CN209545468U - Crossed Circle rotor spherical tanks aircraft - Google Patents
Crossed Circle rotor spherical tanks aircraft Download PDFInfo
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- CN209545468U CN209545468U CN201920183985.4U CN201920183985U CN209545468U CN 209545468 U CN209545468 U CN 209545468U CN 201920183985 U CN201920183985 U CN 201920183985U CN 209545468 U CN209545468 U CN 209545468U
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- posture adjustment
- protective cover
- spherical tanks
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- 230000001681 protective effect Effects 0.000 claims abstract description 57
- 238000010521 absorption reaction Methods 0.000 claims description 29
- 238000006073 displacement reaction Methods 0.000 claims description 20
- 238000009434 installation Methods 0.000 claims description 11
- 238000007363 ring formation reaction Methods 0.000 claims description 7
- 230000003014 reinforcing effect Effects 0.000 claims description 5
- 238000005096 rolling process Methods 0.000 claims description 5
- 238000005339 levitation Methods 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims 1
- 230000007812 deficiency Effects 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 12
- 238000012423 maintenance Methods 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000005389 magnetism Effects 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000005265 energy consumption Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000005457 optimization Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005284 excitation Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
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Abstract
The utility model discloses a kind of Crossed Circle rotor spherical tanks aircrafts, it is intended to solve that aircraft rotary wing blade is exposed outside, there is the risk that collision fractures, and the deficiency of aircraft posture adjustment inconvenience.The utility model includes spherical tanks, upper protective cover, lower protective cover, rotor fixed ring, upper rotor rotor, lower rotor rotor, control system, rotor fixed ring is connected between protective cover and the inner ring of lower protective cover, posture adjustment ring is rotatablely installed in rotor fixed ring, spherical tanks are rotatably installed in posture adjustment ring, the posture adjustment joint shaft that connection two is oppositely arranged between posture adjustment ring and rotor fixed ring, the cabin joint shaft that connection two is oppositely arranged between spherical tanks and posture adjustment ring, posture adjustment joint shaft and cabin joint shaft axis are vertical, one posture adjustment joint shaft and a cabin joint shaft are sequentially connected posture adjustment motor；Upper rotor rotor, lower rotor rotor may be rotatably mounted in rotor fixed ring, and gyroscope is installed in rotor fixed ring, and posture adjustment motor, gyroscope are electrically connected to the control system.
Description
Technical field
The utility model relates to a kind of aircraft, more specifically, it relates to a kind of Crossed Circle rotor spherical tanks aircraft.
Background technique
As General Aviation is determined as pillar industry by country, people are higher and higher to the attention rate of aircraft.Fixed-wing flies
Machine needs runway, and the exposed safety of the rotor of common helicopter is not high, and is equipped with high-power engine because load torque is big,
Transmission system is complicated and easily parts fatigue is caused to regularly replace, and the maintenance cost of aircraft is high, these all significantly limit logical
With the development of aircraft industry.Currently, Development of UAV is quickly, for shooting or even transporting express delivery, but present many unmanned planes
Rotor blade is exposed outside, there is the risk that collision fractures, and unmanned plane posture adjustment is inconvenient and can not achieve heavy-duty ability.
Utility model content
The utility model overcomes that aircraft rotary wing blade is exposed outside, there is the risk that collision fractures, and aircraft posture adjustment
Inconvenient deficiency, provides a kind of Crossed Circle rotor spherical tanks aircraft, aircraft rotary wing blade is hidden in protective cover, rotation process
In will not collide the phenomenon that fractureing, and rotor blade length is short, advantageously reduces and wants to the harsh of rotor blade intensity
It asks and replaces rotor blade without frequent, posture adjustment is convenient and reliable in aircraft flight；Crossed Circle rotor spherical tanks aircraft is significantly
Drive mechanism is simplified, mitigates aircraft self weight, reduces maintenance intensity and expense, increase power output radius, reduce to hair
The requirement of motivation power, considerably reduces energy consumption, is not necessarily to empennage, structure simple optimization.
In order to solve the above-mentioned technical problem, the utility model uses a kind of following technical scheme: Crossed Circle rotor spherical tanks
Aircraft, including spherical tanks, upper protective cover, lower protective cover, rotor fixed ring, upper rotor rotor, lower rotor rotor, control system,
In a ring, rotor fixed ring is connected to protective cover under for upper protective cover, lower protective cover, upper rotor rotor, lower rotor rotor
Between the inner ring of protective cover, posture adjustment ring is rotatablely installed in rotor fixed ring, spherical tanks are rotatably installed in posture adjustment ring, posture adjustment ring and
The posture adjustment joint shaft that connection two is oppositely arranged between rotor fixed ring connects two machines being oppositely arranged between spherical tanks and posture adjustment ring
Cabin joint shaft, posture adjustment joint shaft and cabin joint shaft axis are vertical, a posture adjustment joint shaft and a cabin joint shaft company of transmission
Connect posture adjustment motor；If upper rotor rotor, lower rotor rotor include sports ring, strong magnet rotor, are uniformly connected on sports ring
Dry rotor blade, installation magnet exciting coil stator corresponding with strong magnet rotor in rotor fixed ring, sports ring may be rotatably mounted at rotor
In fixed ring, gyroscope is installed in rotor fixed ring, posture adjustment motor, magnet exciting coil stator, gyroscope are electrically connected with control system
It connects, upper rotor rotor, lower rotor rotor rotation direction are always on the contrary, rotor blade radial outer end is placed in protective cover and lower protection
Between cover.
Magnet exciting coil stator and strong magnet rotor constitute brshless DC motor, the operation of Crossed Circle rotor spherical tanks aircraft together
When, control system is powered to magnet exciting coil stator, and strong magnet rotor drives sports ring to rotate together.Upper rotor rotor, lower rotor turn
Sub- rotation direction is always on the contrary, the reaction torque that air generates is cancelled out each other, when the revolving speed for changing one of rotor rotor, aircraft
It can turn.Spherical tanks center is lower than lower protective cover close to lower end position, spherical tanks lower end.Pass through a pair of of posture adjustment joint shaft
With the setting of a pair of of cabin joint shaft, make to rotate between spherical tanks and rotor fixed ring with any angle.By control system control
Make two posture adjustment motors operating realize posture adjustment joint shaft and cabin joint shaft rotation, due to spherical tanks center of gravity always vertically to
Under, the rotation of posture adjustment joint shaft and cabin joint shaft makes rotor fixed ring form certain inclination angle relative to spherical tanks, and aircraft is
The thrust that can get a horizontal direction enables aircraft to fly to inclination direction.Dip angle signal that gyroscope will test and
Direction signal is transmitted to control system, control system according to gyroscope transmitting come signal instruction is issued to two posture adjustment motors,
Control the revolving speed and rotational angle of posture adjustment motor.Upper rotor rotor, lower rotor rotor be placed in protective cover and lower protective cover it
Between, the concealed setting of rotor blade, will not collide in rotation process the phenomenon that fractureing.Upper rotor rotor, lower rotor rotor
In a ring, screw blade leaf length is short, advantageously reduces the rigors to propeller blade intensity.This Crossed Circle rotor
Spherical tanks wind stick blade is hidden in protective cover, and will not collide the phenomenon that fractureing in rotation process, and spiral shell
It is short to revolve blade leaf length, advantageously reduces the rigors to propeller blade intensity, posture adjustment conveniently may be used in aircraft flight
It leans on.
Preferably, rotor fixed ring is equipped with the mounting grooves of two annulars, it is equipped with suspended ring on sports ring, in suspended ring
Installation absorption ring on wall is equipped with levitation gap between suspended ring, absorption ring and installation groove sidewall, on suspended ring upper and lower surfaces
It is mounted on movable permanent-magnetic clamp, installs in groove sidewall and movable permanent-magnetic clamp corresponding position is equipped with fixed permanent-magnetic clamp, movable permanent magnetism
Ring is identical as the fixed opposite face magnetic pole of permanent-magnetic clamp；Several electromagnetic blocks are uniformly installed, electromagnetic block is radially orientated in rotor fixed ring
Absorption ring and the attraction absorption ring that can be powered, are mounted on close to electromagnetic block position in rotor fixed ring and are radially orientated absorption ring setting
Displacement sensor；Electromagnetic block, displacement sensor are electrically connected to the control system.
The opposite face homopolar-repulsion of movable permanent-magnetic clamp and fixed permanent-magnetic clamp, makes suspended ring be in suspended state；Adsorb ring and
Gap has been remained between installation groove sidewall, it is ensured that is in suspended state in sports ring rotation process always.Control system pair
The energization of electromagnetic block coil makes electromagnetic block attract absorption ring, and the signal that displacement sensor detects is transported to control system, control system
Whether system is powered according to the signal of the displacement sensor of reading to the coil of electromagnetic block and electrical current size controls.Electricity
Magnetic patch is staggered the time on-off, electromagnetic block of the same period to maximum distance position between the displacement sensor detected and absorption ring inner wall
It is powered, so that the electromagnetic block be made to attract absorption ring, shortens the distance between displacement sensor and absorption ring inner wall.
Control system reads displacement transducer signal and the frequency being powered to single electromagnetic block is set as needed, to make to suspend
Ring is in dynamic balance state always.Sports ring is in suspended state always in upper rotor rotor, lower rotor rotor rotation process,
Vibration and noise is small, does not need to lubricate, no mechanical wear, long service life, and maintenance cost is low.
Preferably, sports ring upper surface is equipped with protective ring, several anticollision shafts are uniformly installed on rotor fixed ring outer wall
Hold, between anticollision bearing outer wall and protective ring inner wall be equipped with anticollision gap, anticollision gap radial spacing be less than absorption ring inner wall with
Radial spacing between groove sidewall is installed.
When electromagnetic block breaks down, radially there is subtle offset in sports ring rotation process, anticollision shaft honours protective ring
Inner wall is supported, and prevents relatively large deviation radially occur in rotor rotor rotation process, when can guarantee that electromagnetic block breaks down
Sports ring can also run well.
Another scheme installs rolling bearing between rotor fixed ring and sports ring.Between rotor fixed ring and sports ring
It is realized and is rotatablely connected using rolling bearing, sports ring smooth running is reliable.
Preferably, the rotor blade outer end on same sports ring connects into an entirety by reinforcing ring.Reinforcing ring
It is provided with the structural strength for being conducive to improve rotor blade.
Preferably, lower protective cover upper surface is equipped with positioning convex ring, upper protective cover lower surface outside close to outer edge position
Edge is equipped with lid cyclization, and positioning convex ring is adapted to plug-in with lid cyclization, and the lower end Gai Hehuan is supported on lower protective cover upper surface.
By the inserting of the adaptation of lid cyclization and positioning convex ring, connection is more steady reliable for upper protective cover and lower protective cover.
Preferably, strong magnet rotor includes rotor ring, permanent magnet magnetic shoe, several link slots are laid on rotor ring, even
A permanent magnet magnetic shoe is respectively mounted in access slot, adjacent two permanent magnets magnetic shoe inner surface is magnetic opposite.Magnet exciting coil stator includes stator
Ring, several magnet exciting coils, the corresponding magnet exciting coil of each permanent magnet magnetic shoe, magnet exciting coil is mounted on track ring, on track ring
Several Hall sensors are installed, Hall sensor is radially orientated the setting of permanent magnet magnetic shoe, Hall sensor, magnet exciting coil and control
System electrical connection.The brshless DC motor smooth running that this structure setting is constituted is reliable.
Compared with prior art, the utility model has the beneficial effects that (1) Crossed Circle rotor spherical tanks wind stick
Blade is hidden in protective cover, and will not collide the phenomenon that fractureing in rotation process, and screw blade leaf length is short, favorably
In the rigors reduced to propeller blade intensity and rotor blade is replaced without frequent, posture adjustment is convenient in aircraft flight
Reliably；(2) Crossed Circle rotor spherical tanks aircraft enormously simplifies drive mechanism, mitigates aircraft self weight, reduces maintenance intensity and takes
With, increase power output radius, reduce the requirement to engine power, considerably reduce energy consumption, be not necessarily to empennage, structure
Simple optimization.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of the utility model；
Fig. 2 is the explosive view of the utility model；
Fig. 3 is the posture adjustment schematic diagram of the utility model；
Fig. 4 is the partial sectional view of the embodiments of the present invention 1；
Fig. 5 is the suspension theory figure of the suspended ring of the embodiments of the present invention 1；
Fig. 6 is the schematic diagram of the brshless DC motor of the utility model；
In figure: 1, spherical tanks, 2, upper protective cover, 3, lower protective cover, 4, rotor fixed ring, 5, upper rotor rotor, 6, backspin
Wing rotor, 7, control system, 8, air grid, 9, posture adjustment ring, 10, posture adjustment joint shaft, 11, cabin joint shaft, 12, posture adjustment electricity
Machine, 13, sports ring, 14, strong magnet rotor, 15, rotor blade, 16, magnet exciting coil stator, 17, gyroscope, 18, mounting groove, 19,
Suspended ring, 20, absorption ring, 21, movable permanent-magnetic clamp, 22, fixed permanent-magnetic clamp, 23, electromagnetic block, 24, displacement sensor, 25, protection
Ring, 26, anticollision bearing, 27, reinforcing ring, 28, battery, 29, undercarriage, 30, positioning convex ring, 31, Gai Hehuan, 32, rotor ring,
33, permanent magnet magnetic shoe, 34, link slot, 35, track ring, 36, magnet exciting coil, 37, Hall sensor, 38, aluminium alloy inductance loop,
39, extended loop.
Specific embodiment
Below by specific embodiment, and in conjunction with attached drawing, the technical solution of the utility model work is further specifically retouched
It states:
Embodiment 1: a kind of Crossed Circle rotor spherical tanks aircraft (referring to attached drawing 1 to attached drawing 6), including spherical tanks 1, upper protection
Cover 2, lower protective cover 3, rotor fixed ring 4, upper rotor rotor 5, lower rotor rotor 6, control system 7, upper protective cover, lower protection
Cover, upper rotor rotor, lower rotor rotor in a ring, are equipped with air grid 8, upper protective cover on upper protective cover, lower protective cover
It links together with the outer ring of lower protective cover, rotor fixed ring is connected between protective cover and the inner ring of lower protective cover, rotor
Posture adjustment ring 9 is rotatablely installed in fixed ring, spherical tanks are rotatably installed in posture adjustment ring, connect two between posture adjustment ring and rotor fixed ring
The posture adjustment joint shaft 10 being oppositely arranged, connects the two cabin joint shafts 11 being oppositely arranged between spherical tanks and posture adjustment ring, posture adjustment is closed
Nodal axisn and cabin joint shaft axis are vertical, and a posture adjustment joint shaft and a cabin joint shaft are sequentially connected posture adjustment motor 12；One
Posture adjustment motor is mounted in spherical tanks, and another posture adjustment motor is mounted in rotor fixed ring.Upper rotor rotor, lower rotor rotor are equal
Including sports ring 13, strong magnet rotor 14, several rotor blades 15 on sports ring are uniformly connected to, in rotor fixed ring and strong magnetic
The corresponding installation magnet exciting coil stator 16 of rotor, sports ring may be rotatably mounted in rotor fixed ring, install top in rotor fixed ring
Spiral shell instrument 17, posture adjustment motor, magnet exciting coil stator, gyroscope are electrically connected to the control system.Upper rotor rotor, lower rotor rotor turn
Dynamic direction is always on the contrary, rotor blade radial outer end is placed between protective cover and lower protective cover.Rotor on same sports ring
Blade outer end connects into an entirety by reinforcing ring 27.Control system is powered by battery 28, and battery and control system are equal
It is mounted in spherical tanks.Rotor fixed ring lower end connects several undercarriages 29 being uniformly arranged.Lower protective cover upper surface is close to outer
Marginal position is equipped with positioning convex ring 30, and upper protective cover lower surface outer edge is equipped with lid cyclization 31, and positioning convex ring is adapted to lid cyclization
Plug-in, the lower end Gai Hehuan is supported on lower protective cover upper surface.Strong magnet rotor includes rotor ring 32, permanent magnet magnetic shoe
33, several link slots 34 are laid on rotor ring, are respectively mounted a permanent magnet magnetic shoe in link slot, in adjacent two permanent magnets magnetic shoe
Surface magnetism is opposite.Magnet exciting coil stator includes track ring 35, several magnet exciting coils 36, the corresponding excitation of each permanent magnet magnetic shoe
Coil, magnet exciting coil are mounted on track ring, several Hall sensors 37 are installed on track ring, Hall sensor is radially orientated forever
The setting of magnet magnetic shoe, Hall sensor, magnet exciting coil are electrically connected to the control system.Sports ring is equipped with the extended loop extended downwardly
39, strong magnet rotor is connected on extended loop lower end inner wall.
Rotor fixed ring is equipped with the mounting grooves 18 of two annulars, is equipped with suspended ring 19 on sports ring, on suspended ring inner wall
Installation absorption ring 20, absorption ring are iron hoop, are equipped with levitation gap, suspended ring between suspended ring, absorption ring and installation groove sidewall
It is mounted on movable permanent-magnetic clamp 21 on upper and lower surfaces, installs in groove sidewall and movable permanent-magnetic clamp corresponding position is equipped with and fixes forever
Magnet ring 22, movable permanent-magnetic clamp are identical as the fixed opposite face magnetic pole of permanent-magnetic clamp；Several electromagnetic blocks are uniformly installed in rotor fixed ring
23, electromagnetic block is radially orientated absorption ring and the attraction absorption ring that can be powered, and is mounted in rotor fixed ring close to electromagnetic block position
It is radially orientated the displacement sensor 24 of absorption ring setting；Electromagnetic block, displacement sensor are electrically connected to the control system.On sports ring
Surface is equipped with protective ring 25, uniformly installs several anticollision bearings 26, anticollision bearing in the present embodiment on rotor fixed ring outer wall
Setting eight, is equipped with anticollision gap between anticollision bearing outer wall and protective ring inner wall, anticollision gap radial spacing is less than absorption ring
Radial spacing between inner wall and installation groove sidewall.It holds with anticollision shaft in rotor fixed ring and is correspondingly provided with mounting post, anticollision bearing
Inner ring is installed tightly in mounting post.It adsorbs and aluminium alloy inductance loop 38 is installed on ring inner wall, displacement sensor is radially orientated aluminium conjunction
Golden inductance loop, displacement sensor are eddy current displacement sensor.Electromagnetic block is in U-shape structure, and the both ends of electromagnetic block are respectively facing suction
The two sides up and down of aluminium alloy inductance loop on follower ring inner wall.It is equipped with locating slot with fixed permanent-magnetic clamp corresponding position on mounting groove inner wall,
Fixed permanent-magnetic clamp is securedly mounted in locating slot；Binding groove, movable permanent magnetism are equipped with movable permanent-magnetic clamp corresponding position on suspended ring
Ring is securedly mounted in binding groove.
Magnet exciting coil stator and strong magnet rotor constitute brshless DC motor, the operation of Crossed Circle rotor spherical tanks aircraft together
When, control system is powered to magnet exciting coil stator, and strong magnet rotor drives sports ring to rotate together.Upper rotor rotor, lower rotor turn
Sub- rotation direction is always on the contrary, the reaction torque that air generates is cancelled out each other, when the revolving speed for changing one of rotor rotor, aircraft
It can turn.Spherical tanks center is lower than lower protective cover close to lower end position, spherical tanks lower end.Pass through a pair of of posture adjustment joint shaft
With the setting of a pair of of cabin joint shaft, make to rotate between spherical tanks and rotor fixed ring with any angle.By control system control
Make two posture adjustment motors operating realize posture adjustment joint shaft and cabin joint shaft rotation, due to spherical tanks center of gravity always vertically to
Under, the rotation of posture adjustment joint shaft and cabin joint shaft makes rotor fixed ring form certain inclination angle relative to spherical tanks, and aircraft is
The thrust that can get a horizontal direction enables aircraft to fly to inclination direction.Dip angle signal that gyroscope will test and
Direction signal is transmitted to control system, control system according to gyroscope transmitting come signal instruction is issued to two posture adjustment motors,
Control the revolving speed and rotational angle of posture adjustment motor.Upper rotor rotor, lower rotor rotor be placed in protective cover and lower protective cover it
Between, the concealed setting of rotor blade, will not collide in rotation process the phenomenon that fractureing.Upper rotor rotor, lower rotor rotor
In a ring, screw blade leaf length is short, advantageously reduces the rigors to propeller blade intensity.Movable permanent-magnetic clamp and solid
The opposite face homopolar-repulsion for determining permanent-magnetic clamp makes suspended ring be in suspended state；It is remained between absorption ring and installation groove sidewall
There is gap, it is ensured that be in suspended state in sports ring rotation process always.Control system makes electromagnetic block to the energization of electromagnetic block coil
Attract absorption ring, the signal that displacement sensor detects is transported to control system, and control system is according to the displacement sensor of reading
Signal whether be powered to the coil of electromagnetic block and electrical current size controls.Electromagnetic block is staggered the time on-off, the same period
It is powered to the electromagnetic block of maximum distance position between the displacement sensor detected and absorption ring inner wall, to make the electromagnetism
Block attracts absorption ring, shortens the distance between displacement sensor and absorption ring inner wall.Control system reads displacement sensing
Device signal simultaneously sets the frequency of single electromagnetic block energization as needed, so that suspended ring be made to be in dynamic equilibrium shape always
State.Sports ring is in suspended state always in upper rotor rotor, lower rotor rotor rotation process, and vibration and noise is small, does not need
Lubrication, no mechanical wear, long service life, maintenance cost are low.
Embodiment 2: a kind of Crossed Circle rotor spherical tanks aircraft, structure is similar to Example 1, and main difference is this
Rolling bearing is installed between rotor fixed ring and sports ring in embodiment.Rolling bearing is used between rotor fixed ring and sports ring
Realize rotation connection, sports ring smooth running is reliable.Other structures are same as Example 1.
Embodiment described above is the preferable scheme of the utility model, is not made in any form to the utility model
Limitation, on the premise of not exceeding the technical scheme recorded in the claims there are also other variations and modifications.
Claims (8)
1. a kind of Crossed Circle rotor spherical tanks aircraft, characterized in that fixed including spherical tanks, upper protective cover, lower protective cover, rotor
Ring, upper rotor rotor, lower rotor rotor, control system, upper protective cover, lower protective cover, upper rotor rotor, lower rotor rotor are in
Annular, rotor fixed ring are connected between protective cover and the inner ring of lower protective cover, and posture adjustment ring is rotatablely installed in rotor fixed ring,
Spherical tanks are rotatably installed in posture adjustment ring, and the two posture adjustment joint shafts being oppositely arranged, ball are connected between posture adjustment ring and rotor fixed ring
The cabin joint shaft that connection two is oppositely arranged between shape cabin and posture adjustment ring, posture adjustment joint shaft and cabin joint shaft axis are vertical, and one
Posture adjustment joint shaft and a cabin joint shaft are sequentially connected posture adjustment motor；Upper rotor rotor, lower rotor rotor include movement
Ring, strong magnet rotor, several rotor blades being uniformly connected on sports ring, installation corresponding with strong magnet rotor is encouraged in rotor fixed ring
Magnetic coil stator, sports ring may be rotatably mounted in rotor fixed ring, and gyroscope is installed in rotor fixed ring, and posture adjustment motor is encouraged
Magnetic coil stator, gyroscope are electrically connected to the control system, and upper rotor rotor, lower rotor rotor rotation direction are always on the contrary, rotation
Wing blade radial outer end is placed between protective cover and lower protective cover.
2. Crossed Circle rotor spherical tanks aircraft according to claim 1, characterized in that rotor fixed ring is equipped with two annulars
Mounting groove, suspended ring is equipped on sports ring, installation absorption ring on suspended ring inner wall, suspended ring, absorption ring and mounting groove side
Be equipped with levitation gap between wall, be mounted on movable permanent-magnetic clamp on suspended ring upper and lower surfaces, install in groove sidewall and activity forever
Magnet ring corresponding position is equipped with fixed permanent-magnetic clamp, and movable permanent-magnetic clamp is identical as the fixed opposite face magnetic pole of permanent-magnetic clamp；Rotor is fixed
Several electromagnetic blocks are uniformly installed, electromagnetic block is radially orientated absorption ring and the attraction absorption ring that can be powered, leans in rotor fixed ring on ring
Nearly electromagnetic block position is mounted on the displacement sensor for being radially orientated absorption ring setting；Electromagnetic block, displacement sensor with control
System electrical connection.
3. Crossed Circle rotor spherical tanks aircraft according to claim 2, characterized in that sports ring upper surface is equipped with protection
Ring uniformly installs several anticollision bearings on rotor fixed ring outer wall, and anticollision is equipped between anticollision bearing outer wall and protective ring inner wall
Gap, anticollision gap radial spacing are less than absorption ring inner wall and install the radial spacing between groove sidewall.
4. Crossed Circle rotor spherical tanks aircraft according to claim 1, characterized in that between rotor fixed ring and sports ring
Rolling bearing is installed.
5. Crossed Circle rotor spherical tanks aircraft according to claim 1, characterized in that the rotor blade on same sports ring
Outer end connects into an entirety by reinforcing ring.
6. Crossed Circle rotor spherical tanks aircraft according to claim 1, characterized in that lower protective cover upper surface is close to outside
Edge position is equipped with positioning convex ring, and upper protective cover lower surface outer edge is equipped with lid cyclization, and positioning convex ring is adapted to lid cyclization and is inserted into
Together, the lower end Gai Hehuan is supported on lower protective cover upper surface.
7. according to claim 1 to Crossed Circle rotor spherical tanks aircraft described in 6 any one, characterized in that strong magnet rotor packet
Rotor ring, permanent magnet magnetic shoe are included, several link slots are laid on rotor ring, a permanent magnet magnetic shoe, phase are respectively mounted in link slot
Two permanent magnet magnetic shoe inner surface of neighbour is magnetic opposite.
8. Crossed Circle rotor spherical tanks aircraft according to claim 7, characterized in that magnet exciting coil stator includes stator
Ring, several magnet exciting coils, the corresponding magnet exciting coil of each permanent magnet magnetic shoe, magnet exciting coil is mounted on track ring, on track ring
Several Hall sensors are installed, Hall sensor is radially orientated the setting of permanent magnet magnetic shoe, Hall sensor, magnet exciting coil and control
System electrical connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920183985.4U CN209545468U (en) | 2019-02-01 | 2019-02-01 | Crossed Circle rotor spherical tanks aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920183985.4U CN209545468U (en) | 2019-02-01 | 2019-02-01 | Crossed Circle rotor spherical tanks aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209545468U true CN209545468U (en) | 2019-10-25 |
Family
ID=68272979
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920183985.4U Active CN209545468U (en) | 2019-02-01 | 2019-02-01 | Crossed Circle rotor spherical tanks aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209545468U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109878712A (en) * | 2018-02-28 | 2019-06-14 | 史智勇 | A kind of Crossed Circle rotor spherical tanks aircraft |
-
2019
- 2019-02-01 CN CN201920183985.4U patent/CN209545468U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109878712A (en) * | 2018-02-28 | 2019-06-14 | 史智勇 | A kind of Crossed Circle rotor spherical tanks aircraft |
| CN109878712B (en) * | 2018-02-28 | 2020-08-11 | 浙江安浮航空科技有限公司 | Spherical cabin aircraft of two annular rotors |
| EP3760540A4 (en) * | 2018-02-28 | 2021-11-17 | Shi, Zhiyong | Double-ring rotating wing spherical cabin aircraft |
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Legal Events
| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200628 Address after: Room 1016, building 1, No. 51, Jiusheng Road, Jianggan District, Hangzhou City, Zhejiang Province Patentee after: Zhejiang Anfu Aviation Technology Co., Ltd Address before: 310000 Room 302, Unit 1, 4 South Nine Courts, Daguanyuan, Gongshu District, Hangzhou City, Zhejiang Province Patentee before: Shi Zhiyong |
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| TR01 | Transfer of patent right |