CN107856877A - The transmitting of SUAV, recovery system - Google Patents
The transmitting of SUAV, recovery system Download PDFInfo
- Publication number
- CN107856877A CN107856877A CN201711353931.XA CN201711353931A CN107856877A CN 107856877 A CN107856877 A CN 107856877A CN 201711353931 A CN201711353931 A CN 201711353931A CN 107856877 A CN107856877 A CN 107856877A
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- suav
- car body
- transmitting
- magnet base
- groove
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- 238000011084 recovery Methods 0.000 title claims abstract description 33
- 230000007246 mechanism Effects 0.000 claims abstract description 27
- 238000006073 displacement reaction Methods 0.000 claims description 6
- 230000009286 beneficial effect Effects 0.000 abstract 1
- 230000003068 static effect Effects 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 2
- 230000033001 locomotion Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005259 measurement Methods 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
- B64F1/06—Ground or aircraft-carrier-deck installations for launching aircraft using catapults
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Toys (AREA)
Abstract
The present invention relates to the transmitting of SUAV, recovery system, including car body, the rear side of hull back is provided with emission cavity at roof location, trigger mechanism is installed in emission cavity, car body left back is provided with reclaiming chamber at roof location, recovering mechanism is installed in reclaiming chamber, the groove for connecting both is provided between emission cavity and reclaiming chamber, conveying mechanism is installed in groove.The beneficial effect that the present invention reaches is：Good concealment, mobility are high.
Description
Technical field
The present invention relates to transmitting, the recovery system in unmanned air vehicle technique field, more particularly to SUAV.
Background technology
UAV, abbreviation unmanned plane (UAV), there is maneuverability, rapid reaction, unmanned flight, operation to want
Ask the advantages of low.Unmanned plane is by carrying multiclass sensor, it is possible to achieve image real-time Transmission, high-risk areas detecting function.Mesh
Before, army, police are more and more big to the demand of unmanned plane.For SUAV, often manual control discharges, manually
Operation flight, manual operation recovery.During Artificial Release is put, it is often necessary to discharge from static, if the in-car in motion is released
Put, be then dynamic release, but its more difficult operation, particularly in war or when fighting crime, release simply easily just seems very
It is important., it is necessary to which SUAV is parked in static opening position by people in removal process, just then it can be reclaimed, in order to reduce
The possibility of target exposure is, it is necessary at any time reclaim unmanned plane, and the mode of static recovery can not meet requirement.
The content of the invention
The shortcomings that it is an object of the invention to overcome prior art, there is provided the high miniature self-service of good concealment, mobility
The transmitting of machine, recovery system.
The purpose of the present invention is achieved through the following technical solutions：The transmitting of SUAV, recovery system, including car
Body, the rear side of hull back are provided with emission cavity at roof location, trigger mechanism, car body left back are provided with emission cavity
Reclaiming chamber is provided with roof location, recovering mechanism is installed in reclaiming chamber, is provided with two between emission cavity and reclaiming chamber
The groove of person's connection, is provided with conveying mechanism in groove；
Described trigger mechanism includes Elastomeric launcher, and Elastomeric launcher is arranged on emission cavity antetheca opening position, launched
Chute is provided with the bottom surface of chamber, is provided with guided way, chute is sliding close to the rear end of launch hole close to the front end of car body, guided way
Push block is installed, one end and the Elastomeric launcher of push block are fixedly linked, the other end of push block and minicomputer in groove
Tail end profile is adapted, and inverted T-slot is provided with guided way, and the bottom of the leg of SUAV is fixed with bloom, bloom
Top and bottom and left and right side be provided with can be in retraction bloom roller, set close to one end of chute in the T-slot of guided way
Magnet base A is equipped with, magnet base A switches are provided with magnet base A；
Elastomeric launcher, magnet base switch, the telescopic drive switch of roller electrically connect with processor, and processor is also with distinguishing
In velocity meter and measuring appliance electrical connection of jolting, velocity meter is used for the speed of service for measuring car body, and the measuring appliance that jolts is used
In the displacement of measurement car body car body above-below direction within the unit interval, the measuring appliance that jolts detects displacement of the car body in above-below direction
When upward, Elastomeric launcher just starts, the dynamics for the speed control Elastomeric launcher transmitting that velocity meter measures；
Described recovering mechanism includes recovery telescopic arm, platform, and the one end for reclaiming telescopic arm is fixed in reclaiming chamber, and recovery is flexible
One end of arm is fixed with platform by swivel head, and multiple grooves are provided with platform, is placed with magnet base B in groove, on magnet base B
Magnet base B switches are provided with, each magnetic force B corresponds to a leg of SUAV；
Swivel head, recovery telescopic arm are connected with processor, picture control equipment are additionally provided with car body, picture control is set
Standby, swivel head, recovery telescopic arm are electrically connected with processor, and data-base recording module, data are provided with described processor
The position data of platform when storehouse logging modle record SUAV flies here from different perspectives；
Described conveying mechanism includes crossbeam, clamping conveying arm, and crossbeam is secured transverse on the wall of groove, is provided with crossbeam
The transfer block slided along crossbeam, transfer block are electrically connected with feeder motor, and clamping conveying arm and the defeated arm of clamping are fixed with transfer block
Driving equipment, feeder motor and the equal processor electrical connection of clamping limb driving equipment；
Described clamping conveying arm also includes the telescopic supporting rod of two sections and clamping head, one end of supporting rod are arranged on transfer block
On, the other end of supporting rod is fixed with clamping head, and described clamping head includes two grip blocks in left and right, and grip block opposite face is provided with
Semi-spherical grooves, the leg medium position of described SUAV are fixed with spherical, the hemispherical of the spherical and grip block
Groove is adapted.
The bottom surface of described emission cavity is and low early and high after along car body fore-and-aft direction into certain inclination angle.
The tail end of described SUAV is provided with the higher Shell Plate of intensity.
Each wall in the T-slot of described guided way is the low-down smooth wall of roughness.
Described magnet base A upper surface and the lower surface of T-slot are in same level；Magnet base B upper surface is low
In the upper surface of platform.
Described groove is circular groove, and arc chord angle is provided with the seamed edge of the groove, and the bloom of SUAV leg is
Circular bloom；The upper surface unusual light of platform.
All blooms on the leg of described unmanned plane surround circle.
Described emission cavity, the exit of reclaiming chamber are respectively provided with gate-controlled switch plate.
The present invention has advantages below：（1）By setting Elastomeric launcher, guided way, small-sized nothing can be effectively realized
Man-machine dynamic release；（2）T-slot in guided way, on unmanned plane leg bloom and roller setting, then allow unmanned function more preferable
Launch on ground；（3）The setting of velocity meter, the measuring appliance that jolts, the actual conditions for allowing unmanned plane to be run according to car body are sent out
Penetrate, ensure the quality of transmitting, be easy to unmanned plane self-starting to fly；（4）Magnet base A setting, make unmanned plane before transmission, can quilt
Absorption, close to runner position, ensures the static difference of unmanned plane, while be easy to the transmitting of unmanned plane in guided way；（5）Pass through setting
Telescopic arm, platform and magnet base B are reclaimed, during vehicle movement, is easy to implement the dynamic recovery of SUAV；（6）Rotation
Data-base recording module in head, picture control equipment, processor, can be according to the heading of SUAV, fast velocity modulation
The position of platform is saved, allows unmanned plane quickly low recovery；（7）The smooth setting of platform upper surface, magnet base B upper surfaces are less than platform
Upper surface, the seamed edge of land groove open the setting of arc angle, are when the firm block on the leg of unmanned plane and groove location occur partially
When poor, under the attraction of magnetic force, it is easy to automatically finely tune, allows the firm block of unmanned plane leg to slip into groove.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention；
Fig. 2 is the structural representation of trigger mechanism；
Fig. 3 is the structural representation of recovering mechanism；
Fig. 4 is the structural representation of conveying mechanism；
Fig. 5 is the structural representation of grip block in clamping head；
Fig. 6 is the structural representation of unmanned plane leg；
In figure：1- car bodies, 2- trigger mechanisms, 3- recovering mechanisms, 4- conveying mechanisms, 5- Elastomeric launchers, 6- guided ways, 7- are pushed away
Send block, 8- blooms, 9- rollers, 10- magnet bases A, 11- recovery telescopic arm, 12- platforms, 13- swivel heads, 14- magnet bases B, 15-
Crossbeam, 16- clamping conveying arms, 17- transfer blocks, 18- supporting rods, 19- clamping heads, 20- sphericals.
Embodiment
The present invention will be further described below in conjunction with the accompanying drawings, but protection scope of the present invention is not limited to following institute
State.
As shown in figure 1, the transmitting of SUAV, recovery system, including car body 1, the rear side of the afterbody of car body 1 is close to roof
Opening position is provided with emission cavity, and trigger mechanism 2 is provided with emission cavity, and the left back of car body 1 is provided with recovery at roof location
Chamber, recovering mechanism 3 is installed in reclaiming chamber, the groove for connecting both is provided between emission cavity and reclaiming chamber, is pacified in groove
Equipped with conveying mechanism 4.
Specifically, described trigger mechanism 2 includes Elastomeric launcher 5, and Elastomeric launcher 5 is arranged on emission cavity antetheca
Opening position, chute is provided with the bottom surface of emission cavity, is provided with guided way 6, chute is close close to the front end of car body, guided way 6
The rear end of launch hole, push block 7 is installed in chute, one end and the Elastomeric launcher 5 of push block 7 are fixedly linked, push block 7
The other end be adapted with the tail end profile of minicomputer, inverted T-slot is provided with guided way 6, the leg of SUAV
Bottom is fixed with bloom 8, and the top and bottom and left and right side of bloom 8 are provided with roller 9 that can be in retraction bloom 8, guided way 6
One end in T-slot close to chute is provided with magnet base A10, and magnet base A switches are provided with magnet base A10.
Further, Elastomeric launcher 5, magnet base switch, the telescopic drive switch of roller 9 are electrically connected with processor
Connect, processor also electrically connects with respectively at velocity meter and the measuring appliance that jolts, and velocity meter is used for the operation for measuring car body
Speed, the measuring appliance that jolts are used for the displacement for measuring car body car body above-below direction within the unit interval, and the measuring appliance that jolts detects car
When the displacement of above-below direction is upward, Elastomeric launcher 5 just starts body, the speed control elastic emission that velocity meter measures
The dynamics that device 5 is launched；
Specifically, described recovering mechanism 3 includes recovery telescopic arm 11, platform 12, and one end of recovery telescopic arm 11 is fixed on back
Intracavitary is received, one end of recovery telescopic arm 11 is fixed with platform 12 by swivel head 13, is provided with multiple grooves on platform 12, in groove
Magnet base B14 is placed with, magnet base B switches are provided with magnet base B14, each magnetic force B14 corresponds to one of SUAV
Leg.
Further, swivel head 13, recovery telescopic arm 11 are connected with processor, and image prison is additionally provided with car body 1
Equipment is controlled, picture control equipment, swivel head 13, recovery telescopic arm 11 are electrically connected with processor, set in described processor
There is data-base recording module, the positional number of platform 12 when data-base recording module record SUAV flies here from different perspectives
According to.
Specifically, described conveying mechanism 4 includes crossbeam 15, clamping conveying arm 16, and crossbeam 15 is secured transverse to groove
Wall on, the transfer block 17 slided along crossbeam 15 is installed, transfer block 17 electrically connects with feeder motor, transfer block 17 on crossbeam 15
On be fixed with clamping conveying arm 16 and the defeated arm driving equipment of clamping, feeder motor and the equal processor of clamping limb driving equipment are electrically connected
Connect.
Further, described clamping conveying arm 16 also includes the telescopic supporting rod 18 of two sections and clamping head 19, clamping
One end of bar 18 is arranged in transfer block 17, and the other end of supporting rod 18 is fixed with clamping head 19, and described clamping head 19 includes
The grip block of left and right two, grip block opposite face are provided with semi-spherical grooves, and the leg medium position of described SUAV is fixed with
Spherical 20, the spherical 20 are adapted with the semi-spherical grooves of grip block.
In the present embodiment, the bottom surface of described emission cavity is and low early and high after along car body fore-and-aft direction into certain inclination angle.
In the present embodiment, the tail end of described SUAV is provided with the higher Shell Plate of intensity.
Each wall in the T-slot of described guided way 6 is the low-down smooth wall of roughness, is easy to unmanned plane to send out
Penetrate.
Described magnet base A10 upper surface and the lower surface of T-slot are in same level；Magnet base B14 upper table
Face is less than the upper surface of platform 12.Described groove is circular groove, and arc chord angle, SUAV are provided with the seamed edge of the groove
The bloom 8 of leg is circular bloom；The upper surface unusual light of platform 12.All blooms on the leg of described unmanned plane enclose
Into circle.It is easy to unmanned function to reset recovery in time.
Described emission cavity, the exit of reclaiming chamber are respectively provided with gate-controlled switch plate, improve disguised.
Claims (8)
1. the transmitting of SUAV, recovery system, it is characterised in that：Including car body（1）, car body（1）The rear side of afterbody is close
Emission cavity is provided with roof location, trigger mechanism is installed in emission cavity（2）, car body（1）Left back is at roof location
Reclaiming chamber is provided with, recovering mechanism is installed in reclaiming chamber（3）, it is provided between emission cavity and reclaiming chamber and leads to what both connected
Groove, conveying mechanism is installed in groove（4）；
Described trigger mechanism（2）Including Elastomeric launcher（5）, Elastomeric launcher（5）It is arranged on emission cavity antetheca position
Place, chute is provided with the bottom surface of emission cavity, is provided with guided way（6）, chute is close to the front end of car body, guided way（6）It is close
The rear end of launch hole, push block is installed in chute（7）, push block（7）One end and Elastomeric launcher（5）It is fixedly linked,
Push block（7）The other end be adapted with the tail end profile of minicomputer, guided way（6）In be provided with inverted T-slot, miniature self-service
The bottom of the leg of machine is fixed with bloom（8）, bloom（8）Top and bottom and be provided with can retraction bloom for left and right side（8）It is interior
Roller（9）, guided way（6）T-slot in one end of chute is provided with magnet base A（10）, magnet base A（10）Interior setting
There are magnet base A switches；
Elastomeric launcher（5）, magnet base switch, roller（9）Telescopic drive switch electrically connected with processor, processor is also
Electrically connected with respectively at velocity meter and the measuring appliance that jolts, velocity meter is used for the speed of service for measuring car body, survey of jolting
Measuring device is used for the displacement for measuring car body car body above-below direction within the unit interval, and the measuring appliance that jolts detects car body in above-below direction
Displacement it is upward when, Elastomeric launcher（5）Just start, the speed control Elastomeric launcher that velocity meter measures（5）Hair
The dynamics penetrated；
Described recovering mechanism（3）Including reclaiming telescopic arm（11）, platform（12）, reclaim telescopic arm（11）One end be fixed on back
Intracavitary is received, reclaims telescopic arm（11）One end pass through swivel head（13）It is fixed with platform（12）, platform（12）On be provided with it is multiple recessed
Groove, magnet base B is placed with groove（14）, magnet base B（14）On be provided with magnet base B switch, each magnetic force B（14）It is corresponding small
One leg of type unmanned plane；
Swivel head（13）, recovery telescopic arm（11）It is connected with processor, in car body（1）On be additionally provided with picture control equipment,
Picture control equipment, swivel head（13）, recovery telescopic arm（11）Electrically connected with processor, number is provided with described processor
According to storehouse logging modle, platform when data-base recording module record SUAV flies here from different perspectives（12）Position data；
Described conveying mechanism（4）Include crossbeam（15）, clamping conveying arm（16）, crossbeam（15）It is secured transverse to the wall of groove
On, crossbeam（15）On be provided with along crossbeam（15）The transfer block of slip（17）, transfer block（17）Electrically connect, convey with feeder motor
Block（17）On be fixed with clamping conveying arm（16）And the defeated arm driving equipment of clamping, feeder motor and clamping limb driving equipment are handled
Device electrically connects；
Described clamping conveying arm（16）Also include the two telescopic supporting rods of section（18）And clamping head（19）, supporting rod（18）'s
One end is arranged on transfer block（17）On, supporting rod（18）The other end be fixed with clamping head（19）, described clamping head（19）Bag
Two grip blocks in left and right are included, grip block opposite face is provided with semi-spherical grooves, and the leg medium position of described SUAV is fixed
There is spherical（20）, the spherical（20）It is adapted with the semi-spherical grooves of grip block.
2. the transmitting of SUAV according to claim 1, recovery system, it is characterised in that：Described emission cavity
Bottom surface is and low early and high after along car body fore-and-aft direction into certain inclination angle.
3. the transmitting of SUAV according to claim 2, recovery system, it is characterised in that：Described miniature self-service
The tail end of machine is provided with the higher Shell Plate of intensity.
4. the transmitting of SUAV according to claim 3, recovery system, it is characterised in that：Described guided way（6）
T-slot in each wall be the low-down smooth wall of roughness.
5. the transmitting of SUAV according to claim 1, recovery system, it is characterised in that：Described magnet base A
（10）Upper surface and the lower surface of T-slot be in same level；Magnet base B（14）Upper surface be less than platform（12）It is upper
Surface.
6. the transmitting of SUAV according to claim 5, recovery system, it is characterised in that：Described groove is circle
Connected in star, arc chord angle, the bloom of SUAV leg are provided with the seamed edge of the groove（8）For circular bloom；Platform（12）'s
Upper surface unusual light.
7. the transmitting of SUAV according to claim 6, recovery system, it is characterised in that：Described unmanned plane
All blooms on leg surround circle.
8. the transmitting of SUAV according to claim 1, recovery system, it is characterised in that：Described emission cavity, return
The exit for receiving chamber is respectively provided with gate-controlled switch plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711353931.XA CN107856877B (en) | 2017-12-15 | 2017-12-15 | Small unmanned aerial vehicle's transmission, recovery system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711353931.XA CN107856877B (en) | 2017-12-15 | 2017-12-15 | Small unmanned aerial vehicle's transmission, recovery system |
Publications (2)
| Publication Number | Publication Date |
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| CN107856877A true CN107856877A (en) | 2018-03-30 |
| CN107856877B CN107856877B (en) | 2023-09-05 |
Family
ID=61706247
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711353931.XA Active CN107856877B (en) | 2017-12-15 | 2017-12-15 | Small unmanned aerial vehicle's transmission, recovery system |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109747842A (en) * | 2018-12-27 | 2019-05-14 | 中国航空工业集团公司西安飞机设计研究所 | A drone aerial recovery device |
| CN112644729A (en) * | 2021-01-04 | 2021-04-13 | 航天时代飞鸿技术有限公司 | Automatic launching and recycling device and method based on unmanned vehicle |
| CN113955138A (en) * | 2021-10-29 | 2022-01-21 | 重庆交通大学 | Drone Recovery Platform |
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| CN113955138B (en) * | 2021-10-29 | 2023-11-28 | 重庆交通大学 | Drone recovery platform |
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|---|---|
| CN107856877B (en) | 2023-09-05 |
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