CN207417140U - The overhead suspensions of more rotation centered cubics arrangements float device - Google Patents
The overhead suspensions of more rotation centered cubics arrangements float device Download PDFInfo
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- CN207417140U CN207417140U CN201721458711.9U CN201721458711U CN207417140U CN 207417140 U CN207417140 U CN 207417140U CN 201721458711 U CN201721458711 U CN 201721458711U CN 207417140 U CN207417140 U CN 207417140U
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- floats
- telescopic rod
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- rotation centered
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- 239000000725 suspension Substances 0.000 title claims abstract description 32
- 230000001681 protective effect Effects 0.000 claims abstract description 18
- 239000004677 Nylon Substances 0.000 claims abstract description 5
- 229920001778 nylon Polymers 0.000 claims abstract description 5
- 238000013016 damping Methods 0.000 claims description 17
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 9
- 230000009187 flying Effects 0.000 claims description 6
- 229910001220 stainless steel Inorganic materials 0.000 claims description 5
- 239000010935 stainless steel Substances 0.000 claims description 5
- 230000001360 synchronised effect Effects 0.000 claims description 5
- 239000004033 plastic Substances 0.000 claims description 4
- 238000003466 welding Methods 0.000 claims description 3
- 230000000630 rising effect Effects 0.000 claims 1
- 238000005516 engineering process Methods 0.000 description 9
- 238000010586 diagram Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 3
- RKTYLMNFRDHKIL-UHFFFAOYSA-N copper;5,10,15,20-tetraphenylporphyrin-22,24-diide Chemical compound [Cu+2].C1=CC(C(=C2C=CC([N-]2)=C(C=2C=CC=CC=2)C=2C=CC(N=2)=C(C=2C=CC=CC=2)C2=CC=C3[N-]2)C=2C=CC=CC=2)=NC1=C3C1=CC=CC=C1 RKTYLMNFRDHKIL-UHFFFAOYSA-N 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 1
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- Vibration Dampers (AREA)
Abstract
The overhead suspensions that the utility model provides more rotation centered cubics arrangements float device, and including adjustable link device, cabinet, protective cover, connection sheet and the outstanding device that floats, the outstanding device that floats is mounted on the corner location of cabinet by adjustable link device bolt respectively；Protective cover covers on the outside of the outstanding device that floats by connection sheet respectively.The overhead suspension that the utility model revolves centered cubic arrangement more floats device, can improve the skyborne stability of aerial utensil, can adjust the problem of aircraft size shape, firmly nonsynchronous problem may be employed when multiple aerial boat products that float carry an article；Casing, the first telescopic rod, the setting of the second telescopic rod and adjusting bolt, the spacing between adjustable each outstanding device that floats ensure that the overhead suspensions of more rotation centered cubics arrangements float the having a smooth flight property and collimation of device；Movable pulley is specifically using the nylon universal wheel with brake；Movable pulley is provided with multiple, and the overhead suspensions for being moved easily more rotation centered cubics arrangements float device, so that more convenient using operating.
Description
Technical field
The overhead suspension that the utility model belongs to float boat technical field more particularly to more rotation centered cubic arrangement floats device.
Background technology
Float boat, be it is a kind of can suspension in low latitude and in room, movement, the daily necessities of operation, instrument, toy,
The general name of the aerial article of one major class such as equipment, instrument, flying robot, according to function, feature, purposes, navigation of floaing includes in the industry
Have eliminate sound it is quiet float, the room in room floats, it is extreme low-altitude in near-earth float, the light of night operation floats, rapid flight fly
Float, can manned people is floatd, intelligent program is high intelligence float, can enter in water and the skyborne water that can float floats, is deep into cave well
The hole at bottom floats, be not afraid of baked wheaten cake and the fire of high temperature floats, micro- in small space is floatd etc..Navigation industry of floaing has been started people are daily
People and object in life bring up to a kind of aerial new technology path, and navigation industry of floaing has three with navigation, the difference of civil aviaton, space flight industry
Point：The difference of first mesh, for the purpose of " traveling ", " hanging " is means for navigation, civil aviaton, space flight industry, and navigation industry of floaing is with " outstanding
It is empty " for the purpose of, " movement " is means；The field of second application is different, and navigation, civil aviaton, space flight industry substitutes and of development
It is horizontal and vertical carrier, so application range is extremely narrow；Boat of floaing technology almost can be applied to all industries, several
Can substitute and develop all industries, the field set foot in is extremely extensive, when an article by its " suspension " in the air when, can produce
Raw many unexpected marvellous effects；3rd culture is different, and navigation, civil aviaton, space technology are entirely to be instructed with Western Culture
The technology of lower generation, inflexible, mechanical, inhumanity, boat of floaing technology are the technologies to be generated under the culture guidance of Chinese root, taking human as
This, has peace and quiet, safety, daily life, the characteristic of hommization.
In the prior art, multi-rotor aerocraft simply separates four axis, six axis, eight axis, 12 axis, 16 on a point
Axis, and every group of rotary wings are on one face, and when making large-scale aerial daily necessities, rotary wing is separated from a point, limited
Only on one face, power can be caused unbalanced, aircraft flies unstable in the air.For example flight bed, meet take bride fly
Row bridal sedan chair, large-scale flight billboard etc., multi-rotor aerocraft is designed from the angle of flight, is not appropriate for the outstanding work(that floats
The product of navigation industry of floaing based on energy.
In existing vehicle technology, with large item fly up into the sky sky when, can be led using multiple multi-rotor aerocrafts
Large item so because often each multi-rotor aerocraft spacing is not fixed, firmly asynchronous, and brings problems, and
The design of technology and winged control to operator causes very big difficulty, for example, in the entirety of an aerial utensil, Duo Gesheng
Force is with planar alignment, without multiple lift points compared with center with symmetrical three-dimensional stable array.Itself is skyborne not
Stablize, cause multiple airborne aircrafts when one large and heavy objects of carrying float towards aerial, it is firmly unbalanced, and this cannot be used
Kind method.
Therefore, for insufficient existing for above-mentioned multi-rotor aerocraft, the overhead suspensions for inventing more rotation centered cubics arrangements float device
Tool is very necessary.
Utility model content
In order to solve the above-mentioned technical problem, the utility model provides the overhead suspensions of more rotation centered cubics arrangements and floats device, with solution
Certainly existing aerial utensil there is fly it is unstable, can not adjust the problem of aircraft size shape, multiple aircraft carry
Firmly nonsynchronous problem during one article.
In order to achieve the above object, the technical solution adopted in the utility model
The overhead suspensions of more rotation centered cubics arrangements float device, including adjustable link device, cabinet, protective cover, connection sheet and
The outstanding device that floats, the outstanding device that floats are mounted on the corner location of cabinet by adjustable link device bolt respectively；The protection
Cover covers on the outside of the outstanding device that floats by connection sheet respectively；The adjustable link device include casing, the first telescopic rod, second
Telescopic rod, adjusting bolt, landing gear and Rapid connecting bolt, one end of the casing is socketed the first telescopic rod, another
End cap connects the second telescopic rod；The adjusting bolt is threaded in junction and the casing of casing and the first telescopic rod respectively
With the junction of the second telescopic rod；The landing gear is mounted on by Rapid connecting bolt in the top of the first telescopic rod
Between position.
The work paddle of each more supercentral same positions of rotation is controlled by the single line flown in control, is kept in same position
The paddle that works is synchronous equidirectional with power, and revolves center arrangement mode more, front and rear up and down symmetrical.So each more rotor flyings
Device spacing fixes, is firmly synchronous, firmly symmetrical, does not increase the design difficulty for flying control, does not also increase the operation difficulty of manipulator.
Preferably, the outstanding device that floats is made of the outstanding device fuselage that floats, wing propeller and machine bar, the wing propeller
The corner location of the outstanding device fuselage that floats is mounted on by machine bar respectively.
Preferably, the connection sheet is separately positioned on the upper middle position of machine bar.
Preferably, the landing gear includes crossbeam, fixing pipe, adjusting rod, movable pulley, damping spring and fastening spiral shell
Bolt, the fixing pipe are respectively welded at left and right sides of the lower part of crossbeam；The adjusting rod is plugged on through damping spring one end
The lower inside of fixing pipe, other end welding movable pulley；The fastening bolt is threaded in the company of fixing pipe and adjusting rod
Meet place.
Preferably, the cabinet includes pedestal, connecting rod and mounting groove, and the top left and right sides of the pedestal is respectively
The lower part of pedestal is welded on by connecting rod；The upper middle position of the cabinet opens up mounting groove respectively.
Preferably, the protective cover is specifically using circular PVC plastic protective cover；There are four the protective cover is set.
Preferably, the movable pulley is specifically using the nylon universal wheel with brake；The movable pulley is provided with more
It is a.
Preferably, the damping spring specifically uses cylindrical spring；The damping spring is provided with multiple.
Preferably, the inside centre position of the crossbeam opens up mounting hole.
Preferably, the outstanding implement body that floats is using four.
Preferably, first telescopic rod and the second telescopic rod are using the identical stainless steel of diameter；Described
The length of two telescopic rods is twice of the length of the first telescopic rod.
Preferably, the diameter of first telescopic rod is two millimeters to three millimeters smaller than the diameter of casing；The casing
Length is used as 20 centimetres to 25 centimetres of stainless steel sleeve pipe.
The utility model has the advantages that：The overhead suspension that the utility model revolves centered cubic arrangement more floats device, can
To improve the skyborne stability of aerial utensil, the problem of aircraft size shape can be adjusted, may be employed and multiple float in the air
Firmly nonsynchronous problem when the product that navigates carries an article, meanwhile, the utility model also has following advantageous effect：
1. in the utility model, the outstanding implement body that floats is conducive to improve more rotation centered cubic arrangements using four
Overhead suspension float the having a smooth flight property of device, ensure that overhead suspensions of more rotation centered cubics arrangements float the flight safety of device.
2. in the utility model, the casing, the first telescopic rod, the setting of the second telescopic rod and adjusting bolt, favorably
Spacing between each outstanding device that floats is adjusted, ensure more rotation centered cubics arrangements overhead suspensions float device having a smooth flight property with it is parallel
Property.
3. in the utility model, the movable pulley is specifically using the nylon universal wheel with brake；The movable pulley
It is provided with multiple, the overhead suspensions for being conducive to be moved easily more rotation centered cubics arrangements float device, so that more convenient using operating.
4. in the utility model, the damping spring specifically uses cylindrical spring；The damping spring be provided with it is multiple,
Be conducive to when the overhead suspensions for revolving centered cubics arrangement float device whereabouts more, casing, the first telescopic rod, the second telescopic rod and adjusting
When unpredictable failure occurring between bolt, damping, buffering is played the role of by damping spring, ensures user or delivery
The security of article is allowed to land safely.
5. in the utility model, the protective cover is specifically using circular PVC plastic protective cover；The protection is provide with
There are four putting, be conducive to prevent the wing propeller of the outstanding device that floats from injuring operator during high-speed rotating, and then ensure to make
The personal safety of user.
6. in the utility model, the fixing pipe, the setting of adjusting rod and fastening bolt is conducive to adjust more rotations
The spacing that the overhead suspension of centered cubic arrangement floats between device and ground ensures that more rotation centered cubic arrangements can be used normally
Overhead suspension floats device.
Description of the drawings
Fig. 1 is the structure diagram of the utility model.
Fig. 2 is the structure diagram of the adjustable link device of the utility model.
Fig. 3 is the structure diagram of the landing gear of the utility model.
Fig. 4 is the structure diagram of the cabinet of the utility model.
Fig. 5 is the schematic diagram of one three-dimensional example of the utility model.
In figure：
1st, the device fuselage that floats is hanged；2nd, adjustable link device；21st, casing；22nd, the first telescopic rod；23rd, the second telescopic rod；24、
Adjusting bolt；25th, landing gear；251st, crossbeam；2511st, mounting hole；252nd, fixing pipe；253rd, adjusting rod；254th, movable pulley；
255th, damping spring；256th, fastening bolt；26th, Rapid connecting bolt；3rd, cabinet；31st, pedestal；32nd, connecting rod；33rd, mounting groove；4、
Wing propeller；5th, machine bar；6th, protective cover；7th, connection sheet；8th, the device that floats is hanged.
Specific embodiment
The utility model is described further below in conjunction with attached drawing：
Embodiment：
As shown in attached drawing 1 to attached drawing 4
The overhead suspensions that the utility model provides more rotation centered cubics arrangements float device, including adjustable link device 2, cabinet 3,
Protective cover 6, connection sheet 7 and the outstanding device 8 that floats, the outstanding device 8 that floats are mounted on cabinet 3 by 2 bolt of adjustable link device respectively
Corner location；The protective cover 6 covers on the outside of the outstanding device 8 that floats by connection sheet 7 respectively；The adjustable link device
2 include casing 21, the first telescopic rod 22, the second telescopic rod 23, adjusting bolt 24, landing gear 25 and Rapid connecting bolt
26, one end of the casing 21 is socketed the first telescopic rod 22, and the other end is socketed the second telescopic rod 23；The adjusting bolt 24
The junction of 21 and second telescopic rod 23 of junction and casing of 21 and first telescopic rod 22 of casing is threaded in respectively；Institute
The landing gear 25 stated is mounted on the upper middle position of the first telescopic rod 22 by Rapid connecting bolt 26.
In above-described embodiment, the work paddle of each more supercentral same positions of rotation is controlled by the single line flown in control, is protected
The work paddle held in same position is synchronous equidirectional with power, and revolves center arrangement mode more, front and rear up and down symmetrical.So
Each multi-rotor aerocraft spacing fixes, is firmly synchronous, firmly symmetrical, does not increase the design difficulty for flying control, does not also increase manipulation
The operation difficulty of person.
In above-described embodiment, specifically, the outstanding device 8 that floats is by the outstanding device fuselage 1 that floats, 5 structure of wing propeller 4 and machine bar
Into the wing propeller 4 is mounted on the corner location of the outstanding device fuselage 1 that floats by machine bar 5 respectively.
In above-described embodiment, specifically, the connection sheet 7 is separately positioned on the upper middle position of machine bar 5.
In above-described embodiment, specifically, the landing gear 25 includes crossbeam 251, fixing pipe 252, adjusting rod
253, movable pulley 254, damping spring 255 and fastening bolt 256, the lower part that the fixing pipe 252 is respectively welded at crossbeam 251 are left
Right both sides；The adjusting rod 253 is plugged on the lower inside of fixing pipe 252 through 255 one end of damping spring, and other end welding moves
Driving wheel 254；The fastening bolt 256 is threaded in the junction of fixing pipe 252 and adjusting rod 253.
In above-described embodiment, specifically, the cabinet 3 includes pedestal 31, connecting rod 32 and mounting groove 33, the bottom
It is welded on the lower part of pedestal 31 at left and right sides of the top of seat 31 by connecting rod 32 respectively；The top interposition of the cabinet 3
It puts and opens up mounting groove 33 respectively.
In above-described embodiment, specifically, the protective cover 6 is specifically using circular PVC plastic protective cover；The protection
There are four cover 6 is set.
In above-described embodiment, specifically, the movable pulley 254 is specifically using the nylon universal wheel with brake；It is described
Movable pulley 254 be provided with it is multiple.
In above-described embodiment, specifically, the damping spring 255 specifically uses cylindrical spring；The damping spring 255 is set
It is equipped with multiple.
In above-described embodiment, specifically, the inside centre position of the crossbeam 251 opens up mounting hole 2511.
In above-described embodiment, specifically, the outstanding device 8 that floats is specifically using four.
In above-described embodiment, specifically, first telescopic rod 22 and the second telescopic rod 23 are identical using diameter
Stainless steel；The length of second telescopic rod 23 is twice of the length of the first telescopic rod 22.
In above-described embodiment, specifically, two millimeters smaller than the diameter of casing 21 of the diameter of first telescopic rod 22 is extremely
Three millimeters；The casing 21 uses length as 20 centimetres to 25 centimetres of stainless steel sleeve pipe.Fig. 5 is in being revolved eight more
The schematic diagram of the tetragonal prism multi-rotor aerocraft of the heart, each angle of tetragonal prism are more rotation centers, are mounted on each more rotation centers
One outstanding device that floats, the propeller in the same positions of eight outstanding devices that float, by flying the identical signal line traffic control in control.
Operation principle
It in the utility model, is fixedly connected by using multiple outstanding devices 8 that float, one flies control and this multiple hangs is controlled to float simultaneously
Device 8, the wing propeller 4 of same location are controlled with the same root line in control is flown, and keep the different outstanding identical bits floatd on device 8
4 rotating speed of wing propeller put is consistent.
Using technical solution described in the utility model or those skilled in the art in technical solutions of the utility model
Under inspiration, similar technical solution is designed, and reaches above-mentioned technique effect, is the protection model for falling into the utility model
It encloses.
Claims (10)
1. the overhead suspension that centered cubic arrangement is revolved floats device more, which is characterized in that overhead suspensions of more rotation centered cubics arrangements float device
Including adjustable link device（2）, cabinet（3）, protective cover（6）, connection sheet（7）With the outstanding device that floats（8）, the outstanding device that floats（8）
Pass through adjustable link device respectively（2）Bolt is mounted on cabinet（3）Corner location；The protective cover（6）Pass through respectively
Connection sheet（7）Cover on the outstanding device that floats（8）Outside；The adjustable link device（2）Including casing（21）, the first telescopic rod
（22）, the second telescopic rod（23）, adjusting bolt（24）, landing gear（25）And Rapid connecting bolt（26）, the casing
（21）One end be socketed the first telescopic rod（22）, the other end the second telescopic rod of socket（23）；The adjusting bolt（24）Respectively
It is threaded in casing（21）With the first telescopic rod（22）Junction and casing（21）With the second telescopic rod（23）Connection
Place；The landing gear（25）Pass through Rapid connecting bolt（26）Mounted on the first telescopic rod（22）Top interposition
It puts.
The device 2. overhead suspension of more rotation centered cubic arrangements as described in claim 1 floats, which is characterized in that the outstanding device that floats
（8）By the outstanding device fuselage that floats（1）, wing propeller（4）With machine bar（5）It forms, the wing propeller（4）Pass through machine bar respectively
（5）Mounted on the outstanding device fuselage that floats（1）Corner location.
The device 3. overhead suspension of more rotation centered cubic arrangements as described in claim 1 floats, which is characterized in that described rising and falling is rack-mounted
It puts（25）Including crossbeam（251）, fixing pipe（252）, adjusting rod（253）, movable pulley（254）, damping spring（255）And fastening bolt
（256）, the fixing pipe（252）It is respectively welded at crossbeam（251）Lower part at left and right sides of；The adjusting rod（253）It passes through
Wear damping spring（255）One end is plugged on fixing pipe（252）Lower inside, the other end welding movable pulley（254）；The fastening
Bolt（256）It is threaded in fixing pipe（252）And adjusting rod（253）Junction.
The device 4. overhead suspension of more rotation centered cubic arrangements as described in claim 1 floats, which is characterized in that the cabinet（3）
Including pedestal（31）, connecting rod（32）And mounting groove（33）, the pedestal（31）Top at left and right sides of pass through connection respectively
Bar（32）It is welded on pedestal（31）Lower part；The cabinet（3）Upper middle position open up mounting groove respectively（33）.
The device 5. overhead suspension of more rotation centered cubic arrangements as described in claim 1 floats, which is characterized in that the protective cover
（6）It is specific to use circular PVC plastic protective cover；The protective cover（6）There are four settings.
The device 6. overhead suspension of more rotation centered cubic arrangements as claimed in claim 3 floats, which is characterized in that the movable pulley
（254）It is specific to use the nylon universal wheel with brake；The movable pulley（254）It is provided with multiple.
The device 7. overhead suspension of more rotation centered cubic arrangements as claimed in claim 3 floats, which is characterized in that the damping spring
（255）Specifically use cylindrical spring；The damping spring（255）It is provided with multiple.
The device 8. overhead suspension of more rotation centered cubic arrangements as claimed in claim 3 floats, which is characterized in that the crossbeam
（251）Inside centre position open up mounting hole（2511）.
The device 9. overhead suspension of more rotation centered cubic arrangements as described in claim 1 floats, which is characterized in that described first is flexible
Bar（22）With the second telescopic rod（23）Using the identical stainless steel of diameter；Second telescopic rod（23）Length be
One telescopic rod（22）Twice of length.
The device 10. overhead suspension of more rotation centered cubic arrangements as described in claim 1 floats, which is characterized in that each more rotation centers
On same position work paddle by flying the same root line traffic control in control, keep the work paddle in same position synchronous with power Tongfang
To, and revolve center arrangement mode more, it is front and rear up and down symmetrical.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721458711.9U CN207417140U (en) | 2017-11-06 | 2017-11-06 | The overhead suspensions of more rotation centered cubics arrangements float device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721458711.9U CN207417140U (en) | 2017-11-06 | 2017-11-06 | The overhead suspensions of more rotation centered cubics arrangements float device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207417140U true CN207417140U (en) | 2018-05-29 |
Family
ID=62307340
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721458711.9U Active CN207417140U (en) | 2017-11-06 | 2017-11-06 | The overhead suspensions of more rotation centered cubics arrangements float device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207417140U (en) |
-
2017
- 2017-11-06 CN CN201721458711.9U patent/CN207417140U/en active Active
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Effective date of registration: 20240814 Address after: Room 210, 2nd Floor, Building C, No. 199 Xiangjiang Road, Xiannv Town, Jiangdu District, Yangzhou City, Jiangsu Province, China 225000 Patentee after: Yangzhou Juhui Electronic Information Technology Co.,Ltd. Country or region after: China Address before: 450000, No. C017, 4th Floor, Building B, Shihang Window, Airport Cross border E-commerce Demonstration Park, Yingbin Avenue, Zhengzhou Airport District, Zhengzhou City, Henan Province Patentee before: ZHENGZHOU AIR HARBOR PIAOTIANXIA INTERNET OF THINGS TECHNOLOGY CO.,LTD. Country or region before: China |
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