CN110203409A - A kind of military unmanned air vehicle carry system - Google Patents
A kind of military unmanned air vehicle carry system Download PDFInfo
- Publication number
- CN110203409A CN110203409A CN201910503478.9A CN201910503478A CN110203409A CN 110203409 A CN110203409 A CN 110203409A CN 201910503478 A CN201910503478 A CN 201910503478A CN 110203409 A CN110203409 A CN 110203409A
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- 238000009434 installation Methods 0.000 claims abstract description 14
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 13
- 238000006243 chemical reaction Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 4
- 230000002045 lasting effect Effects 0.000 description 3
- 238000013507 mapping Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000013486 operation strategy Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
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- 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
- B64D47/00—Equipment not otherwise provided for
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- 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)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention belongs to military unmanned air vehicle fields, especially a kind of military unmanned air vehicle carry system, for it is existing cannot simultaneously carry multiple equipment, and equipment assembling is complex, it is not easy to dismount, carry equipment is inconvenient to carry out position adjusting, the problem of being unable to satisfy the carry demand of a variety of cruise tasks, now propose following scheme, it includes toggle switch module, carry controls plate module, power module, carry assembly module and UAV Flight Control module, the toggle switch module is connected with carry control plate module, power module is connected with carry control plate module, carry control plate module is connected with carry assembly module.The configuration of the present invention is simple, it is easy to operate, the military unmanned air vehicle carry system can not only simultaneously carry multiple equipment, the installation and removal of equipment are more convenient, and carry equipment facilitate carry out position adjusting, be able to satisfy the carry demand of a variety of cruise tasks.
Description
Technical field
The present invention relates to military unmanned air vehicle technical field more particularly to a kind of military unmanned air vehicle carry systems.
Background technique
Currently, the operation strategies of unmanned plane are more and more extensive with the development of science and technology, power department, public security department, traffic police
Mechanisms, the units such as department, land mapping, video display camera shooting, live news purchase unmanned plane for solving the various of each department successively
Demand, military unmanned air vehicle mostly use more four axis unmanned planes of rotor as a carrier, and purposes depends on the carry mould of unmanned plane
Block, the different module of carry can complete different tasks, and carry video camera is achievable the tasks such as to take photo by plane, carry infrared camera
The tasks such as achievable power-line patrolling, the achievable mapping task of carry remote sensing equipment；
However there are many defects for existing military unmanned air vehicle carry system, on the one hand, cannot simultaneously carry multiple equipment,
And equipment assembling is complex, is not easy to dismount, on the other hand, carry equipment is inconvenient to carry out position adjusting, be unable to satisfy more
The carry demand of kind cruise task.
Summary of the invention
The purpose of the present invention is to solve exist in the prior art cannot simultaneously carry multiple equipment, and equipment assembling compared with
It for complexity, is not easy to dismount, carry equipment is inconvenient to carry out position adjusting, is unable to satisfy the carry demand of a variety of cruise tasks
Disadvantage, and a kind of military unmanned air vehicle carry system proposed.
To achieve the goals above, present invention employs following technical solutions:
A kind of military unmanned air vehicle carry system, including toggle switch module, carry control plate module, power module, carry
Assembly module and UAV Flight Control module, the toggle switch module are connected with carry control plate module, power module
It is connected with carry control plate module, carry control plate module is connected with carry assembly module, UAV Flight Control module
It is connected with carry assembly module, the carry control plate module includes carry generic disk, the fixed peace in the top of carry generic disk
Equipped with drone body, the bottom of carry generic disk is equipped with buck plate, and there are two telescopic foldings for the top fixed installation of buck plate
Bar, the top of two telescopic folding bars are fixedly mounted on the bottom of carry generic disk, and the bottom of the carry generic disk opens up
There are three plug slot, the bottom of buck plate is opened up there are three mounting groove, is equipped with fixed device, three peaces in three mounting grooves
Mounting base is movably installed in tankage, mounting base is adapted with corresponding fixed device, is rotatablely installed in three mounting bases
There is carry device, mounting hole is offered in the top inner wall of three mounting grooves, is fixedly installed with connection in three mounting holes
Line, one end of three connecting lines are fixedly installed with plug, and plug is adapted with corresponding plug slot.
Preferably, pressure spring slot is offered on the two sides inner wall of the plug slot, is slidably installed in two pressure spring slots
There is clamping limb, two clamping limbs are adapted with plug, and the side that two clamping limbs are located remotely from each other is welded with pressure spring, two pressures
One end that spring is located remotely from each other is welded in corresponding two pressure spring slots.
Preferably, three carry devices are respectively video camera, infrared camera and remote sensing equipment, one end of three connecting lines
Be separately mounted on the output line of video camera, infrared camera and remote sensing equipment, power module includes battery, battery with take the photograph
Camera, infrared camera and remote sensing equipment are electrically connected.
Preferably, the fixed device includes threaded post, spring, rotating wheel, rack gear, screw rod, first bevel gear, movement
Block, inserted block, rotating bar, second bevel gear, reel, movable plate and connecting rope offer spring in the top inner wall of mounting groove
Slot, threaded post are slidably mounted in spring groove, and one end of threaded post is welded on spring, and the other end of spring is welded on spring groove
Inner wall on, the other end of threaded post is welded on movable plate, and movable plate is in contact with mounting base, and rotating wheel is threadably mounted at spiral shell
On line column, rotating wheel is rotatably installed on the side inner wall of mounting groove, offers the first groove on the two sides inner wall of mounting groove,
Rack gear is slidably mounted in corresponding first groove, and two rack gears are engaged with rotating wheel.
Preferably, the side that two rack gears are located remotely from each other offers thread groove, and wire rod thread is mounted on corresponding screw thread
In slot, one end of screw rod is rotatably installed on the side inner wall of the first groove, and first bevel gear fixation is set on screw rod, is installed
The two sides of seat offer socket, offer the second groove on the two sides inner wall of mounting groove, movable block is slidably mounted on correspondence
The second groove in, offer the same rotation hole, rotating bar on the second groove and the first groove side inner wall close to each other
It being rotatably installed in rotation hole, the top of rotating bar is welded in second bevel gear, and second bevel gear is engaged with first bevel gear,
Auxiliary tank is offered on the inner wall of second groove, auxiliary block is welded on movable block, and auxiliary block is slidably mounted on corresponding auxiliary
In slot, one end of auxiliary block is welded with one end of buffer spring, and the other end of buffer spring is welded on the inner wall of auxiliary tank.
Preferably, the bottom end of the rotating bar is welded on reel, and connecting rope is wound around on reel, and the one of connecting rope
End is fixedly mounted on movable block, and two movable block sides close to each other offer placing groove, and inserted block is slidably mounted on pair
In the placing groove answered, inserted block is adapted with corresponding socket, and the side that two inserted blocks are located remotely from each other is welded with extension spring, and two
One end that a extension spring is located remotely from each other is welded on the inner wall of corresponding two placing grooves.
Preferably, offer control flume on the side inner wall of the socket, be slidably fitted with mandril in control flume, mandril with
Corresponding inserted block is in contact, and the two sides of mounting base offer link slot, is slidably fitted with control-rod in two link slots, control
The same connecting hole is offered on slot processed and link slot side inner wall close to each other, is slidably fitted with connecting rod in connecting hole,
One end of connecting rod is welded on control-rod, and the other end of connecting rod is welded on mandril.
Preferably, the bottom of the mounting base offers fixing groove, offers rotation slot on the two sides inner wall of fixing groove,
Rotating block is rotatably equipped in two rotation slots, two rotating blocks side close to each other is fixedly installed with the same rotation
Column, carry device are fixedly mounted on the bottom of Rotational Cylindrical, and the side of mounting base is fixedly installed with driving motor, driving motor it is defeated
Shaft is welded on rotating block, and driving motor and battery are electrically connected.
In the present invention, a kind of military unmanned air vehicle carry system, can be with due to being provided with UAV Flight Control module
The stability and control for guaranteeing unmanned plane, the ability and flight quality that improve completion task can due to being provided with power module
To provide lasting continuation of the journey for equipment；
Due to being provided with carry control plate module and carry assembly module, on unmanned plane body can with carry multiple equipment,
When needing to install carry equipment, by corresponding mounting base be inserted into mounting groove in, can position of the fixed mounting in mounting groove,
Driving motor drive rotating block rotation, can drive carry equipment adjust angle, by plug be inserted into plug slot in, clamping limb because
Plug is gripped for the elastic reaction of pressure spring, can carry equipment is connected and be used with unmanned plane body；
The configuration of the present invention is simple, it is easy to operate, the military unmanned air vehicle carry system can not only simultaneously carry multiple equipment, if
Standby installation and removal are more convenient, and carry equipment facilitates progress position adjusting, and the carry for being able to satisfy a variety of cruise tasks needs
It asks.
Detailed description of the invention
Fig. 1 is a kind of system block diagram of military unmanned air vehicle carry system proposed by the present invention；
Fig. 2 is a kind of schematic view of the front view of military unmanned air vehicle carry system proposed by the present invention；
Fig. 3 is a kind of part A structural schematic diagram of military unmanned air vehicle carry system proposed by the present invention；
Fig. 4 is a kind of part B structural schematic diagram of military unmanned air vehicle carry system proposed by the present invention；
Fig. 5 is a kind of C portion structural schematic diagram of military unmanned air vehicle carry system proposed by the present invention.
In figure: 1 carry generic disk, 2 unmanned plane bodies, 3 buck plates, 4 telescopic folding bars, 5 plug slots, 6 mounting grooves, 7
It is mounting base, 8 fixing grooves, 9 Rotational Cylindricals, 10 driving motors, 11 spring grooves, 12 threaded posts, 13 springs, 14 rotating wheels, 15 first recessed
Slot, 16 rack gears, 17 screw rods, 18 first bevel gears, 19 second grooves, 20 movable blocks, 21 inserted blocks, 22 rotating bars, 23 reels, 24
Second bevel gear, 25 movable plates, 26 connecting ropes, 27 clamping limbs, 28 plugs.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.
Embodiment 1
Referring to Fig.1-5, a kind of military unmanned air vehicle carry system, including toggle switch module, carry control plate module, power supply
Module, carry assembly module and UAV Flight Control module, toggle switch module are connected with carry control plate module, power supply
Module is connected with carry control plate module, and carry control plate module is connected with carry assembly module, UAV Flight Control
Module is connected with carry assembly module, and it includes carry generic disk 1 that carry, which controls plate module, and the top of carry generic disk 1 is fixed
Drone body 2 is installed, the bottom of carry generic disk 1 is equipped with buck plate 3, and there are two stretch for the top fixed installation of buck plate 3
Contracting folding rod 4, the top of two telescopic folding bars 4 are fixedly mounted on the bottom of carry generic disk 1, the bottom of carry generic disk 1
Portion is opened up there are three plug slot 5, and the bottom of buck plate 3 is opened up there are three mounting groove 6, is equipped with fixation in three mounting grooves 6
Device is movably installed with mounting base 7 in three mounting grooves 6, and mounting base 7 is adapted with corresponding fixed device, three installations
It is rotatably equipped with carry device on seat 7, offers mounting hole in the top inner wall of three mounting grooves 6, in three mounting holes
It is fixedly installed with connecting line, one end of three connecting lines is fixedly installed with plug 28, plug 28 and corresponding plug slot 5
It is adapted.
In the present embodiment, pressure spring slot is offered on the two sides inner wall of plug slot 5, is slidably installed in two pressure spring slots
There is clamping limb 27, two clamping limbs 27 are adapted with plug 28, and the side that two clamping limbs 27 are located remotely from each other is welded with pressure
Spring, one end that two pressure springs are located remotely from each other are welded in corresponding two pressure spring slots.
In the present embodiment, three carry devices are respectively video camera, infrared camera and remote sensing equipment, three connecting lines
One end is separately mounted on the output line of video camera, infrared camera and remote sensing equipment, and power module includes battery, battery
It is electrically connected with video camera, infrared camera and remote sensing equipment.
In the present embodiment, fixed device includes threaded post 12, spring 13, rotating wheel 14, rack gear 16, the cone of screw rod 17, first
Gear 18, movable block 20, inserted block 21, rotating bar 22, second bevel gear 24, reel 23, movable plate 25 and connecting rope 26, installation
Spring groove 11 is offered in the top inner wall of slot 6, threaded post 12 is slidably mounted in spring groove 11, one end welding of threaded post 12
On spring 13, the other end of spring 13 is welded on the inner wall of spring groove 11, and the other end of threaded post 12 is welded on movable plate
On 25, movable plate 25 is in contact with mounting base 7, and rotating wheel 14 is threadably mounted in threaded post 12, and rotating wheel 14 is rotatably installed in
On the side inner wall of mounting groove 6, the first groove 15 is offered on the two sides inner wall of mounting groove 6, rack gear 16 is slidably mounted on pair
In the first groove 15 answered, two rack gears 16 are engaged with rotating wheel 14.
In the present embodiment, the side that two rack gears 16 are located remotely from each other offers thread groove, and screw rod 17 is threadably mounted at pair
In the thread groove answered, one end of screw rod 17 is rotatably installed on the side inner wall of the first groove 15,18 fixing sleeve of first bevel gear
It being located on screw rod 17, the two sides of mounting base 7 offer socket, the second groove 19 is offered on the two sides inner wall of mounting groove 6,
Movable block 20 is slidably mounted in corresponding second groove 19, the second groove 19 and the first groove 15 side inner wall close to each other
On offer the same rotation hole, rotating bar 22 is rotatably installed in rotation hole, and the top of rotating bar 22 is welded on the second cone tooth
On wheel 24, second bevel gear 24 is engaged with first bevel gear 18, and auxiliary tank, movable block 20 are offered on the inner wall of the second groove 19
On be welded with auxiliary block, auxiliary block is slidably mounted in corresponding auxiliary tank, and one end of auxiliary block is welded with the one of buffer spring
End, the other end of buffer spring are welded on the inner wall of auxiliary tank.
In the present embodiment, the bottom end of rotating bar 22 is welded on reel 23, and connecting rope 26 is wound around on reel 23, even
One end of splicing 26 is fixedly mounted on movable block 20, and two sides close to each other of movable block 20 offer placing groove, is inserted
Block 21 is slidably mounted in corresponding placing groove, and inserted block 21 is adapted with corresponding socket, two inserted blocks 21 be located remotely from each other one
Side is welded with extension spring, and one end that two extension springs are located remotely from each other is welded on the inner wall of corresponding two placing grooves
On.
In the present embodiment, control flume is offered on the side inner wall of socket, is slidably fitted with mandril in control flume, mandril with
Corresponding inserted block 21 is in contact, and the two sides of mounting base 7 offer link slot, is slidably fitted with control in two link slots
The same connecting hole, the company of being slidably fitted in connecting hole are offered on bar, control flume and link slot side inner wall close to each other
One end of extension bar, connecting rod is welded on control-rod, and the other end of connecting rod is welded on mandril.
In the present embodiment, the bottom of mounting base 7 offers fixing groove 8, offers rotation on the two sides inner wall of fixing groove 8
Slot is rotatably equipped with rotating block in two rotation slots, and two rotating blocks side close to each other is fixedly installed with same
Rotational Cylindrical 9, carry device are fixedly mounted on the bottom of Rotational Cylindrical 9, and the side of mounting base 7 is fixedly installed with driving motor 10, drive
The output shaft of dynamic motor 10 is welded on rotating block, and driving motor 10 and battery are electrically connected.
In the present embodiment, due to being provided with UAV Flight Control module, it is ensured that the stability and manipulation of unmanned plane
Property, improve completion task ability and flight quality, due to be provided with power module, lasting continuation of the journey can be provided for equipment；By
It, can be with carry multiple equipment, toggle switch mould on unmanned plane body 2 in being provided with carry control plate module and carry assembly module
Block, carry control plate module, power module, carry assembly module and UAV Flight Control module belong to the prior art, such as
Application No. is 201711182855.0 to disclose a kind of unmanned plane carry identifying system, wherein describing the tool of above-mentioned module in detail
The connection type and working principle of body when needing to install carry equipment, corresponding mounting base 7 are inserted into mounting groove 6, mounting base
7 drive movable plate 25 mobile, and movable plate 25 drives threaded post 12 mobile, and threaded post 12 drives rotating wheel 14 to rotate, rotating wheel 14
It driving two rack gears 16 mobile, drives screw rod 17 to rotate when rack gear 16 is mobile, screw rod 17 drives first bevel gear 18 to rotate, and first
Bevel gear 18 drives second bevel gear 24 to rotate, and second bevel gear 24 drives rotating bar 22 to rotate, and rotating bar 22 drives reel
23 rotations, reel 23 decontrol connecting rope 26, because the elastic reaction of buffer spring drives auxiliary block mobile, auxiliary block is driven
Movable block 20 is mobile, and movable block 20 drives inserted block 21 mobile, so that inserted block 21 is in contact with mounting base 7, inserted block 21 is moved to slotting
Mouthful position after because extension spring elastic reaction drive inserted block 21 slide into socket in, can fixed mounting 7 in mounting groove
Position in 6, driving motor 10 drive rotating block rotation, and rotating block can drive Rotational Cylindrical 9 to rotate, and Rotational Cylindrical 9 can drive extension
It carries equipment and adjusts angle, plug 28 is inserted into plug slot 5, clamping limb 27 is because the elastic reaction of pressure spring clamps plug 28
It is fixed, can carry equipment be connected and be used with unmanned plane body 2；The military unmanned air vehicle carry system can not only simultaneously carry
The installation and removal of multiple equipment, equipment are more convenient, and carry equipment facilitates progress position adjusting, are able to satisfy a variety of cruises and appoint
The carry demand of business.
Embodiment 2
Referring to Fig.1-5, it is further improved on the basis of embodiment 1:
A kind of military unmanned air vehicle carry system, including toggle switch module, carry control plate module, power module, carry
Assembly module and UAV Flight Control module, toggle switch module are connected with carry control plate module, power module and extension
It carries control plate module to be connected, carry control plate module is connected with carry assembly module, UAV Flight Control module and extension
It carries assembly module to be connected, it includes carry generic disk 1 that carry, which controls plate module, and the top of carry generic disk 1 is bolted
Drone body 2 is installed, the bottom of carry generic disk 1 is equipped with buck plate 3, and the top of buck plate 3 is bolted installation
There are two telescopic folding bar 4, the top of two telescopic folding bars 4 is mounted by means of bolts on the bottom of carry generic disk 1,
The bottom of carry generic disk 1 is opened up there are three plug slot 5, and the bottom of buck plate 3 is opened up there are three mounting groove 6, and three are installed
It is equipped with fixed device in slot 6, is movably installed with mounting base 7 in three mounting grooves 6, mounting base 7 and corresponding fixed device
It is adapted, carry device is rotatably equipped in three mounting bases 7, offers installation in the top inner wall of three mounting grooves 6
Hole is bolted in three mounting holes and is equipped with connecting line, and one end of three connecting lines is bolted installation
There is plug 28, plug 28 is adapted with corresponding plug slot 5.
In the present embodiment, pressure spring slot is offered on the two sides inner wall of plug slot 5, is slidably installed in two pressure spring slots
There is clamping limb 27, two clamping limbs 27 are adapted with plug 28, and the side that two clamping limbs 27 are located remotely from each other is welded with pressure
Spring, one end that two pressure springs are located remotely from each other are welded in corresponding two pressure spring slots.
In the present embodiment, three carry devices are respectively video camera, infrared camera and remote sensing equipment, three connecting lines
One end is separately mounted on the output line of video camera, infrared camera and remote sensing equipment, and power module includes battery, battery
It is electrically connected with video camera, infrared camera and remote sensing equipment.
In the present embodiment, fixed device includes threaded post 12, spring 13, rotating wheel 14, rack gear 16, the cone of screw rod 17, first
Gear 18, movable block 20, inserted block 21, rotating bar 22, second bevel gear 24, reel 23, movable plate 25 and connecting rope 26, installation
Spring groove 11 is offered in the top inner wall of slot 6, threaded post 12 is slidably mounted in spring groove 11, one end welding of threaded post 12
On spring 13, the other end of spring 13 is welded on the inner wall of spring groove 11, and the other end of threaded post 12 is welded on movable plate
On 25, movable plate 25 is in contact with mounting base 7, and rotating wheel 14 is threadably mounted in threaded post 12, and rotating wheel 14 is rotatably installed in
On the side inner wall of mounting groove 6, the first groove 15 is offered on the two sides inner wall of mounting groove 6, rack gear 16 is slidably mounted on pair
In the first groove 15 answered, two rack gears 16 are engaged with rotating wheel 14.
In the present embodiment, the side that two rack gears 16 are located remotely from each other offers thread groove, and screw rod 17 is threadably mounted at pair
In the thread groove answered, one end of screw rod 17 is rotatably installed on the side inner wall of the first groove 15,18 fixing sleeve of first bevel gear
It being located on screw rod 17, the two sides of mounting base 7 offer socket, the second groove 19 is offered on the two sides inner wall of mounting groove 6,
Movable block 20 is slidably mounted in corresponding second groove 19, the second groove 19 and the first groove 15 side inner wall close to each other
On offer the same rotation hole, rotating bar 22 is rotatably installed in rotation hole, and the top of rotating bar 22 is welded on the second cone tooth
On wheel 24, second bevel gear 24 is engaged with first bevel gear 18, and auxiliary tank, movable block 20 are offered on the inner wall of the second groove 19
On be welded with auxiliary block, auxiliary block is slidably mounted in corresponding auxiliary tank, and one end of auxiliary block is welded with the one of buffer spring
End, the other end of buffer spring are welded on the inner wall of auxiliary tank.
In the present embodiment, the bottom end of rotating bar 22 is welded on reel 23, and connecting rope 26 is wound around on reel 23, even
One end of splicing 26 is mounted by means of bolts on movable block 20, and two sides close to each other of movable block 20 offer and put
Slot is set, inserted block 21 is slidably mounted in corresponding placing groove, and inserted block 21 is adapted with corresponding socket, and two inserted blocks 21 are mutually remote
From side be welded with extension spring, one end that two extension springs are located remotely from each other is welded on corresponding two placing grooves
On inner wall.
In the present embodiment, control flume is offered on the side inner wall of socket, is slidably fitted with mandril in control flume, mandril with
Corresponding inserted block 21 is in contact, and the two sides of mounting base 7 offer link slot, is slidably fitted with control in two link slots
The same connecting hole, the company of being slidably fitted in connecting hole are offered on bar, control flume and link slot side inner wall close to each other
One end of extension bar, connecting rod is welded on control-rod, and the other end of connecting rod is welded on mandril.
In the present embodiment, the bottom of mounting base 7 offers fixing groove 8, offers rotation on the two sides inner wall of fixing groove 8
Slot is rotatably equipped with rotating block in two rotation slots, and two rotating blocks side close to each other is bolted installation
There is the same Rotational Cylindrical 9, carry device is mounted by means of bolts on the bottom of Rotational Cylindrical 9, and the side of mounting base 7 passes through bolt
It is fixedly installed with driving motor 10, the output shaft of driving motor 10 is welded on rotating block, and driving motor 10 and battery are electrical
Connection.
In the present embodiment, due to being provided with UAV Flight Control module, it is ensured that the stability and manipulation of unmanned plane
Property, improve completion task ability and flight quality, due to be provided with power module, lasting continuation of the journey can be provided for equipment；By
It, can be with carry multiple equipment, toggle switch mould on unmanned plane body 2 in being provided with carry control plate module and carry assembly module
Block, carry control plate module, power module, carry assembly module and UAV Flight Control module belong to the prior art, such as
Application No. is 201711182855.0 to disclose a kind of unmanned plane carry identifying system, wherein describing the tool of above-mentioned module in detail
The connection type and working principle of body when needing to install carry equipment, corresponding mounting base 7 are inserted into mounting groove 6, mounting base
7 drive movable plate 25 mobile, and movable plate 25 drives threaded post 12 mobile, and threaded post 12 drives rotating wheel 14 to rotate, rotating wheel 14
It driving two rack gears 16 mobile, drives screw rod 17 to rotate when rack gear 16 is mobile, screw rod 17 drives first bevel gear 18 to rotate, and first
Bevel gear 18 drives second bevel gear 24 to rotate, and second bevel gear 24 drives rotating bar 22 to rotate, and rotating bar 22 drives reel
23 rotations, reel 23 decontrol connecting rope 26, because the elastic reaction of buffer spring drives auxiliary block mobile, auxiliary block is driven
Movable block 20 is mobile, and movable block 20 drives inserted block 21 mobile, so that inserted block 21 is in contact with mounting base 7, inserted block 21 is moved to slotting
Mouthful position after because extension spring elastic reaction drive inserted block 21 slide into socket in, can fixed mounting 7 in mounting groove
Position in 6, driving motor 10 drive rotating block rotation, and rotating block can drive Rotational Cylindrical 9 to rotate, and Rotational Cylindrical 9 can drive extension
It carries equipment and adjusts angle, plug 28 is inserted into plug slot 5, clamping limb 27 is because the elastic reaction of pressure spring clamps plug 28
It is fixed, can carry equipment be connected and be used with unmanned plane body 2；The military unmanned air vehicle carry system can not only simultaneously carry
The installation and removal of multiple equipment, equipment are more convenient, and carry equipment facilitates progress position adjusting, are able to satisfy a variety of cruises and appoint
The carry demand of business
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Anyone skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (8)
1. a kind of military unmanned air vehicle carry system, including toggle switch module, carry control plate module, power module, carry group
Part module and UAV Flight Control module, which is characterized in that the toggle switch module is connected with carry control plate module,
Power module is connected with carry control plate module, and carry control plate module is connected with carry assembly module, unmanned plane during flying
Control module is connected with carry assembly module, and the carry control plate module includes carry generic disk (1), carry generic disk
(1) it is fixedly installed at the top of drone body (2), the bottom of carry generic disk (1) is equipped with buck plate (3), buck plate (3)
There are two telescopic folding bar (4) for top fixed installation, and the top of two telescopic folding bars (4) is fixedly mounted on carry generic disk
(1) bottom, the bottom of the carry generic disk (1) are opened up there are three plug slot (5), and the bottom of buck plate (3) offers
Three mounting grooves (6), three mounting grooves (6) are interior to be equipped with fixed device, is movably installed with mounting base in three mounting grooves (6)
(7), mounting base (7) is adapted with corresponding fixed device, is rotatably equipped with carry device on three mounting bases (7), and three
Mounting hole is offered in the top inner wall of mounting groove (6), and connecting line, three connecting lines are fixedly installed in three mounting holes
One end be fixedly installed with plug (28), plug (28) is adapted with corresponding plug slot (5).
2. a kind of military unmanned air vehicle carry system according to claim 1, which is characterized in that the plug slot (5)
Pressure spring slot is offered on the inner wall of two sides, is slidably fitted in two pressure spring slots clamping limb (27), and two clamping limbs (27) are equal
It is adapted with plug (28), the side that two clamping limbs (27) are located remotely from each other is welded with pressure spring, what two pressure springs were located remotely from each other
One end is welded in corresponding two pressure spring slots.
3. a kind of military unmanned air vehicle carry system according to claim 1, which is characterized in that three carry devices are respectively
Video camera, infrared camera and remote sensing equipment, one end of three connecting lines are separately mounted to video camera, infrared camera and remote sensing
On the output line of equipment, power module includes battery, and battery electrically connects with video camera, infrared camera and remote sensing equipment
It connects.
4. a kind of military unmanned air vehicle carry system according to claim 1, which is characterized in that the fixed device includes spiral shell
Line column (12), spring (13), rotating wheel (14), rack gear (16), screw rod (17), first bevel gear (18), movable block (20), inserted block
(21), rotating bar (22), second bevel gear (24), reel (23), movable plate (25) and connecting rope (26), mounting groove (6)
It is offered in top inner wall spring groove (11), threaded post (12) is slidably mounted in spring groove (11), one end of threaded post (12)
It is welded on spring (13), the other end of spring (13) is welded on the inner wall of spring groove (11), the other end of threaded post (12)
It is welded on movable plate (25), movable plate (25) is in contact with mounting base (7), and rotating wheel (14) is threadably mounted at threaded post (12)
On, rotating wheel (14) is rotatably installed on the side inner wall of mounting groove (6), and is offered on the two sides inner wall of mounting groove (6)
One groove (15), rack gear (16) are slidably mounted in corresponding first groove (15), two rack gears (16) with rotating wheel (14)
Engagement.
5. a kind of military unmanned air vehicle carry system according to claim 4, which is characterized in that two rack gears (16) are mutually remote
From side offer thread groove, screw rod (17) is threadably mounted in corresponding thread groove, and one end of screw rod (17) rotates peace
On the side inner wall of the first groove (15), first bevel gear (18) fixation is set on screw rod (17), and the two of mounting base (7)
Side offers socket, offers on the two sides inner wall of mounting groove (6) the second groove (19), and movable block (20) is slidably mounted on
In corresponding second groove (19), offered on the second groove (19) side inner wall close to each other with the first groove (15) same
A rotation hole, rotating bar (22) are rotatably installed in rotation hole, and the top of rotating bar (22) is welded on second bevel gear (24),
Second bevel gear (24) is engaged with first bevel gear (18), offers auxiliary tank, movable block on the inner wall of the second groove (19)
(20) auxiliary block is welded on, auxiliary block is slidably mounted in corresponding auxiliary tank, and one end of auxiliary block is welded with buffer spring
One end, the other end of buffer spring is welded on the inner wall of auxiliary tank.
6. a kind of military unmanned air vehicle carry system according to claim 4, which is characterized in that the bottom of the rotating bar (22)
End is welded on reel (23), and connecting rope (26) is wound around on reel (23), and one end of connecting rope (26) is fixedly mounted on
On movable block (20), two movable block (20) sides close to each other offer placing groove, and inserted block (21) is slidably mounted on pair
In the placing groove answered, inserted block (21) is adapted with corresponding socket, and the side that two inserted blocks (21) are located remotely from each other is welded with drawing
Spring is stretched, one end that two extension springs are located remotely from each other is welded on the inner wall of corresponding two placing grooves.
7. a kind of military unmanned air vehicle carry system according to claim 5, which is characterized in that the side inner wall of the socket
On offer control flume, mandril is slidably fitted in control flume, mandril is in contact with corresponding inserted block (21), mounting base (7)
Two sides offer link slot, are slidably fitted with control-rod in two link slots, control flume and link slot it is close to each other one
The same connecting hole is offered on the inner wall of side, connecting rod is slidably fitted in connecting hole, and one end of connecting rod is welded on control-rod
On, the other end of connecting rod is welded on mandril.
8. a kind of military unmanned air vehicle carry system according to claim 1, which is characterized in that the bottom of the mounting base (7)
Portion offers fixing groove (8), and rotation slot is offered on the two sides inner wall of fixing groove (8), is rotatablely installed in two rotation slots
There is rotating block, two rotating blocks side close to each other is fixedly installed with the same Rotational Cylindrical (9), and carry device is fixedly mounted
In the bottom of Rotational Cylindrical (9), the side of mounting base (7) is fixedly installed with driving motor (10), the output shaft of driving motor (10)
It is welded on rotating block, driving motor (10) and battery are electrically connected.
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| CN201910503478.9A CN110203409A (en) | 2019-06-11 | 2019-06-11 | A kind of military unmanned air vehicle carry system |
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| CN201910503478.9A CN110203409A (en) | 2019-06-11 | 2019-06-11 | A kind of military unmanned air vehicle carry system |
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