CN109334964A - A kind of unmanned plane formula light of stage audio device - Google Patents
A kind of unmanned plane formula light of stage audio device Download PDFInfo
- Publication number
- CN109334964A CN109334964A CN201811163615.0A CN201811163615A CN109334964A CN 109334964 A CN109334964 A CN 109334964A CN 201811163615 A CN201811163615 A CN 201811163615A CN 109334964 A CN109334964 A CN 109334964A
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- CN
- China
- Prior art keywords
- rotor
- unmanned plane
- hawser
- movable end
- component
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Classifications
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- 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
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- 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
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- 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
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- 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
- B64D47/00—Equipment not otherwise provided for
-
- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
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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
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- 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
Abstract
The invention discloses a kind of unmanned plane formula light of stage audio device, it is characterized in that, it includes sighting device (1), rotor tilting component (2), flying platform (3), more rotor angles adjustment component (4), rotor assemblies (5), rotor pose adjustment component (6), hawser folding and unfolding component (7), hawser movable end positioning component (8), the selection of keynote sound and transports component (9) and king light optical assembly (10).Freedom of motion of the invention is high, strong flexibility, light and it is acoustic be arranged it is high-efficient, at low cost, adaptable, be easy to adjust.
Description
Technical field
The present invention relates to a kind of lighting sound device, specifically a kind of unmanned plane formula light of stage audio device.
Background technique
When setting up a makeshift stage, it need to take a substantial amount of time and carry out light and acoustic setting with manpower, and be arranged
It is not easy to adjust after the completion, risk is big, at high cost, low efficiency.
Summary of the invention
In view of the above existing problems in the prior art, the present invention provides a kind of unmanned plane formula light of stage audio device,
It is characterized in that, it includes sighting device, rotor tilting component, flying platform, more rotor angles adjustment component, rotor assemblies, rotation
Wing pose adjusts component, hawser folding and unfolding component, hawser movable end positioning component, keynote and rings selection and transport component and key lights
Component.The present invention can be used for the light of makeshift stage and acoustics is arranged, and provides environmental information by sighting device and is controlled
System adjusts component by rotor tilting component, rotor assemblies and rotor pose and controls unmanned plane formula light of stage audio device
It circumvents barrier and quickly reaches specified region；Then by hawser folding and unfolding component folding and unfolding hawser, pass through hawser movable end positioning group
Part, keynote, which are rung, chooses and transports component and king light optical assembly progress light of stage and acoustic setting.Fortune of the invention
Dynamic freedom degree is high, strong flexibility, light and it is acoustic be arranged it is high-efficient, at low cost, adaptable, be easy to adjust.
To achieve the goals above, the technical solution adopted by the present invention is that: a kind of unmanned plane formula light of stage audio device,
It is characterized in that, it include sighting device, rotor tilting component, flying platform, more rotor angles adjustment component, rotor assemblies,
Rotor pose adjusts component, hawser folding and unfolding component, hawser movable end positioning component, keynote and rings selection and transport component and king light
Optical assembly.The present invention can be used for the light of makeshift stage and acoustics is arranged, and provides environmental information by sighting device and carries out
Control adjusts component by rotor tilting component, rotor assemblies and rotor pose and controls unmanned plane formula light of stage sound equipment dress
It sets and circumvents barrier and quickly reach specified region；Then it by hawser folding and unfolding component folding and unfolding hawser, is positioned by hawser movable end
Component, keynote, which are rung, chooses and transports component and king light optical assembly progress light of stage and acoustic setting.Of the invention
Freedom of motion is high, strong flexibility, light and it is acoustic be arranged it is high-efficient, at low cost, adaptable, be easy to adjust.
The rotor assemblies include propeller, propeller swivel bearing, propeller carrier and propeller electric rotating
Machine；The Internal and external cycle of propeller swivel bearing is fixed with propeller and propeller carrier bolt respectively, propeller rotating electric machine
Body is bolted on propeller carrier, and output shaft and propeller are keyed, and axial by baffle and bolt
Positioning；Propeller rotating electric machine output shaft, around the rotary motion of its axis, drives propeller relative to spiral relative to its body
The rotation of paddle carrier forms the power perpendicular to rotor assemblies plane by the reaction force of air, is unmanned plane formula stage
The mobile offer precondition of lighting sound device.
The rotor pose adjustment component includes that rotor moves typed ball bearing pair, rotor moves telescopic shaft, rotor movement is hydraulic
Flexural pivot and rotor pose adjusting seat；Rotor movement typed ball bearing pair has three groups, and 120 degree of fixing end interval is welded on propeller carrying
On frame；Rotor, which moves hydraulic flexural pivot, three groups, and 120 degree of fixing end interval is welded in rotor pose adjusting seat；Rotor movement
Telescopic shaft has three groups, and both ends move typed ball bearing pair movable end with rotor respectively and rotor moves hydraulic flexural pivot movable end and is welded on one
It rises, to constitute parallel pose adjustment device, rotor moves hydraulic flexural pivot movable end and is secured relative to it end around its centre of sphere
The rotary motion of any axis of point, in conjunction with rotor movement telescopic shaft one end relative to the other end along the linear movement of its axis, spirit
Pose of the adjustment propeller carrier living relative to rotor pose adjusting seat, so as to adjust the born air reaction of rotor assemblies
The direction of power, then by the revolving speed of propeller rotating electric machine come the size of corrective action power, so that unmanned plane formula dance be adjusted flexibly
The whole stress of desk lamp light audio device realizes movement and hovering under many attitude, passes rapidly through barrier arrival and refers to
Positioning is set；In addition, the upper circular arc of rotor pose adjusting seat is small compared with the radius of lower circular arc, air-flow flows through the speed of upper surface more
Fastly, according to bernoulli effect, air pressure suffered by lower surface is bigger compared with upper surface, so that generating one lifts power, motor can be with
More power are separated for promoting, make the movement speed of unmanned plane formula light of stage audio device faster.
The rotor tilting component includes that rotor pitch arm, rotor pitch bearing, rotor pitching motor and rotor are bowed
Face upward pedestal；Rotor pitch arm is welded and fixed with rotor pose adjusting seat, the Internal and external cycle of rotor pitch bearing respectively with rotor pitching
Arm and rotor pitching foundation bolt are fixed, and the body of rotor pitching motor is bolted on rotor pitching pedestal, defeated
Shaft and rotor pitch arm are keyed；Rotor pitching motor output shaft, around the rotary motion of its axis, passes through rotation with respect to its body
Wing pitch arm drives rotor pose adjusting seat to rotate around the axis of rotor pitching motor, to realize unmanned plane formula light of stage sound
The adaptive pitching of each rotor relative flight platform of device is rung, unmanned plane formula light of stage audio device is on the one hand improved and is moving
On the other hand freedom degree and flexibility in the process execute the setting of light and sound equipment in unmanned plane formula light of stage audio device
The relative angle of each rotor and flying platform is adjusted flexibly when task, avoids generating interference to task execution process.
More rotor angles adjustment component includes rotor arcuate movement sliding rail and rotor arcuate movement sliding block；Rotor arc
It is 360 degree of round sliding rails that shape, which moves sliding rail, rotor arcuate movement sliding block one group four, can be on rotor arcuate movement sliding rail certainly
Such as sliding；Rotor arcuate movement sliding rail welds together with flying platform, rotor arcuate movement sliding block and rotor pitching pedestal spiral shell
Bolt is fixed；Rotor arcuate movement sliding block moves freely along rotor arcuate movement sliding rail, is driven by rotor pitching pedestal corresponding
Rotor moves freely along rotor arcuate movement sliding rail, realizes the angle adjustment between adjacent rotor, when one to two rotors occur
When failure, the relative position of each rotor of unmanned plane formula light of stage audio device is adjusted, work is continued with the moving equilibrium for reaching new
Make.
The hawser folding and unfolding component has two sets and symmetrically placed；It includes reel, reel swivel bearing, reel electric rotating
Base, reel rotating electric machine, hawser, pulley and cable guide；Reel electric rotating base is fixed with flying platform bolt, volume
The Internal and external cycle of cylinder swivel bearing is fixed with reel electric rotating base and reel bolt respectively, and the body of reel rotating electric machine passes through spiral shell
Bolt is fixed on reel electric rotating base, and output shaft and reel are keyed；The pulley base and cable guide of pulley pass through
Bolt is fixed on flying platform, and hawser one end is fixed on reel, and other end winding reel is after a few, then successively leads by hawser
The pulley body of pilot hole and pulley to part is fixed on hawser movable end positioning component later；Reel rotating electric machine output shaft phase
To its body around the rotary motion of its axis, band movable reel is rotated about the axis thereof, and realizes the adaptive folding and unfolding of hawser, when not in use
Hawser is rolled into withdrawal, avoids the movement of interference unmanned plane formula light of stage audio device, when use releases hawser, in conjunction with cable
Rope movable end positioning component, keynote ring the movement realization light of stage and sound equipment effect for choosing and transporting component and king light optical assembly
The setting of fruit.
The hawser movable end positioning component includes hawser movable end fixing piece, movable end positioning unmanned plane, positioning nothing
Man-machine fixing seat, secondary lamps and lanterns, secondary lamps and lanterns wave hydraulic flexural pivot and secondary sound equipment；The work of hawser movable end fixing piece one end and hawser
Moved end is fixedly clamped, and the other end positions unmanned machine bolt with movable end and fixes, and positioning unmanned plane fixing seat is bolted on
On flying platform；Secondary sound equipment and secondary lamp power is small, small in size, light weight, secondary sound equipment is bolted on movable end positioning
On unmanned plane, the movable end that secondary lamps and lanterns wave hydraulic flexural pivot with secondary lamps and lanterns is welded and fixed, and secondary lamps and lanterns wave the fixation of hydraulic flexural pivot
End is welded on flying platform again, and secondary lamps and lanterns wave hydraulic flexural pivot movable end with respect to its fixing end around any axis of its center point
Rotary motion, drive and realize that secondary lamps and lanterns are adjusted with respect to the adaptive pose of movable end positioning unmanned plane；When work, received in hawser
Under the premise of putting component releasing hawser, one side movable end positions the installation that unmanned plane drives the movable end of hawser to reach main sound box
Position and by manually fixing rings in conjunction with keynote and chooses and transport the work of component and realize the setting of main sound box effect, another party
Face, after the completion of main sound box configuration, secondary sound equipment and secondary lamps and lanterns under the drive of movable end positioning unmanned plane, cooperation keynote ring choose and
Stage entirety light and acoustic setting are realized in the work for transporting component and king light optical assembly；When not working, movable end is fixed
Position unmanned plane is realized by positioning unmanned plane fixing seat and is fixed with the position of flying platform, its being moved through in flying platform is prevented
It is fallen in journey.
The keynote ring choose and transport component include main sound box, main sound box arc movement device, lower magnet fixing member,
Keynote lower box part electromagnet, keynote upper box part electromagnet, upper magnet fixing member, upper magnet lift telescopic axis, upper magnet wave liquid
Pressure ball hinge and hawser moving member；Main sound box have it is multiple and can there are many type, power is big, volume is big, quality weight, bottom
It is embedded with stainless steel plate with top, the electromagnet after being energized is adsorbed；Main sound box arc movement device is by 360 degree of concentric strokings
Rail and a series of built-in drivings can pass through bolt along the sliding block composition that sliding rail moves freely, the sliding rail of main sound box arc movement device
Be fixed on flying platform, sliding block is fixed with lower magnet fixing member bolt, lower magnet fixing member again with keynote lower box part electromagnetism
Iron bolt is fixed；The built-in driving of hawser moving member, can move freely, upper magnet waves the fixing end and work of hydraulic flexural pivot along hawser
Fixing end of the moved end respectively with hawser moving member and upper magnet lift telescopic axis is welded and fixed, upper magnet lift telescopic axis it is another
End is welded and fixed with upper magnet fixing member, and upper magnet fixing member is fixed with keynote upper box part electromagnet bolt again；Acoustics is set
Before setting, the main sound box of suitable quantity suitable type is chosen according to demand, they are placed on one by one on keynote lower box part electromagnet
And being powered fixes the two absorption；Acoustics be arranged when, main sound box arc movement device drive main sound box by them successively
It is moved to main sound box and transports starting point, then movable end positioning unmanned plane drives the movable end of hawser to reach the installation that current keynote is rung
Position and by manually fixing, next upper magnet lift telescopic axis, upper magnet waves hydraulic flexural pivot and hawser moving member is common
Effect is bonded keynote upper box part electromagnet with the top of main sound box, and subsequently keynote lower box part electromagnet powers off, on main sound box
Electromagnet energization in portion's makes it adsorb fixation with main sound box, and finally upper magnet lift telescopic axis drives main sound box to be detached from keynote lower box part
Electromagnet, hawser moving member drive main sound box to be moved to installation site and are configured；It so repeats, until completing all main sound boxs
Position setting, the secondary sound equipment of position can be adjusted in real time in conjunction with by movable end positioning UAV flight, realize stage entirety sound
Ring the setting of effect.
The king light optical assembly includes king light tool, king light tool waves hydraulic flexural pivot and king light has arc movement device；
King light have multiple and type is various, power is big, volume is big, quality weight, king light have arc movement device have 360 degree of circle sliding rails
It can be bolted on winged along the sliding block composition that sliding rail moves freely, the sliding rail of king light tool arc movement device with built-in driving
On row platform, king light has sliding block and the master that the fixing end for waving hydraulic flexural pivot and movable end have arc movement device with king light respectively
Lamps and lanterns are welded and fixed；King light has freely movement of the arc movement device sliding block with respect to its sliding rail, waves hydraulic ball in conjunction with king light tool
The rotary motion that movable end bypasses any axis of its center point with respect to its fixing end is cut with scissors, collective effect realizes that king light has relative flight
The adaptive pose of platform adjusts, and the real-time pose of movement and secondary lamps and lanterns in conjunction with flying platform adjusts, and realizes that stage is whole
The setting of lighting effects.
The present invention is a kind of unmanned plane formula light of stage audio device, which is characterized in that it includes that sighting device, rotor are bowed
Face upward component, flying platform, more rotor angles adjustment component, rotor assemblies, rotor pose adjustment component, hawser folding and unfolding component, cable
Rope movable end positioning component, keynote, which are rung, chooses and transports component and king light optical assembly.The present invention can be used for the lamp of makeshift stage
Light and acoustics are arranged, and provide environmental information by sighting device and are controlled, by rotor tilting component, rotor assemblies with
And rotor pose adjustment component control unmanned plane formula light of stage audio device circumvents barrier and quickly reaches specified region；Then
By hawser folding and unfolding component folding and unfolding hawser, is rung by hawser movable end positioning component, keynote and choose and transport component and king light
Optical assembly carries out light of stage and acoustic setting.Freedom of motion of the invention is high, strong flexibility, and light and sound equipment are imitated
The setting of fruit is high-efficient, it is at low cost, adaptable, be easy to adjust.
Detailed description of the invention
Fig. 1 is a kind of unmanned plane formula light of stage audio device schematic illustration 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, the selection of keynote sound and transport
Component, 10, king light optical assembly.
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, pulley, 7.7, cable guide.
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, 8.4,
Secondary lamps and lanterns, 8.5, secondary lamps and lanterns wave hydraulic flexural pivot, 8.6, secondary sound equipment.
Figure 17 is that keynote provided in an embodiment of the present invention rings selection and transports assembly principle schematic diagram；
In figure: 9.1, main sound box, 9.2, main sound box arc movement device, 9.3, lower magnet fixing member, 9.4, keynote lower box part electricity
Magnet, 9.5, keynote upper box part electromagnet, 9.6, upper magnet fixing member, 9.7, upper magnet lift telescopic axis, 9.8, upper magnet shakes
Put hydraulic flexural pivot, 9.9, hawser moving member.
Figure 18 is key lights assembly principle schematic diagram provided in an embodiment of the present invention；
In figure: 10.1, king light has, 10.2, king light tool wave hydraulic flexural pivot, 10.3, king light have arc movement device.
Figure 19 is main sound box shipping situation schematic diagram provided in an embodiment of the present invention.
Figure 20 is expanded schematic diagram of the 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, be a kind of unmanned plane formula light of stage audio device schematic illustration provided in an embodiment of the present invention,
It includes sighting device 1, rotor tilting component 2, flying platform 3, more rotor angles adjustment component 4, rotor assemblies 5, rotor position
Appearance adjusts component 6, hawser folding and unfolding component 7, hawser movable end positioning component 8, keynote and rings selection and transport component 9 and key lights
Component 10.The present invention can be used for the light of makeshift stage and acoustics is arranged, and provides environmental information by sighting device 1 and carries out
Control adjusts component 6 by rotor tilting component 2, rotor assemblies 5 and rotor pose and controls unmanned plane formula light of stage sound equipment
Device circumvents barrier and quickly reaches specified region；Then fixed by hawser movable end by 7 folding and unfolding hawser of hawser folding and unfolding component
Hyte part 8, keynote, which are rung, chooses and transports component 9 and the progress light of stage of king light optical assembly 10 and acoustic setting.This
The freedom of motion of invention is high, strong flexibility, light and it is acoustic be arranged it is high-efficient, at low cost, adaptable, be easy to adjust
It is whole.
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 unmanned plane formula stage lighting
The mobile offer precondition of light audio device.
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 man-machine formula light of stage audio device realizes movement and hovering under many attitude, passes rapidly through obstacle
Object 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 table
Faster, according to bernoulli effect, air pressure suffered by lower surface is bigger compared with upper surface for the speed in face, lifts to generate one
Power, motor can separate more power for promoting, make the movement speed of unmanned plane formula light of stage audio device 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 that unmanned plane formula is waved
On the one hand the adaptive pitching of each rotor relative flight platform 3 of desk lamp light audio device improves unmanned plane formula light of stage sound equipment
The freedom degree and flexibility of device during the motion, on the other hand unmanned plane formula light of stage audio device execute light with
The relative angle of each rotor Yu flying platform 3 is adjusted flexibly when the setting task of sound equipment, avoids 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 unmanned plane formula light of stage audio device is adjusted, is worked on the moving equilibrium for reaching new.
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.
Figure 15 is please referred to, is hawser folding and unfolding assembly principle schematic diagram provided in an embodiment of the present invention, the hawser folding and unfolding
Component 7 has two sets and symmetrically placed, it includes reel 7.1, reel swivel bearing 7.2, reel electric rotating base 7.3, reel rotation
Rotating motor 7.4, hawser 7.5, pulley 7.6 and cable guide 7.7；Reel electric rotating base 7.3 and 3 bolt of flying platform are solid
Fixed, 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, reel electric rotating
The body of machine 7.4 is bolted on reel electric rotating base 7.3, and output shaft and reel 7.1 are keyed；Pulley 7.6
Pulley base and cable guide 7.7 be bolted on flying platform 3,7.5 one end of hawser is fixed on reel 7.1
On, other end winding reel 7.1 is after a few, then successively after the pulley body of the pilot hole Jing Guo cable guide 7.7 and pulley 7.6
It is fixed on hawser movable end positioning component 8；Rotation of 7.4 output shaft of reel rotating electric machine relative to its body around its axis is transported
Dynamic, band movable reel 7.1 rotates about the axis thereof, and realizes the adaptive folding and unfolding of hawser 7.5, hawser 7.5 is rolled withdrawal when not in use,
The movement of interference unmanned plane formula light of stage audio device is avoided, when use releases hawser 7.5, positions in conjunction with hawser movable end
Component 8, keynote ring selection and the movement of transport component 9 and king light optical assembly 10 realizes that light of stage is set with acoustic
It sets.
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, positioning unmanned plane fixing seat 8.3, secondary lamps and lanterns 8.4, secondary lamps and lanterns shake
Put hydraulic flexural pivot 8.5 and secondary sound equipment 8.6；8.1 one end of hawser movable end fixing piece and the movable end of hawser 7.5 are fixedly clamped,
The other end is fixed with movable end positioning 8.2 bolt of unmanned plane, and positioning unmanned plane fixing seat 8.3 is bolted on flying platform
On 3；Secondary sound equipment 8.6 and 8.4 power of secondary lamps and lanterns is small, small in size, light weight, it is fixed that secondary sound equipment 8.6 is bolted on movable end
On the unmanned plane 8.2 of position, the movable end that secondary lamps and lanterns 8.4 wave hydraulic flexural pivot 8.5 with secondary lamps and lanterns is welded and fixed, and secondary lamps and lanterns wave hydraulic
The fixing end of flexural pivot 8.5 is welded on again on flying platform 3, secondary lamps and lanterns wave hydraulic 8.5 movable end of flexural pivot with respect to its fixing end around
The rotary motion of any axis of its center point is crossed, drives and realizes the adaptive of the opposite movable end positioning unmanned plane 8.2 of secondary lamps and lanterns 8.4
Pose adjustment；When work, under the premise of hawser folding and unfolding component 7 releases hawser 7.5, one side movable end positions unmanned plane 8.2
The movable end of drive hawser 7.5 reaches the installation site of main sound box and by manually fixing, and rings selection and transport group in conjunction with keynote
The setting of main sound box effect is realized in the work of part 9, on the other hand, after the completion of main sound box configuration, secondary sound equipment 8.6 and secondary lamps and lanterns 8.4
Under the drive of movable end positioning unmanned plane 8.2, cooperation keynote rings selection and the work of transport component 9 and king light optical assembly 10 is real
Existing stage entirety light and acoustic setting；When not working, movable end positions unmanned plane 8.2 and is fixed by positioning unmanned plane
Seat 8.3 is realized to be fixed with the position of flying platform 3, prevents it from falling in the motion process of flying platform 3.
Figure 17 is please referred to, is that keynote provided in an embodiment of the present invention rings selection and transports assembly principle schematic diagram, it includes
Main sound box 9.1, main sound box arc movement device 9.2, lower magnet fixing member 9.3, keynote lower box part electromagnet 9.4, on main sound box
Portion's electromagnet 9.5, upper magnet fixing member 9.6, upper magnet lift telescopic axis 9.7, upper magnet wave hydraulic flexural pivot 9.8 and hawser
Moving member 9.9；Main sound box 9.1 have it is multiple and can there are many type subwoofer, bass, middle pitch, high pitch, ultrahigh frequency, power it is big,
Volume is big, quality weight, and bottom and top are embedded with stainless steel plate, and the electromagnet after being energized is adsorbed；Main sound box arc
Telecontrol equipment 9.2 can be made of 360 degree of round sliding rails and a series of built-in drivings along the sliding block that sliding rail moves freely, main sound box arc
The sliding rail of shape telecontrol equipment 9.2 is bolted on flying platform 3, and sliding block is fixed with lower 9.3 bolt of magnet fixing member,
Lower magnet fixing member 9.3 is fixed with 9.4 bolt of keynote lower box part electromagnet again；The built-in driving of hawser moving member 9.9, can be along hawser
7.5 move freely, upper magnet wave hydraulic flexural pivot 9.8 fixing end and movable end respectively with hawser moving member 9.9 and upper magnet
The fixing end of lift telescopic axis 9.7 is welded and fixed, and the other end and upper magnet fixing member 9.6 of upper magnet lift telescopic axis 9.7 weld
Fixation is connect, upper magnet fixing member 9.6 is fixed with 9.5 bolt of keynote upper box part electromagnet again；Before acoustics setting, according to demand
The main sound box 9.1 of suitable quantity suitable type is chosen, they being placed on keynote lower box part electromagnet 9.4 one by one and being powered makes
The two absorption is fixed；When acoustics is arranged, main sound box 9.1 is driven successively to move them in main sound box arc movement device 9.2
It moves main sound box 9.1 and transports starting point, then movable end positioning unmanned plane 8.2 drives the movable end of hawser 7.5 to reach current keynote
Ring 9.1 installation site and by manually fixing, next upper magnet lift telescopic axis 9.7, upper magnet wave hydraulic flexural pivot 9.8 with
And 9.9 collective effect of hawser moving member is bonded keynote upper box part electromagnet 9.5 with the top of main sound box 9.1, subsequently keynote
Lower box part electromagnet 9.4 powers off, and the energization of keynote upper box part electromagnet 9.5 makes it adsorb fixation with main sound box 9.1, finally upper magnet
Lift telescopic axis 9.7 drives main sound box 9.1 to be detached from keynote lower box part electromagnet 9.4, and hawser moving member 9.9 drives main sound box 9.1
Installation site is moved to be configured；It so repeats, until the position setting of all main sound boxs 9.1 is completed, in conjunction with by activity
End positioning unmanned plane 8.2 carries the secondary sound equipment 8.6 that can adjust position in real time, realizes stage integrally acoustic setting.
Please refer to Figure 18, be key lights assembly principle schematic diagram provided in an embodiment of the present invention, it include king light tool 10.1,
King light tool waves hydraulic flexural pivot 10.2 and king light tool arc movement device 10.3；King light tool 10.1 have multiple and type it is various,
Power is big, volume is big, quality weight, and king light tool arc movement device 10.3 has 360 degree of circle sliding rails and built-in driving can be along sliding rail
The sliding rail of the sliding block composition moved freely, king light tool arc movement device 10.3 is bolted on flying platform 3, king light
Tool waves the fixing end of hydraulic flexural pivot 10.2 and movable end has with the sliding block of king light tool arc movement device 10.3 and king light respectively
10.1 are welded and fixed；King light has freely movement of 10.3 sliding block of arc movement device with respect to its sliding rail, waves liquid in conjunction with king light tool
Pressure ball cuts with scissors the rotary motion that 10.2 movable ends bypass any axis of its center point with respect to its fixing end, and collective effect realizes king light tool
The adaptive pose of 10.1 relative flight platforms 3 adjusts, the real-time pose of movement and secondary lamps and lanterns 8.4 in conjunction with flying platform 3
The setting of stage entirety lighting effects is realized in adjustment.
Figure 19 is please referred to, is main sound box shipping situation schematic diagram 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 (8)
1. a kind of unmanned plane formula light of stage audio device, which is characterized in that it includes sighting device (1), rotor tilting component
(2), flying platform (3), more rotor angles adjustment component (4), rotor assemblies (5), rotor pose adjustment component (6), hawser are received
Component (7), hawser movable end positioning component (8), keynote is put to ring selection and transport component (9) and king light optical assembly (10)；Institute
The rotor assemblies (5) stated include propeller (5.1), propeller swivel bearing (5.2), propeller carrier (5.3) and spiral
Paddle rotating electric machine (5.4)；The Internal and external cycle of propeller swivel bearing (5.2) respectively with propeller (5.1) and propeller carrier
(5.3) bolt is fixed, and the body of propeller rotating electric machine (5.4) is bolted on propeller carrier (5.3), defeated
Shaft and propeller (5.1) are keyed, and pass through baffle and bolt axially position；Propeller rotating electric machine (5.4) output shaft phase
For its body around the rotary motion of its axis, drives propeller (5.1) to rotate relative to propeller carrier (5.3), pass through
The reaction force of air forms the power perpendicular to rotor assemblies (5) plane, is unmanned plane formula light of stage audio device
It is mobile that precondition is provided.
2. a kind of unmanned plane formula light of stage audio device according to claim 1, which is characterized in that the rotor position
Appearance adjustment component (6) includes rotor movement typed ball bearing pair (6.1), rotor movement telescopic shaft (6.2), the hydraulic flexural pivot of rotor movement
(6.3) and rotor pose adjusting seat (6.4)；Rotor movement typed ball bearing pair (6.1) has three groups, the welding of 120 degree of fixing end interval
On propeller carrier (5.3)；Rotor, which moves hydraulic flexural pivot (6.3), three groups, and 120 degree of fixing end interval is welded on rotor
In pose adjusting seat (6.4)；Rotor movement telescopic shaft (6.2) has three groups, and both ends are living with rotor movement typed ball bearing pair (6.1) respectively
Moved end and rotor move hydraulic flexural pivot (6.3) movable end and weld together, to constitute parallel pose adjustment device, rotor fortune
Hydrodynamic pressure flexural pivot (6.3) movable end is secured relative to it the rotary motion that end bypasses any axis of its center point, transports in conjunction with rotor
Relative to the other end, along the linear movement of its axis, it is opposite that propeller carrier (5.3) is adjusted flexibly in dynamic telescopic shaft (6.2) one end
In the pose of rotor pose adjusting seat (6.4), so as to adjust the direction of the born air reaction force of rotor assemblies (5), then lead to
The revolving speed for crossing propeller rotating electric machine (5.4) carrys out the size of corrective action power, so that unmanned plane formula light of stage sound be adjusted flexibly
The whole stress of device is rung, realizes movement and hovering under many attitude, barrier is passed rapidly through and reaches designated position；This
Outside, the upper circular arc of rotor pose adjusting seat (6.4) is small compared with the radius of lower circular arc, and air-flow flows through the speed of upper surface faster, root
According to bernoulli effect, air pressure suffered by lower surface is bigger compared with upper surface, so that generating one lifts power, motor can be separated more
More power makes the movement speed of unmanned plane formula light of stage audio device faster for promoting.
3. a kind of unmanned plane formula light of stage audio device according to claim 1, which is characterized in that the rotor is bowed
Facing upward component (2) 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) is welded and fixed with rotor pose adjusting seat (6.4), rotor pitch bearing (2.2) it is interior
Outer ring is fixed with rotor pitch arm (2.1) and rotor pitching pedestal (2.4) bolt respectively, the body of rotor pitching motor (2.3)
It is bolted on rotor pitching pedestal (2.4), output shaft and rotor pitch arm (2.1) are keyed；Rotor pitching electricity
Machine (2.3) output shaft, around the rotary motion of its axis, drives the adjustment of rotor pose by rotor pitch arm (2.1) with respect to its body
Seat (6.4) is rotated around the axis of rotor pitching motor (2.3), to realize each rotor phase of unmanned plane formula light of stage audio device
Adaptive pitching to flying platform (3), on the one hand improve unmanned plane formula light of stage audio device during the motion from
It is on the other hand flexible when unmanned plane formula light of stage audio device executes the setting task of light and sound equipment by degree and flexibility
The relative angle for adjusting each rotor Yu flying platform (3) avoids generating interference to task execution process.
4. a kind of unmanned plane formula light of stage audio device according to claim 1, which is characterized in that more rotors
It includes rotor arcuate movement sliding rail (4.1) and rotor arcuate movement sliding block (4.2) that angle, which adjusts component (4),；Rotor arcuate movement
Sliding rail (4.1) is 360 degree of round sliding rails, rotor arcuate movement sliding block (4.2) one groups four, can be in rotor arcuate movement sliding rail
(4.1) it is slided freely on；Rotor arcuate movement sliding rail (4.1) welds together with flying platform (3), rotor arcuate movement sliding block
(4.2) it is fixed with rotor pitching pedestal (2.4) bolt；Rotor arcuate movement sliding block (4.2) is along rotor arcuate movement sliding rail (4.1)
Movement freely, drive corresponding rotor to move freely along rotor arcuate movement sliding rail (4.1) by rotor pitching pedestal (2.4),
Realize that the angle adjustment between adjacent rotor adjusts unmanned plane formula light of stage sound equipment when one to two rotors break down
The relative position of each rotor of device, is worked on the moving equilibrium for reaching new.
5. a kind of unmanned plane formula light of stage audio device according to claim 1, which is characterized in that the hawser is received
Putting component (7) has two sets and symmetrically placed；It includes reel (7.1), reel swivel bearing (7.2), reel electric rotating base
(7.3), reel rotating electric machine (7.4), hawser (7.5), pulley (7.6) and cable guide (7.7)；Reel electric rotating base
(7.3) fixed with flying platform (3) bolt, the Internal and external cycle of reel swivel bearing (7.2) respectively with reel electric rotating base (7.3)
It is fixed with reel (7.1) bolt, the body of reel rotating electric machine (7.4) is bolted on reel electric rotating base (7.3)
On, output shaft and reel (7.1) are keyed；The pulley base and cable guide (7.7) of pulley (7.6) are bolted
On flying platform (3), hawser (7.5) one end is fixed on reel (7.1), and other end winding reel (7.1) is after a few, then successively
Hawser movable end positioning component (8) is fixed on after the pulley body of pilot hole and pulley (7.6) by cable guide (7.7)
On；Reel rotating electric machine (7.4) output shaft is with respect to its body around the rotary motion of its axis, and band movable reel (7.1) is around its axis
Rotation realizes the adaptive folding and unfolding of hawser (7.5), hawser (7.5) is rolled withdrawal when not in use, avoids interference unmanned plane formula dance
The movement of desk lamp light audio device releases hawser (7.5) when use, rings choosing in conjunction with hawser movable end positioning component (8), keynote
Light of stage and acoustic setting are realized in the movement for taking and transporting component (9) and king light optical assembly (10).
6. a kind of unmanned plane formula light of stage audio device according to claim 1, which is characterized in that the hawser is living
Moved end positioning component (8) includes hawser movable end fixing piece (8.1), movable end positions unmanned plane (8.2), positioning unmanned plane is fixed
Seat (8.3), secondary lamps and lanterns (8.4), secondary lamps and lanterns wave hydraulic flexural pivot (8.5) and secondary sound equipment (8.6)；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 unmanned plane (8.2) bolt, fixed
Position unmanned plane fixing seat (8.3) is bolted on flying platform (3)；Secondary sound equipment (8.6) and secondary lamps and lanterns (8.4) power
Small, small in size, light weight, secondary sound equipment (8.6) are bolted in movable end positioning unmanned plane (8.2), secondary lamps and lanterns (8.4)
The movable end for waving hydraulic flexural pivot (8.5) with secondary lamps and lanterns is welded and fixed, and the fixing end that secondary lamps and lanterns wave hydraulic flexural pivot (8.5) is welded again
It connects on flying platform (3), secondary lamps and lanterns wave hydraulic flexural pivot (8.5) movable end with respect to its fixing end around any axis of its center point
The rotary motion of line drives the adaptive pose adjustment for realizing secondary lamps and lanterns (8.4) with respect to movable end positioning unmanned plane (8.2)；Work
When making, under the premise of hawser folding and unfolding component (7) releases hawser (7.5), one side movable end positions unmanned plane (8.2) and drives cable
The movable end of rope (7.5) reaches the installation site of main sound box and by manually fixing, and rings in conjunction with keynote and chooses and transport component (9)
Work realize main sound box effect setting, on the other hand, main sound box configuration after the completion of, secondary sound equipment (8.6) and pair lamps and lanterns (8.4)
Under the drive of movable end positioning unmanned plane (8.2), cooperation keynote, which is rung, chooses and transports component (9) and king light optical assembly (10)
Stage entirety light and acoustic setting are realized in work；When not working, movable end positions unmanned plane (8.2) and passes through positioning nothing
Man-machine fixing seat (8.3) is realized fixes with the position of flying platform (3), prevents it from sending out in the motion process of flying platform (3)
Life is fallen.
7. a kind of unmanned plane formula light of stage audio device according to claim 1, which is characterized in that the keynote is rung
Choosing and transport component (9) includes main sound box (9.1), main sound box arc movement device (9.2), lower magnet fixing member (9.3), master
Speaker lower part electromagnet (9.4), keynote upper box part electromagnet (9.5), upper magnet fixing member (9.6), upper magnet lift telescopic axis
(9.7), upper magnet waves hydraulic flexural pivot (9.8) and hawser moving member (9.9)；Main sound box (9.1) has multiple and can have more
Seed type (subwoofer, bass, middle pitch, high pitch, ultrahigh frequency), power is big, volume is big, quality weight, and bottom and top are embedded with
Stainless steel plate, the electromagnet after being energized are adsorbed；Main sound box arc movement device (9.2) is by 360 degree of round sliding rails and one
Serial built-in driving can pass through bolt along the sliding block composition that sliding rail moves freely, the sliding rail of main sound box arc movement device (9.2)
Be fixed on flying platform (3), sliding block is fixed with lower magnet fixing member (9.3) bolt, lower magnet fixing member (9.3) again with master
Speaker lower part electromagnet (9.4) bolt is fixed；The built-in driving of hawser moving member (9.9), can move freely along hawser (7.5), on
Magnet wave hydraulic flexural pivot (9.8) fixing end and movable end respectively with hawser moving member (9.9) and upper magnet lift telescopic axis
(9.7) fixing end is welded and fixed, and the other end of upper magnet lift telescopic axis (9.7) and upper magnet fixing member (9.6) welding are solid
Fixed, upper magnet fixing member (9.6) is fixed with keynote upper box part electromagnet (9.5) bolt again；Before acoustics setting, according to demand
The main sound box (9.1) for choosing suitable quantity suitable type, they is placed on keynote lower box part electromagnet (9.4) one by one and is led to
Electricity fixes the two absorption；Acoustics be arranged when, main sound box arc movement device (9.2) drive main sound box (9.1) by it
Be successively moved to main sound box (9.1) transport starting point, then movable end positioning unmanned plane (8.2) drive hawser (7.5) activity
End reaches the installation site of current keynote sound (9.1) and by manually fixing, next upper magnet lift telescopic axis (9.7), upper magnetic
Iron, which waves hydraulic flexural pivot (9.8) and hawser moving member (9.9) collective effect, makes keynote upper box part electromagnet (9.5) and main sound box
(9.1) top fitting, subsequently keynote lower box part electromagnet (9.4) powers off, and keynote upper box part electromagnet (9.5) energization makes it
It adsorbs and fixes with main sound box (9.1), finally upper magnet lift telescopic axis (9.7) drives main sound box (9.1) to be detached from keynote lower box part
Electromagnet (9.4), hawser moving member (9.9) drive main sound box (9.1) to be moved to installation site and are configured；It so repeats, directly
It is arranged to the position for completing all main sound boxs (9.1), position can be adjusted in real time in conjunction with being carried by movable end positioning unmanned plane (8.2)
The secondary sound equipment (8.6) set realizes stage integrally acoustic setting.
8. a kind of unmanned plane formula light of stage audio device according to claim 1, which is characterized in that the key lights
Component (10) includes king light tool (10.1), king light tool waves hydraulic flexural pivot (10.2) and king light has arc movement device
(10.3)；King light tool (10.1) has that multiple and type is various, power is big, volume is big, quality weight, king light tool arc movement device
(10.3) it can be made of along the sliding block that sliding rail moves freely 360 degree of circle sliding rails and built-in driving, king light has arc movement device
(10.3) sliding rail is bolted on flying platform (3), and king light has the fixing end and work for waving hydraulic flexural pivot (10.2)
Moved end is welded and fixed with the sliding block of king light tool arc movement device (10.3) and king light tool (10.1) respectively；King light has arcuate movement
It is solid with respect to it to wave hydraulic flexural pivot (10.2) movable end in conjunction with king light tool with respect to the movement freely of its sliding rail for device (10.3) sliding block
Fixed end bypasses the rotary motion of any axis of its center point, and collective effect realizes king light tool (10.1) relative flight platform (3)
The real-time pose of adaptive pose adjustment, movement and secondary lamps and lanterns (8.4) in conjunction with flying platform (3) adjusts, and realizes that stage is whole
The setting of body lighting effects.
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| CN201811163615.0A CN109334964A (en) | 2018-10-01 | 2018-10-01 | A kind of unmanned plane formula light of stage audio device |
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| CN201811163615.0A CN109334964A (en) | 2018-10-01 | 2018-10-01 | A kind of unmanned plane formula light of stage audio device |
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Application publication date: 20190215 |