation of the second inclined plate
The center line of hinge sleeve, the 3rd hinge sleeve and two the 4th hinge sleeves is set along left and right horizontal direction, and the 3rd hinge sleeve is located at two the
Between four hinge sleeves, the second articulated shaft is equipped in the 3rd hinge sleeve and two the 4th hinge sleeves；The rear lateral portion of first inclined plate is inclined-plane
Structure.
7. unmanned plane emitter according to claim 6, it is characterised in that：It is received there are two opening up the bottom surface of second inclined plate
Receive slot, two accommodating grooves or so are arranged side by side and the length direction of each accommodating groove is consistent with the length direction of the second inclined plate, often
Hydraulic pressure support component is equipped in a accommodating groove, hydraulic pressure support component includes support cylinder, and the cylinder ends of support cylinder are hinged on
The front side of accommodating groove, the piston rod end of support cylinder are hinged with backing plate.
8. unmanned plane emitter according to claim 6, it is characterised in that：It is offered on the downside of the rear end portion of second inclined plate
Mounting groove, mounting groove is interior to be equipped with shop bolt, and one end of shop bolt is hinged on the front side cell wall of mounting groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711396706.4A CN108116690B (en) | 2017-12-21 | 2017-12-21 | Unmanned aerial vehicle emitter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711396706.4A CN108116690B (en) | 2017-12-21 | 2017-12-21 | Unmanned aerial vehicle emitter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108116690A true CN108116690A (en) | 2018-06-05 |
| CN108116690B CN108116690B (en) | 2021-08-06 |
Family
ID=62231070
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711396706.4A Active CN108116690B (en) | 2017-12-21 | 2017-12-21 | Unmanned aerial vehicle emitter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108116690B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111924123A (en) * | 2020-06-24 | 2020-11-13 | 耿新利 | Agricultural thing networking fixed wing unmanned aerial vehicle jettison device |
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| CN204452644U (en) * | 2015-02-05 | 2015-07-08 | 郑州宇通重工有限公司 | High-mobility, multipurpose, wheeled vehicle central axle flat truck |
| CN104803006A (en) * | 2015-04-27 | 2015-07-29 | 西北工业大学 | UAV (Unmanned Aerial Vehicle) catapult-assisted take-off device |
| CN105667789A (en) * | 2016-01-13 | 2016-06-15 | 中国科学院自动化研究所 | Universal type elastic potential energy mechanical catapult for single tandem wing unmanned aerial vehicle with rear propeller |
| CN105775154A (en) * | 2016-05-12 | 2016-07-20 | 孙立民 | General launching platform for unmanned aerial vehicle |
| CN205707412U (en) * | 2016-04-16 | 2016-11-23 | 沈阳航空航天大学 | Electric catapult is accelerated in SUAV Chain conveyer modularity classification |
| CN206012986U (en) * | 2016-08-08 | 2017-03-15 | 成都锦泰铂锐科技有限公司 | A kind of unmanned aerial vehicle ejecting frame |
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2017
- 2017-12-21 CN CN201711396706.4A patent/CN108116690B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204452644U (en) * | 2015-02-05 | 2015-07-08 | 郑州宇通重工有限公司 | High-mobility, multipurpose, wheeled vehicle central axle flat truck |
| CN104803006A (en) * | 2015-04-27 | 2015-07-29 | 西北工业大学 | UAV (Unmanned Aerial Vehicle) catapult-assisted take-off device |
| CN105667789A (en) * | 2016-01-13 | 2016-06-15 | 中国科学院自动化研究所 | Universal type elastic potential energy mechanical catapult for single tandem wing unmanned aerial vehicle with rear propeller |
| CN205707412U (en) * | 2016-04-16 | 2016-11-23 | 沈阳航空航天大学 | Electric catapult is accelerated in SUAV Chain conveyer modularity classification |
| CN105775154A (en) * | 2016-05-12 | 2016-07-20 | 孙立民 | General launching platform for unmanned aerial vehicle |
| CN206012986U (en) * | 2016-08-08 | 2017-03-15 | 成都锦泰铂锐科技有限公司 | A kind of unmanned aerial vehicle ejecting frame |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111924123A (en) * | 2020-06-24 | 2020-11-13 | 耿新利 | Agricultural thing networking fixed wing unmanned aerial vehicle jettison device |
| CN111924123B (en) * | 2020-06-24 | 2022-05-03 | 耿新利 | Agricultural thing networking fixed wing unmanned aerial vehicle jettison device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108116690B (en) | 2021-08-06 |
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