CN109334961A - A kind of accurate delivery device of relief supplies - Google Patents
A kind of accurate delivery device of relief supplies Download PDFInfo
- Publication number
- CN109334961A CN109334961A CN201811149426.8A CN201811149426A CN109334961A CN 109334961 A CN109334961 A CN 109334961A CN 201811149426 A CN201811149426 A CN 201811149426A CN 109334961 A CN109334961 A CN 109334961A
- Authority
- CN
- China
- Prior art keywords
- hawser
- supply case
- movable end
- fixed
- reel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/52—Tilting of rotor bodily relative to fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
-
- 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
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- 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
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of accurate delivery devices of relief supplies, it includes that sighting device (1), flying platform (3), hawser folding and unfolding component (7), hawser movable end positioning component (8) and article deliver component (9), can be used for the accurate delivery of goods and materials, food, drinking water, first-aid dressing and other items under the situations such as disaster area, region of war, personnel are stranded；Environmental information is provided by sighting device (1) to be controlled, and specified region is quickly reached by flying platform (3)；Then by hawser folding and unfolding component (7) folding and unfolding hawser, hawser movable end is accurately sent to delivery location by hawser movable end positioning component (8) and by manually fixing, delivers the accurate delivery that component (9) carry out urgent article finally by article.
Description
Technical field
The present invention relates to a kind of accurate delivery devices of relief supplies.
Background technique
Under disaster area, region of war and the situations such as personnel are stranded, it usually needs goods and materials, food, drinking water, first-aid dressing and other items
Delivery supply, the prior art mostly uses the mode that helicopter high-altitude is delivered or manpower ground is delivered, precision is low, low efficiency,
Risk is big and at high cost.
Summary of the invention
In view of the above existing problems in the prior art, the present invention provides a kind of accurate delivery devices of relief supplies, can be used for
The accurate delivery of goods and materials, food, drinking water, first-aid dressing and other items under the situations such as disaster area, region of war, personnel are stranded；It is filled by vision
It sets offer environmental information to be controlled, component is adjusted by rotor tilting component, rotor assemblies and rotor pose and controls nobody
The accurate delivery device of the urgent article of machine formula circumvents barrier and quickly reaches specified region；Then pass through hawser folding and unfolding component folding and unfolding cable
Rope, is accurately sent hawser movable end to delivery location by hawser movable end positioning component and by manually fixing, finally by object
Product deliver the accurate delivery that component carries out urgent article.Freedom of motion of the present invention is high, strong flexibility, and urgent article is delivered accurate
Degree is high and distributing procedure is steady, highly-safe, high-efficient, at low cost.
To achieve the goals above, the technical solution adopted by the present invention is that: a kind of urgent article of unmanned plane formula is precisely delivered
Device, which is characterized in that it includes sighting device, flying platform, hawser folding and unfolding component, hawser movable end positioning component and object
Product deliver component.The present invention is a kind of accurate delivery device of urgent article of unmanned plane formula, and it is stranded to can be used for disaster area, region of war, personnel
Etc. the accurate delivery of goods and materials, food, drinking water, first-aid dressing and other items under situations；Environmental information is provided by sighting device to carry out
Control quickly reaches specified region by flying platform；Then by hawser folding and unfolding component folding and unfolding hawser, pass through hawser movable end
Hawser movable end is accurately sent to delivery location and by manually fixing by positioning component, is delivered component finally by article and is carried out promptly
The accurate delivery of article.Freedom of motion of the present invention is high, strong flexibility, and urgent article delivers that precision is high and distributing procedure is flat
Surely, highly-safe, high-efficient, at low cost.
The hawser folding and unfolding component include reel, reel swivel bearing, reel electric rotating base, reel rotating electric machine, hawser,
Front wheel, cable guide and rear wheel；Reel electric rotating base is fixed with flying platform bolt, reel swivel bearing it is interior
Outer ring is fixed with reel electric rotating base and reel bolt respectively, and the body of reel electric rotating base is bolted on reel
On electric rotating base, output shaft and reel are keyed；The pulley base of front wheel, the pulley base of rear wheel and cable guide
It is bolted on flying platform, hawser one end is fixed on reel, and other end winding reel is after a few, then successively passes through
Hawser movable end positioning group is fixed on after the pulley body of the pulley body of front wheel, the pilot hole of cable guide and rear wheel
On part；With respect to its body around the rotary motion of its axis, band movable reel is rotated about the axis thereof, is realized reel rotating electric machine output shaft
The adaptive folding and unfolding of hawser, rolls withdrawal for hawser when not in use, avoids the interference accurate delivery device of the urgent article of unmanned plane formula
Movement, when use releases hawser, is carried by hawser movable end positioning component to delivery location and realizes artificial fixed, is tight
The accurate delivery of anxious article provides precondition.
The hawser movable end positioning component includes hawser movable end fixing piece, movable end positioning unmanned plane and positioning
Unmanned plane fixing seat；The movable end of hawser movable end fixing piece one end and hawser is fixedly clamped, and the other end and movable end position nothing
Man-machine bolt is fixed, and positioning unmanned plane fixing seat is bolted on flying platform；When work, put in hawser folding and unfolding component
Out under the premise of hawser, the movable end arrival that movable end positioning unmanned plane carries hawser need to carry out the position of article delivery and by people
Work is steady fixed by it, provides precondition for the accurate delivery of urgent article；When not working, movable end positioning unmanned plane passes through
Positioning unmanned plane fixing seat is realized fixes with the position of flying platform, prevents it from falling in the motion process of flying platform
It falls.
It includes that supply case arc movement device, supply case, supply case end cap, lower magnet are fixed that the article, which delivers component,
Part, lower part electromagnet, top electromagnet, upper magnet fixing member, telescopic shaft, hydraulic flexural pivot and hawser moving member；Supply case arc
Shape telecontrol equipment can be made of 360 degree of round sliding rails and a series of built-in driving devices along the sliding block that sliding rail moves freely, be fed
The sliding rail of case arc movement device is fixed with flying platform bolt, the sliding block of supply case arc movement device and lower magnet fixing member
Bolt is fixed, and lower magnet fixing member is fixed with lower part electromagnetism iron bolt again；Driving device built in hawser moving member, can be along hawser certainly
Such as movement, fixing end of the fixing end of hydraulic flexural pivot with movable end respectively with hawser moving member and telescopic shaft welds together, stretches
The movable end of contracting axis welds together with upper magnet fixing member again, and top electromagnet is bolted on magnet fixing member
On；Supply case and supply case end cap can be threadably secured, and the material of main part of supply case and supply case end cap is rigid plastics,
The bottom of supply case and the outside of supply case end cap are embedded with round stainless steel plate, enable supply case and supply case end cap respectively by
Lower part electromagnet and the absorption of top electromagnet after energization are fixed；Hydraulic flexural pivot movable end bypasses its center point with respect to its fixing end
The rotary motion of any axis passes through upper magnet along the linear movement of its axis with respect to its fixing end in conjunction with telescopic shaft movable end
Fixing piece drives the adaptive pose adjustment for realizing top electromagnet；In transportational process, supply case and supply case end cap screw thread are solid
Fixed, lower part electromagnet is bonded and is powered with supply case bottom, and supply case is smoothly absorbed and fixed on flying platform；It reaches and throws
After sending region, hawser movable end is sent to delivery location simultaneously in hawser folding and unfolding component and hawser movable end positioning component cooperating
Under the premise of realizing artificial fix, supply case arc movement device, telescopic shaft and hydraulic flexural pivot collective effect make top electric
Magnet is bonded and is powered with the supply case end cap that need to deliver supply case, and then lower part electromagnet powers off, so that the supply that need to be delivered
Case and top electromagnet smoothly adsorb fixation, and subsequently telescopic shaft drives the supply case that need to be delivered to be detached from lower part electromagnet, most
It is precisely delivered by hawser moving member band trend designated position afterwards；It delivers after reaching, electromagnet power-off in top puts down supply case so
It is driven and is returned to carry out the delivery of next supply case by hawser moving member afterwards, personnel open supply case end cap and feed；One
After place is delivered, the position of flying platform and movable end positioning unmanned plane is adjusted, carries out the urgent article essence in next place
Standard is delivered.
The present invention is a kind of accurate delivery device of urgent article of unmanned plane formula, can be used for the shapes such as disaster area, region of war, personnel are stranded
The accurate delivery of goods and materials, food, drinking water, first-aid dressing and other items under condition；Environmental information is provided by sighting device to be controlled,
Specified region is quickly reached by flying platform；Then it by hawser folding and unfolding component folding and unfolding hawser, is positioned by hawser movable end
Hawser movable end is accurately sent to delivery location and by manually fixing by component, is delivered component finally by article and is carried out urgent article
Accurate delivery.Freedom of motion of the present invention is high, strong flexibility, and urgent article delivers that precision is high and distributing procedure is steady, peace
It is Quan Xinggao, high-efficient, at low cost.
Detailed description of the invention
Fig. 1 is a kind of accurate delivery device schematic illustration of relief supplies provided in an embodiment of the present invention；
In figure: 1, sighting device, 2, rotor tilting component, 3, flying platform, 4, more rotor angles adjustment component, 5, rotor group
Part, 6, rotor pose adjustment component, 7, hawser folding and unfolding component, 8, hawser movable end positioning component, 9, article delivery component.
Fig. 2 is rotor assemblies schematic illustration provided in an embodiment of the present invention；
In figure: 5.1, propeller, 5.2, propeller swivel bearing, 5.3, propeller carrier, 5.4, propeller rotating electric machine.
Fig. 3 is that rotor pose provided in an embodiment of the present invention adjusts assembly principle schematic diagram；
In figure: 6.1, rotor moves typed ball bearing pair, 6.2, rotor movement telescopic shaft, 6.3, the hydraulic flexural pivot of rotor movement, 6.4, rotor
Pose adjusting seat.
Fig. 4 is rotor tilting component schematic illustration provided in an embodiment of the present invention；
In figure: 2.1, rotor pitch arm, 2.2, rotor pitch bearing, 2.3, rotor pitching motor, 2.4, rotor pitching pedestal.
It is to avoid generating task execution that used rotor upwarp state is interfered to show that Fig. 5, which is provided in an embodiment of the present invention,
It is intended to.
Fig. 6 is that more rotor angles provided in an embodiment of the present invention adjust assembly principle schematic diagram；
In figure: 4.1, rotor arcuate movement sliding rail, 4.2, rotor arcuate movement sliding block.
Fig. 7 is quadrotor motor pattern figure provided in an embodiment of the present invention.
Fig. 8 is the three rotor motor pattern figures provided in an embodiment of the present invention when a rotor breaks down.
Fig. 9 ~ 10 are the two rotor motor pattern figures provided in an embodiment of the present invention when two rotors break down.
Figure 11 is the floating state air reaction force schematic diagram under quadrotor motor pattern provided in an embodiment of the present invention.
Figure 12 is the translation state air reaction force schematic diagram under quadrotor motor pattern provided in an embodiment of the present invention.
Figure 13 is the rollover states air reaction force schematic diagram under quadrotor motor pattern provided in an embodiment of the present invention.
Figure 14 is the side pose floating state air reaction force under quadrotor motor pattern provided in an embodiment of the present invention
Schematic diagram.
Figure 15 is hawser folding and unfolding assembly principle schematic diagram provided in an embodiment of the present invention；
In figure: 7.1, reel, 7.2, reel swivel bearing, 7.3, reel electric rotating base, 7.4, reel rotating electric machine, 7.5, cable
Rope, 7.6, front wheel, 7.7, cable guide, 7.8, rear wheel.
Figure 16 is hawser movable end positioning component schematic illustration provided in an embodiment of the present invention；
In figure: 8.1, hawser movable end fixing piece, 8.2, movable end positioning unmanned plane, 8.3, positioning unmanned plane fixing seat.
Figure 17 is that article provided in an embodiment of the present invention delivers assembly principle schematic diagram；
In figure: 9.1, supply case arc movement device, 9.2, supply case, 9.3, supply case end cap, 9.4, lower magnet fixing member,
9.5, lower part electromagnet, 9.6, top electromagnet, 9.7, upper magnet fixing member, 9.8, telescopic shaft, 9.9, hydraulic flexural pivot, 9.10,
Hawser moving member.
Figure 18 is the urgent accurate delivery status schematic diagram of article provided in an embodiment of the present invention.
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.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Referring to Fig. 1, being a kind of accurate delivery device schematic illustration of relief supplies provided in an embodiment of the present invention, it is wrapped
Include sighting device 1, rotor tilting component 2, flying platform 3, more rotor angles adjustment component 4, rotor assemblies 5, rotor pose tune
Whole group part 6, hawser folding and unfolding component 7, hawser movable end positioning component 8 and article deliver component 9.The present invention is a kind of unmanned plane
The accurate delivery device of the urgent article of formula can be used for goods and materials, food, drinking water, first aid under the situations such as disaster area, region of war, personnel are stranded
The accurate delivery of packet and other items；Environmental information is provided by sighting device 1 to be controlled, and rotor tilting component 2, rotor group are passed through
Part 5 and rotor pose adjustment component 6 control the accurate delivery device of the urgent article of unmanned plane formula and circumvent barrier and quickly reach and refer to
Determine region；Then by hawser movable end positioning component 8 that hawser movable end is accurate by 7 folding and unfolding hawser of hawser folding and unfolding component
It send to delivery location and by manually fixing, delivers the accurate delivery that component 9 carries out urgent article finally by article.Present invention fortune
Dynamic freedom degree is high, strong flexibility, and urgent article delivers that precision is high and distributing procedure is steady, highly-safe, high-efficient, cost
It is low.
Referring to Fig. 2, being rotor assemblies schematic illustration provided in an embodiment of the present invention, it includes propeller 5.1, spiral
Paddle swivel bearing 5.2, propeller carrier 5.3 and propeller rotating electric machine 5.4；The Internal and external cycle of propeller swivel bearing 5.2
It is fixed respectively with propeller 5.1 and 5.3 bolt of propeller carrier, the body of propeller rotating electric machine 5.4 is bolted
On propeller carrier 5.3, output shaft and propeller 5.1 are keyed, and pass through baffle and bolt axially position；Propeller
5.4 output shaft of rotating electric machine, around the rotary motion of its axis, drives propeller 5.1 to carry relative to propeller relative to its body
Frame 5.3 rotates, and forms the power perpendicular to 5 plane of rotor assemblies by the reaction force of air, is the urgent object of unmanned plane formula
The mobile offer precondition of the accurate delivery device of product.
Referring to Fig. 3, being rotor pose adjustment assembly principle schematic diagram provided in an embodiment of the present invention, it includes rotor fortune
Dynamic typed ball bearing pair 6.1, rotor movement telescopic shaft 6.2, rotor move hydraulic flexural pivot 6.3 and rotor pose adjusting seat 6.4；Rotor fortune
Dynamic typed ball bearing pair 6.1 has three groups, and 120 degree of fixing end interval is welded on propeller carrier 5.3；Rotor moves hydraulic flexural pivot
6.3 have three groups, and 120 degree of fixing end interval is welded in rotor pose adjusting seat 6.4；Rotor movement telescopic shaft 6.2 has three groups,
Its both ends moves 6.1 movable end of typed ball bearing pair with rotor respectively and rotor moves hydraulic 6.3 movable end of flexural pivot and welds together, thus
Parallel pose adjustment device is constituted, rotor moves hydraulic 6.3 movable end of flexural pivot and is secured relative to it end around its center point times
The rotary motion of meaning axis, in conjunction with rotor movement 6.2 one end of telescopic shaft relative to the other end along the linear movement of its axis, flexibly
Pose of the propeller carrier 5.3 relative to rotor pose adjusting seat 6.4 is adjusted, so as to adjust the born air of rotor assemblies 5
The direction of reaction force, then by the revolving speed of propeller rotating electric machine 5.4 come the size of corrective action power, so that nothing be adjusted flexibly
The whole stress of the accurate delivery device of the man-machine urgent article of formula is realized movement and hovering under many attitude, is passed rapidly through
Barrier reaches designated position；In addition, the upper circular arc of rotor pose adjusting seat 6.4 is small compared with the radius of lower circular arc, air-flow flows through
Faster, according to bernoulli effect, air pressure suffered by lower surface is bigger compared with upper surface for the speed of upper surface, to generate a support
Lifting force, motor can separate more power for promoting, make the movement speed of the accurate delivery device of the urgent article of unmanned plane formula
Faster.
Referring to Fig. 4, being rotor tilting component schematic illustration provided in an embodiment of the present invention, it includes rotor pitch arm
2.1, rotor pitch bearing 2.2, rotor pitching motor 2.3 and rotor pitching pedestal 2.4；Rotor pitch arm 2.1 and rotor position
Appearance adjusting seat 6.4 is welded and fixed, the Internal and external cycle of rotor pitch bearing 2.2 respectively with rotor pitch arm 2.1 and rotor pitching pedestal
2.4 bolts are fixed, and the body of rotor pitching motor 2.3 is bolted on rotor pitching pedestal 2.4, output shaft and rotation
Wing pitch arm 2.1 is keyed；2.3 output shaft of rotor pitching motor, around the rotary motion of its axis, passes through rotor with respect to its body
Pitch arm 2.1 drives rotor pose adjusting seat 6.4 to rotate around the axis of rotor pitching motor 2.3, to realize urgent article essence
On the one hand the adaptive pitching of quasi- each rotor relative flight platform 3 of delivery device improves the urgent article of unmanned plane formula and precisely delivers
On the other hand the freedom degree and flexibility of device during the motion execute object in the accurate delivery device of the urgent article of unmanned plane formula
The relative angle of each rotor Yu flying platform 3 is adjusted flexibly in product when precisely delivering task, avoid generating task execution process dry
It disturbs.
Referring to Fig. 5, be it is provided in an embodiment of the present invention for avoid generating task execution interfere used by rotor
Stick up status diagram.
Referring to Fig. 6, being more rotor angle adjustment assembly principle schematic diagrames provided in an embodiment of the present invention, it includes rotor
Arcuate movement sliding rail 4.1 and rotor arcuate movement sliding block 4.2；Rotor arcuate movement sliding rail 4.1 is 360 degree of round sliding rails, rotor
It arcuate movement sliding block 4.2 1 groups four, can be slided freely on rotor arcuate movement sliding rail 4.1；Rotor arcuate movement sliding rail
4.1 weld together with flying platform 3, and rotor arcuate movement sliding block 4.2 is fixed with 2.4 bolt of rotor pitching pedestal；Rotor arc
Shape moving slide block 4.2 moves freely along rotor arcuate movement sliding rail 4.1, drives corresponding rotor by rotor pitching pedestal 2.4
It is moved freely along rotor arcuate movement sliding rail 4.1, realizes the angle adjustment between adjacent rotor, when event occurs for one to two rotors
When barrier, the relative position of each rotor of the accurate delivery device of the urgent article of unmanned plane formula is adjusted, is continued with the moving equilibrium for reaching new
Work.
Referring to Fig. 7, being quadrotor motor pattern figure provided in an embodiment of the present invention.
Referring to Fig. 8, being the three rotor motor pattern figures provided in an embodiment of the present invention when a rotor breaks down.
Fig. 9 ~ 10 are please referred to, are the two rotor motor patterns provided in an embodiment of the present invention when two rotors break down
Figure.
Figure 11 ~ 14 are please referred to, are four kinds of motion state air under quadrotor motor pattern provided in an embodiment of the present invention
Reaction force schematic diagram.
Please refer to Figure 15, be hawser folding and unfolding assembly principle schematic diagram provided in an embodiment of the present invention, it include reel 7.1,
Reel swivel bearing 7.2, reel electric rotating base 7.3, reel rotating electric machine 7.4, hawser 7.5 use wirerope or high intensity
Chinlon material hawser, front wheel 7.6, cable guide 7.7 and rear wheel 7.8；Reel electric rotating base 7.3 and flying platform
3 bolts are fixed, and the Internal and external cycle of reel swivel bearing 7.2 is fixed with reel electric rotating base 7.3 and 7.1 bolt of reel respectively, volume
The body of cylinder electric rotating base 7.3 is bolted on reel electric rotating base 7.3, and output shaft and 7.1 key of reel connect
It connects；It is flat that the pulley base of front wheel 7.6, the pulley base of rear wheel 7.8 and cable guide 7.7 are bolted on flight
On platform 3,7.5 one end of hawser is fixed on reel 7.1, and other end winding reel 7.1 is after a few, then successively by front wheel 7.6
Hawser movable end positioning component is fixed on after the pulley body of pulley body, the pilot hole of cable guide 7.7 and rear wheel 7.8
On 8；With respect to its body around the rotary motion of its axis, band movable reel 7.1 revolves 7.4 output shaft of reel rotating electric machine around its axis
Turn, realize the adaptive folding and unfolding of hawser 7.5, hawser 7.5 is rolled into withdrawal when not in use, avoids the interference urgent article of unmanned plane formula
The movement of accurate delivery device, when use, release hawser 7.5, are carried to delivery location simultaneously by hawser movable end positioning component 8
It realizes and manually fixes, provide precondition for the accurate delivery of urgent article.
Figure 16 is please referred to, is hawser movable end positioning component schematic illustration provided in an embodiment of the present invention, it includes cable
Rope movable end fixing piece 8.1, movable end positioning unmanned plane 8.2 and positioning unmanned plane fixing seat 8.3；Hawser movable end fixing piece
8.1 one end and the movable end of hawser 7.5 are fixedly clamped, and the other end is fixed with movable end positioning 8.2 bolt of unmanned plane, position nobody
Machine fixing seat 8.3 is bolted on flying platform 3；When work, the premise of hawser 7.5 is released in hawser folding and unfolding component 7
Under, the movable end arrival that movable end positioning unmanned plane 8.2 carries hawser 7.5 need to carry out the position of article delivery and by manually by it
It is steady fixed, precondition is provided for the accurate delivery of urgent article；When not working, movable end positions unmanned plane 8.2 by determining
Position unmanned plane fixing seat 8.3 is realized fixes with the position of flying platform 3, prevents it from occurring in the motion process of flying platform 3
It falls.
Figure 17 is please referred to, is that article provided in an embodiment of the present invention delivers assembly principle schematic diagram, it includes supply case arc
Shape telecontrol equipment 9.1, supply case 9.2, supply case end cap 9.3, lower magnet fixing member 9.4, lower part electromagnet 9.5, top electromagnetism
Iron 9.6, upper magnet fixing member 9.7, telescopic shaft 9.8, hydraulic flexural pivot 9.9 and hawser moving member 9.10；Supply case arcuate movement
Device 9.1 can be made of 360 degree of round sliding rails and a series of built-in driving devices along the sliding block that sliding rail moves freely, supply case arc
The sliding rail of shape telecontrol equipment 9.1 is fixed with 3 bolt of flying platform, and the sliding block of supply case arc movement device 9.1 and lower magnet are solid
Determine 9.4 bolt of part to fix, lower magnet fixing member 9.4 is fixed with 9.5 bolt of lower part electromagnet again；Hawser moving member 9.10 is built-in to be driven
Dynamic device, can move freely along hawser 7.5, the fixing end and movable end of hydraulic flexural pivot 9.9 respectively with hawser moving member 9.10 and
The fixing end of telescopic shaft 9.8 welds together, and the movable end of telescopic shaft 9.8 welds together with upper magnet fixing member 9.7 again, on
Portion's electromagnet 9.6 is bolted on magnet fixing member 9.7；Supply case 9.2 and supply case end cap 9.3 can pass through screw thread
Fixed, the material of main part of supply case 9.2 and supply case end cap 9.3 is rigid plastics, the bottom and supply case end of supply case 9.2
The outside of lid 9.3 is embedded with round stainless steel plate, the lower part after enabling supply case 9.2 and supply case end cap 9.3 to be energized respectively
Electromagnet 9.5 and the absorption of top electromagnet 9.6 are fixed；Hydraulic 9.9 movable end of flexural pivot is appointed with respect to its fixing end around its center point
The rotary motion of meaning axis passes through upper magnet along the linear movement of its axis with respect to its fixing end in conjunction with 9.8 movable end of telescopic shaft
Fixing piece 9.7 drives the adaptive pose adjustment for realizing top electromagnet 9.6；In transportational process, supply case 9.2 and supply case end
Lid 9.3 is screwed, and lower part electromagnet 9.5 is bonded and is powered with 9.2 bottom of supply case, supply case 9.2 is smoothly adsorbed solid
It is scheduled on flying platform 3；After reaching delivery service area, incited somebody to action in hawser folding and unfolding component 7 and 8 cooperating of hawser movable end positioning component
7.5 movable end of hawser is sent to delivery location and under the premise of realizing artificial fix, supply case arc movement device 9.1, telescopic shaft
9.8 and 9.9 collective effect of hydraulic flexural pivot make top electromagnet 9.6 with need to deliver supply case 9.2 supply case end cap 9.3 paste
Merge and be powered, then lower part electromagnet 9.5 powers off, so that the supply case 9.2 that need to be delivered smoothly is adsorbed with top electromagnet 9.6
Fixed, subsequently telescopic shaft 9.8 drives the supply case 9.2 that need to be delivered to be detached from lower part electromagnet 9.5, finally by hawser moving member
It precisely delivers 9.10 band trend designated positions；Deliver reach after, top electromagnet 9.6 power-off by supply case 9.2 put down then by
Hawser moving member 9.10, which drives, to be returned to carry out the delivery of next supply case 9.2, and personnel open supply case end cap 9.3 and mend
It gives；After one place is delivered, the position of flying platform 3 and movable end positioning unmanned plane 8.2 is adjusted, next place is carried out
Urgent article is precisely delivered.
Figure 18 is please referred to, is the accurate delivery status schematic diagram of urgent article provided in an embodiment of the present invention.
It is obvious to a person skilled in the art that invention is not limited to the details of the above exemplary embodiments, Er Qie
In the case where without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the present invention is by appended power
Benefit requires rather than above description limits, it is intended that all by what is fallen within the meaning and scope of the equivalent elements of the claims
Variation is included within the present invention.Any reference signs in the claims should not be construed as limiting the involved claims.
Claims (4)
1. a kind of accurate delivery device of relief supplies, which is characterized in that it includes sighting device (1), flying platform (3), hawser
Folding and unfolding component (7), hawser movable end positioning component (8) and article deliver component (9), and it is stranded to can be used for disaster area, region of war, personnel
Etc. the accurate delivery of goods and materials, food, drinking water, first-aid dressing and other items under situations；By sighting device (1) provide environmental information into
Row control quickly reaches specified region by flying platform (3)；Then by hawser folding and unfolding component (7) folding and unfolding hawser, pass through cable
Hawser movable end is accurately sent to delivery location and by manually fixing by rope movable end positioning component (8), is delivered finally by article
Component (9) carries out the accurate delivery of urgent article.
2. the accurate delivery device of a kind of relief supplies according to claim 1, which is characterized in that the hawser folding and unfolding group
Part (7) includes reel (7.1), reel swivel bearing (7.2), reel electric rotating base (7.3), reel rotating electric machine (7.4), cable
Rope (7.5), front wheel (7.6), cable guide (7.7) and rear wheel (7.8)；Reel electric rotating base (7.3) and flight
Platform (3) bolt is fixed, the Internal and external cycle of reel swivel bearing (7.2) respectively with reel electric rotating base (7.3) and reel (7.1)
Bolt is fixed, and the body of reel electric rotating base (7.3) is bolted on reel electric rotating base (7.3), output
Axis and reel (7.1) are keyed；The pulley base and cable guide of the pulley base of front wheel (7.6), rear wheel (7.8)
(7.7) it is bolted on flying platform (3), hawser (7.5) one end is fixed on reel (7.1), other end coiling
Cylinder (7.1) is after a few, then successively by the pulley body of front wheel (7.6), the pilot hole and rear wheel of cable guide (7.7)
(7.8) it is fixed on hawser movable end positioning component (8) after pulley body；Reel rotating electric machine (7.4) output shaft is with respect to it
Body is rotated about the axis thereof around the rotary motion of its axis with movable reel (7.1), realizes the adaptive folding and unfolding of hawser (7.5), no
Hawser (7.5) is rolled into withdrawal when use, avoids the movement of the interference accurate delivery device of the urgent article of unmanned plane formula, it will when use
Hawser (7.5) is released, and is carried by hawser movable end positioning component (8) to delivery location and realization is manually fixed, be urgent article
Accurate delivery provide precondition.
3. the accurate delivery device of a kind of relief supplies according to claim 1, which is characterized in that the hawser movable end
Positioning component (8) includes that hawser movable end fixing piece (8.1), movable end positioning unmanned plane (8.2) and positioning unmanned plane are fixed
Seat (8.3)；Hawser movable end fixing piece (8.1) one end and the movable end of hawser (7.5) are fixedly clamped, and the other end and movable end are fixed
Position unmanned plane (8.2) bolt is fixed, and positioning unmanned plane fixing seat (8.3) is bolted on flying platform (3)；Work
When, under the premise of hawser folding and unfolding component (7) releases hawser (7.5), movable end positions unmanned plane (8.2) and carries hawser (7.5)
Movable end reach the position that need to carry out article delivery and by manually that it is steady fixed, provided for accurate deliver of urgent article
Precondition；When not working, it is flat by positioning unmanned plane fixing seat (8.3) realization and flight that movable end positions unmanned plane (8.2)
The position of platform (3) is fixed, and prevents it from falling in the motion process of flying platform (3).
4. the accurate delivery device of a kind of relief supplies according to claim 1, which is characterized in that the article delivery group
Part (9) includes supply case arc movement device (9.1), supply case (9.2), supply case end cap (9.3), lower magnet fixing member
(9.4), lower part electromagnet (9.5), top electromagnet (9.6), upper magnet fixing member (9.7), telescopic shaft (9.8), hydraulic flexural pivot
(9.9) and hawser moving member (9.10)；Supply case arc movement device (9.1) is by 360 degree of round sliding rails and a series of built-in
Driving device can be along the sliding block composition that sliding rail moves freely, sliding rail and flying platform (3) of supply case arc movement device (9.1)
Bolt is fixed, and the sliding block of supply case arc movement device (9.1) is fixed with lower magnet fixing member (9.4) bolt, and lower magnet is fixed
Part (9.4) is fixed with lower part electromagnet (9.5) bolt again；Driving device built in hawser moving member (9.10), can be along hawser (7.5)
It moves freely, the fixing end of hydraulic flexural pivot (9.9) and movable end are consolidated with hawser moving member (9.10) and telescopic shaft (9.8) respectively
Fixed end welds together, and the movable end of telescopic shaft (9.8) welds together with upper magnet fixing member (9.7) again, top electromagnet
(9.6) it is bolted on magnet fixing member (9.7)；Supply case (9.2) and supply case end cap (9.3) can pass through screw thread
Fixed, the material of main part of supply case (9.2) and supply case end cap (9.3) is rigid plastics, the bottom of supply case (9.2) and benefit
Be embedded with round stainless steel plate to the outside of case end cap (9.3), make supply case (9.2) and supply case end cap (9.3) can respectively by
Lower part electromagnet (9.5) and top electromagnet (9.6) absorption after energization are fixed；Hydraulic flexural pivot (9.9) movable end is solid with respect to it
Fixed end bypasses the rotary motion of any axis of its center point, in conjunction with telescopic shaft (9.8) movable end with respect to its fixing end along its axis
Linear movement, pass through upper magnet fixing member (9.7) drive realize top electromagnet (9.6) adaptive pose adjustment；Transport
In the process, supply case (9.2) and supply case end cap (9.3) are screwed, lower part electromagnet (9.5) and supply case (9.2) bottom
It is bonded and is powered, supply case (9.2) is smoothly absorbed and fixed on flying platform (3)；After reaching delivery service area, received in hawser
Component (7) and hawser movable end positioning component (8) cooperating is put to send hawser (7.5) movable end to delivery location and realize people
Under the premise of work is fixed, supply case arc movement device (9.1), telescopic shaft (9.8) and hydraulic flexural pivot (9.9) collective effect make
It obtains top electromagnet (9.6) to be bonded and be powered with the supply case end cap (9.3) that need to deliver supply case (9.2), then lower part electromagnetism
Iron (9.5) power-off is subsequently stretched so that smoothly absorption is fixed for the supply case (9.2) that need to be delivered and top electromagnet (9.6)
Axis (9.8) drives the supply case (9.2) that need to be delivered to be detached from lower part electromagnet (9.5), is finally driven by hawser moving member (9.10)
It is precisely delivered to designated position；It delivers after reaching, top electromagnet (9.6) power-off puts down supply case (9.2) then by hawser
Moving member (9.10), which drives, to be returned to carry out the delivery of next supply case (9.2), and personnel open supply case end cap (9.3) and mend
It gives；After one place is delivered, the position of flying platform (3) and movable end positioning unmanned plane (8.2) is adjusted, is carried out nextly
The urgent article of point is precisely delivered.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811149426.8A CN109334961A (en) | 2018-09-29 | 2018-09-29 | A kind of accurate delivery device of relief supplies |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811149426.8A CN109334961A (en) | 2018-09-29 | 2018-09-29 | A kind of accurate delivery device of relief supplies |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109334961A true CN109334961A (en) | 2019-02-15 |
Family
ID=65307926
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811149426.8A Pending CN109334961A (en) | 2018-09-29 | 2018-09-29 | A kind of accurate delivery device of relief supplies |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109334961A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109334963A (en) * | 2018-09-30 | 2019-02-15 | 江苏师范大学 | A kind of accurate dispenser of unmanned plane formula express delivery take-away |
| US20210163151A1 (en) * | 2016-08-20 | 2021-06-03 | Modern Technology Solutions, Inc. | Anchored tether for delivering personnel and cargo from a fixed-wing aircraft |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204341394U (en) * | 2014-12-24 | 2015-05-20 | 马鞍山市靓马航空科技有限公司 | The many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue |
| CN204415733U (en) * | 2015-01-19 | 2015-06-24 | 青岛科技大学 | A kind of express delivery dispensing unmanned plane |
| CN106041980A (en) * | 2016-08-08 | 2016-10-26 | 江苏捷帝机器人股份有限公司 | Mechanical arm for mounting of spring in machine and working method of mechanical arm |
| US20160340006A1 (en) * | 2015-05-19 | 2016-11-24 | Rujing Tang | Unmanned aerial vehicle system and methods for use |
| US20170066530A1 (en) * | 2015-10-27 | 2017-03-09 | Guided Systems Technologies, Inc. | Method and apparatus for remote, interior inspection of cavities using an unmanned aircraft system |
| CN206187334U (en) * | 2016-11-18 | 2017-05-24 | 哈尔滨理工大学 | Four -rotor aircraft |
| CN107512397A (en) * | 2017-09-08 | 2017-12-26 | 徐秀芳 | One kind investigation BFR |
| CN107626058A (en) * | 2017-11-13 | 2018-01-26 | 苏州市皎朝纳米科技有限公司 | A kind of structural fire fighting device |
-
2018
- 2018-09-29 CN CN201811149426.8A patent/CN109334961A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204341394U (en) * | 2014-12-24 | 2015-05-20 | 马鞍山市靓马航空科技有限公司 | The many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue |
| CN204415733U (en) * | 2015-01-19 | 2015-06-24 | 青岛科技大学 | A kind of express delivery dispensing unmanned plane |
| US20160340006A1 (en) * | 2015-05-19 | 2016-11-24 | Rujing Tang | Unmanned aerial vehicle system and methods for use |
| US20170066530A1 (en) * | 2015-10-27 | 2017-03-09 | Guided Systems Technologies, Inc. | Method and apparatus for remote, interior inspection of cavities using an unmanned aircraft system |
| CN106041980A (en) * | 2016-08-08 | 2016-10-26 | 江苏捷帝机器人股份有限公司 | Mechanical arm for mounting of spring in machine and working method of mechanical arm |
| CN206187334U (en) * | 2016-11-18 | 2017-05-24 | 哈尔滨理工大学 | Four -rotor aircraft |
| CN107512397A (en) * | 2017-09-08 | 2017-12-26 | 徐秀芳 | One kind investigation BFR |
| CN107626058A (en) * | 2017-11-13 | 2018-01-26 | 苏州市皎朝纳米科技有限公司 | A kind of structural fire fighting device |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20210163151A1 (en) * | 2016-08-20 | 2021-06-03 | Modern Technology Solutions, Inc. | Anchored tether for delivering personnel and cargo from a fixed-wing aircraft |
| US11667394B2 (en) * | 2016-08-20 | 2023-06-06 | Modern Technology Solutions, Inc. | Anchored tether for delivering personnel and cargo from a fixed-wing aircraft |
| CN109334963A (en) * | 2018-09-30 | 2019-02-15 | 江苏师范大学 | A kind of accurate dispenser of unmanned plane formula express delivery take-away |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109334962A (en) | A kind of accurate delivery device of urgent article of unmanned plane formula | |
| EP3268275B1 (en) | Adjustable weight distribution for multi-rotor helicopter drone | |
| AU711268B2 (en) | Aircraft | |
| CN108814404A (en) | A kind of unmanned plane formula high-altitude glass-cleaning machine device people | |
| CN109334961A (en) | A kind of accurate delivery device of relief supplies | |
| CN108454847B (en) | Rotor wing attitude adjusting device and multi-rotor wing unmanned aerial vehicle comprising same | |
| CN103078184A (en) | Plate-like antenna adjustment device | |
| CN110217389A (en) | A kind of coaxial double-rotary wing unmanned plane that vector verts | |
| CN109094779A (en) | A kind of electric inspection process flying robot | |
| CN110279337A (en) | A kind of unmanned plane formula high-altitude glass-cleaning machine device people | |
| CN109178768A (en) | A kind of double rolling bed transportation systems and its working method | |
| CN110077633B (en) | Angle and eccentric adjusting device and microgravity rolling state simulation system | |
| CN109008772A (en) | A kind of high-altitude glass-cleaning machine device people | |
| CN108316167A (en) | A kind of rotary unmanned plane airplane parking area | |
| CN106379534A (en) | Spin control system and aircraft | |
| CN205802525U (en) | A kind of portable bag bag and bulk cargo multipurpose ship loader | |
| CN109334963A (en) | A kind of accurate dispenser of unmanned plane formula express delivery take-away | |
| CN207630893U (en) | A kind of land and air double-used quadrotor | |
| CN108482691B (en) | A kind of break catching apparatus and unmanned plane | |
| CN110286422A (en) | XCTD probe is automatic puts in device and is used rotating base | |
| CN109453924A (en) | A kind of tank body rotary spraying device | |
| CN109808886A (en) | A kind of unmanned plane waters deliverance apparatus | |
| CN109334964A (en) | A kind of unmanned plane formula light of stage audio device | |
| CN109407458B (en) | Aerial projection device | |
| CN212671088U (en) | Unmanned aerial vehicle sprayer |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190215 |