CN105129088B - Spherical uniaxial rudder oriented intelligent aircraft - Google Patents
Spherical uniaxial rudder oriented intelligent aircraft Download PDFInfo
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- CN105129088B CN105129088B CN201510619038.1A CN201510619038A CN105129088B CN 105129088 B CN105129088 B CN 105129088B CN 201510619038 A CN201510619038 A CN 201510619038A CN 105129088 B CN105129088 B CN 105129088B
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Abstract
The invention relates to a spherical uniaxial rudder oriented intelligent aircraft, which comprises a hollow sphere (1) and is characterized in that a main paddle (22) is arranged in a vertical direction of the hollow sphere (1), and controls rising or descending of the aircraft; a first sub-paddle (31) and a second sub-paddle (41) which are capable of rotating forwards and backwards are arranged in the horizontal direction of the hollow sphere (1) and control moving of the aircraft in the horizontal direction. The spherical uniaxial rudder oriented intelligent aircraft flies in two manners of rotary wings and a fixed wing, so the aircraft has respective advantages of the rotary wings and the fixed wing, the rotary wings are used for realizing control and suspension stop in a flying direction, and realizing vertical taking off and landing, and the fixed wing is used for realizing high speed flying after achieving certain height.
Description
Technical field
The present invention relates to a kind of aircraft, is oriented to Intelligent flight device more particularly, to a kind of spherical single shaft rudder.
Background technology
Multi-axis aircraft can realize hovering and flying in multi-direction, but not readily portable and rotor blade break object and
Accident Jing of people of injuring often occurs；As flight efficiency is different, the common fault of rotor craft is flying radius well below fixation
Rotor aircraft；Rotor craft windage is big, and during operation, wind resistance is bad in the wild；Airborne equipment intelligent level is low；It is airborne to take the photograph
As head and induction apparatuss as Flight Vehicle Structure has dead angle.Spherical single shaft aircraft is reversely rotated to provide using DCB Specimen and is risen at present
Power, it is difficult to operate, continuation of the journey and flight speed can only accomplish remote-control toy level application.
The content of the invention
The present invention devises a kind of spherical single shaft rudder and is oriented to Intelligent flight device, and its technical problem for solving is current spherical list
Axle aircraft is reversely rotated using DCB Specimen and provides lift, it is difficult to operated, continuation of the journey and flight speed can only accomplish remote-control toy level
Using.
In order to solve above-mentioned technical problem, below scheme is present invention employs：
A kind of spherical single shaft rudder is oriented to Intelligent flight device, including hollow ball（1）, it is characterised in that：In hollow ball（1）
Vertical direction be provided with main blade（22）, which controls rising or falling for aircraft；In hollow ball（1）Horizontal direction be provided with
Can rotating first time blade（31）With second blade（41）, they control aircraft and move in the horizontal direction.
Further, the hollow ball（1）Vertical direction be provided with main air duct（5）, main blade（22）Positioned at main air duct（5）
Among, main blade（22）By mair motor（21）Drive；In the hollow ball（1）Inwall at least provided with main air duct first
Commutator segment（51）With the second commutator segment of main air duct（52）.
Further, the first commutator segment of the main air duct（51）Or/and the second commutator segment of main air duct（52）For ridge structure, its
Mid portion is raised.
Further, the hollow ball（1）By upper body（11）And lower case（12）Combination is assembled, it is described on
Portion's housing（11）Upper end is upper protective cover grid（13）, the lower case（12）Lower end is lower protective cover grid（14）, upper guarantor
Shield grid（13）With lower protective cover grid（14）Between passage be main air duct（5）.
Further, the main blade（22）Using coaxial two reverse blade overlaying structures, or torsion is offset by little blade
The single-blade impeller structure of power.
Further, the hollow ball（1）Horizontal direction be provided with first time air channel（6）With second air channel（7）；First
Secondary air channel（6）With second air channel（7）Positioned at the hollow ball（1）In cavity between inside and outside wall, and according to the sky
Bulbus cordis body（1）Arc sphere extends；In the hollow ball（1）Two the first air inlet/outlets are provided with outer wall（15）With two
Two air inlet/outlets（16）；First time air channel（6）By two the first air inlet/outlets（15）Enter and travel out gas, first time air channel（6）
In be provided with can rotating first time blade（31）, first time blade（31）By first time motor（32）Drive；Second wind
Road（7）By two the second air inlet/outlets（16）Enter and travel out gas, second air channel（7）In be provided with can rotating second oar
Leaf（41）, second blade（41）By second motor（42）Drive.
Further, first time blade（31）With first time motor（32）It is arranged on the first commutator segment of the main air duct（51）Mountain
In groove inside ridge structure, in the first commutator segment of main air duct（51）The texturearunaperpendicular direction pass through intermediate membrane（63）Will
First time air channel（6）Two parts are isolated into, in intermediate membrane（63）On be provided with through hole, first time blade（31）Positioned at the through hole
Among；Second blade（41）With second motor（42）It is arranged on the second commutator segment of the main air duct（52）Ridge inside configuration
Groove in, in the second commutator segment of main air duct（52）The texturearunaperpendicular direction pass through intermediate membrane（73）By second air channel
（7）Two parts are isolated into, in intermediate membrane（73）On be provided with through hole, second blade（41）Among the through hole.
Further, first time air channel（6）With second air channel（7）It is mutually isolated, and with hollow ball（1）One diameter pair
Claim distribution.
Further, first time motor（32）By first time motor supporting base（321）It is fixed on hollow ball（1）Outer wall with
The first commutator segment of main air duct（51）Between, second motor（42）By second motor supporting base（421）It is fixed on hollow ball
Body（1）Outer wall and the second commutator segment of main air duct（52）Between.
Further, in the hollow ball（1）Slide rail type photographic head is installed on spherical housing.
The spherical single shaft rudder is oriented to Intelligent flight device compared with existing aircraft, has the advantages that：
（1）The present invention is due to being flown using rotor and fixed-wing two ways so that aircraft has rotor and solid simultaneously
Determine the respective advantage of the wing, rotor realizes the control and hovering of heading, and is capable of achieving VTOL, solid after arrival certain altitude
Determine the wing and can realize high-speed flight.
（2）Aircraft of the present invention adopts spherical housing and for spherical band aperture plate shell, can prevent propeller from hurting sb.'s feelings
Thing, and windage is reduced, lift wind resistance.
（3）The present invention adopts slide rail type photographic head, airborne photographic head and induction apparatuss can in spherome surface all-directional rotation,
Dead angle is not sensed.
Description of the drawings
Fig. 1：The spherical single shaft rudder of the present invention is oriented to the perspective interior structural representation of Intelligent flight device；
Fig. 2：The spherical single shaft rudder of the present invention is oriented to the three-dimensional external structure schematic diagram of Intelligent flight device；
Fig. 3：The spherical single shaft rudder of the present invention is oriented to the top view of Intelligent flight device；
Fig. 4：The spherical single shaft rudder of the present invention is oriented to the front view of Intelligent flight device.
Description of reference numerals：
1 hollow ball；11 upper bodies；12 lower cases；Protective cover grid on 13；14 times protective cover nets
Lattice；15 first air inlet/outlets；16 second air inlet/outlets；21 mair motors；22 main blades；23 pedestals；31 first
Secondary blade；32 first time motors；321 first time motor supporting bases；41 second blade；42 second motor；
421 second motor supporting base；5 main air ducts；51 the first commutator segments of main air duct；52 the second commutator segments of main air duct；6—
First time air channel；Dividing plate before 61；62 rear bulkheads；63 intermediate membranes；7 second air channel；Dividing plate before 71；After 72
Dividing plate；73 intermediate membranes.
Specific embodiment
With reference to Fig. 1 to Fig. 4, the present invention will be further described：
The spherical housing of the present invention：Using composite, plastics and metal, upper and lower has air inlet and outlet aperture plate.Power
System：Motor, propeller, electricity are adjusted, direction rudder blade, battery.Electronic system：The winged control of intelligence, communication module, induction apparatuss include red
Outward, ultrasound wave, laser, gyroscope, gravity sensor, acceleration induction apparatuss, GPS, shooting are first-class.
Aircraft power is provided with propeller, heading control and hovering are realized by direction rudder blade, and be capable of achieving to hang down
Straight landing, reaches certain altitude, and propeller is by vertically switching to horizontal direction, and high-speed flight.
The fixed high constant speed of aircraft and automatic airline operation are realized by electronic system, avoidance are realized by induction apparatuss, with
And layout of roads.
Communication with control end, monitoring and management aircraft are realized by communication system.
Script of taking photo by plane can be realized, track up to subject is realized with modes such as bat, ring bats according to forward and backward.
Specifically：
A kind of spherical single shaft rudder is oriented to Intelligent flight device, including hollow ball 1, is provided with the vertical direction of hollow ball 1
Main blade 22, which controls rising or falling for aircraft；The horizontal direction of hollow ball 1 be provided with can rotating first time oar
Leaf 31 and second blade 41, they control aircraft and move in the horizontal direction.
The vertical direction of hollow ball 1 is provided with main air duct 5, and among main blade 22 is located at main air duct 5, main blade 22 is by master
Motor 21 drives；At least provided with the first commutator segment of main air duct 51 and the second commutator segment of main air duct 52 on the inwall of hollow ball 1.
Mair motor 21 is arranged on pedestal 23, and pedestal 23 is fixed on the inwall of hollow ball 1 by many fix bars.
The first commutator segment of main air duct 51 or/and the second commutator segment of main air duct 52 are ridge structure, and intermediate portion is raised.
Hollow ball 1 is assembled by upper body 11 and the combination of lower case 12, and 11 upper end of upper body is upper protection
Cover grid 13,12 lower end of lower case are lower protective cover grid 14, are led between upper protective cover grid 13 and lower protective cover grid 14
Road is main air duct 5.Upper and lower protective cover grid can prevent propeller from hurting sb.'s feelings thing, and reduce windage, lift wind resistance.
Main blade 22 is using coaxial two reverse blade overlaying structures, or the single-blade leaf knot that torsion is offset by little blade
Structure.
The horizontal direction of hollow ball 1 is provided with first time air channel 6 and second air channel 7；First time air channel 6 and second wind
Road 7 is located in the cavity between 1 inside and outside wall of hollow ball, and is extended according to 1 arc sphere of the hollow ball；In hollow ball
Two the first air inlet/outlets 15 and two the second air inlet/outlets 16 are provided with 1 outer wall of body；First time, air channel 6 entered by two first
Gas outlet 15 is entered to travel out gas, be provided with first time air channel 6 can rotating first time blade 31, first time blade 31 is by the
No. one time motor 32 drives；Second air channel 7 is entered to travel out gas by two the second air inlet/outlets 16, is provided with second air channel 7
Can rotating second blade 41, second blade 41 driven by second motor 42.
First time blade 31 and first time motor 32 are arranged on the groove of 51 ridge inside configuration of the first commutator segment of main air duct
In, first time air channel 6 is isolated into by two parts by intermediate membrane 63 in the texturearunaperpendicular direction of the first commutator segment of main air duct 51,
Through hole is provided with intermediate membrane 63, among first time blade 31 is located at through hole；Second blade 41 and second motor 42 set
Put in the groove of 52 ridge inside configuration of the second commutator segment of main air duct, in the texturearunaperpendicular direction of the second commutator segment of main air duct 52
Second air channel 7 is isolated into by two parts by intermediate membrane 73, through hole is provided with intermediate membrane 73, second blade 41
Among through hole.
First time air channel 6 and second air channel 7 it is mutually isolated and symmetrical with 1 one diameter of hollow ball.The isolation
Concrete structure is：First time, two ends in air channel 6 were respectively equipped with front dividing plate 61 and rear bulkhead 62.In the same manner, second air channel 7
Two ends are also respectively equipped with front dividing plate 71 and rear bulkhead 72.Two air channels can use same front dividing plate and same rear bulkhead,
Independent front dividing plate and rear bulkhead can also be used.
It is whole with main air duct first that first time motor 32 is fixed on 1 outer wall of hollow ball by first time motor supporting base 321
Between flow 51, second motor 42 is fixed on 1 outer wall of hollow ball and main air duct second by second motor supporting base 421
Between commutator segment 52.
Slide rail type photographic head is installed on 1 spherical housing of hollow ball.Airborne photographic head and induction apparatuss can be in spheroids
Surface all-directional rotation, does not sense dead angle.
First time blade 31 and second blade 41 carry out the control of heading by following control mode：
1st, while advancing or retreating with revolution in the same direction；
2nd, only one is rotated or one rotates forward a reversion and turns to.
Main blade 22 carries out the control of heading by following control mode：
1st, vertical rotor is moved up and down or is hovered.
Exemplary description is carried out to the present invention above in conjunction with accompanying drawing, it is clear that aforesaid way is not received in the realization of the present invention
Restriction, it is as long as employing method of the present invention design and the various improvement that carry out of technical scheme, or not improved by the present invention
Design and technical scheme directly apply to other occasions, within the scope of the present invention.
Claims (9)
1. a kind of spherical single shaft rudder is oriented to Intelligent flight device, including hollow ball（1）, it is characterised in that：In hollow ball（1）'s
Vertical direction is provided with main blade（22）, which controls rising or falling for aircraft；In hollow ball（1）Horizontal direction be provided with can
The first time blade of rotating（31）With second blade（41）, which controls aircraft and moves in the horizontal direction；The hollow ball
Body（1）Horizontal direction be provided with first time air channel（6）With second air channel（7）；First time air channel（6）With second air channel（7）
Positioned at the hollow ball（1）In cavity between inside and outside wall, and according to the hollow ball（1）Arc sphere extends；
The hollow ball（1）Two the first air inlet/outlets are provided with outer wall（15）With two the second air inlet/outlets（16）；First time wind
Road（6）By two the first air inlet/outlets（15）Enter and travel out gas, first time air channel（6）In be provided with can rotating first time oar
Leaf（31）, first time blade（31）By first time motor（32）Drive；Second air channel（7）By two the second air inlet/outlets
（16）Enter and travel out gas, second air channel（7）In be provided with can rotating second blade（41）, second blade（41）Pass through
Second motor（42）Drive.
2. spherical single shaft rudder is oriented to Intelligent flight device according to claim 1, it is characterised in that：The hollow ball（1）'s
Vertical direction is provided with main air duct（5）, main blade（22）Positioned at main air duct（5）Among, main blade（22）By mair motor（21）Drive
It is dynamic；In the hollow ball（1）Inwall at least provided with the first commutator segment of main air duct（51）With the second commutator segment of main air duct
（52）.
3. spherical single shaft rudder is oriented to Intelligent flight device according to claim 2, it is characterised in that：The first rectification of the main air duct
Piece（51）Or/and the second commutator segment of main air duct（52）For ridge structure, intermediate portion projection.
4. according to Claims 2 or 3, spherical single shaft rudder is oriented to Intelligent flight device, it is characterised in that：The hollow ball（1）
By upper body（11）And lower case（12）Combination is assembled, the upper body（11）Upper end is upper protective cover grid
（13）, the lower case（12）Lower end is lower protective cover grid（14）, upper protective cover grid（13）With lower protective cover grid
（14）Between passage be main air duct（5）.
5. spherical single shaft rudder is oriented to Intelligent flight device according to claim 4, it is characterised in that：The main blade（22）Using
Coaxial two reverse blade overlaying structures, or the single-blade impeller structure that torsion is offset by little blade.
6. spherical single shaft rudder is oriented to Intelligent flight device according to claim 2, it is characterised in that：First time blade（31）With
Motor（32）It is arranged on the first commutator segment of the main air duct（51）It is in the groove of ridge inside configuration, whole in main air duct first
Flow（51）The texturearunaperpendicular direction pass through intermediate membrane（63）By first time air channel（6）Two parts are isolated into, at middle part
Dividing plate（63）On be provided with through hole, first time blade（31）Among the through hole；Second blade（41）With second motor
（42）It is arranged on the second commutator segment of the main air duct（52）In the groove of ridge inside configuration, in the second commutator segment of main air duct（52）
The texturearunaperpendicular direction pass through intermediate membrane（73）By second air channel（7）Two parts are isolated into, in intermediate membrane（73）
On be provided with through hole, second blade（41）Among the through hole.
7. spherical single shaft rudder is oriented to Intelligent flight device according to claim 1, it is characterised in that：First time air channel（6）With
Secondary air duct（7）It is mutually isolated, and with hollow ball（1）One diameter is symmetrical.
8. spherical single shaft rudder is oriented to Intelligent flight device according to claim 7, it is characterised in that：First time motor（32）Pass through
First time motor supporting base（321）It is fixed on hollow ball（1）Outer wall and the first commutator segment of main air duct（51）Between, second electricity
Machine（42）By second motor supporting base（421）It is fixed on hollow ball（1）Outer wall and the second commutator segment of main air duct（52）It
Between.
9. according to any one of claim 1,2,3,5,6,7 or 8, spherical single shaft rudder is oriented to Intelligent flight device, its feature
It is：In the hollow ball（1）Slide rail type photographic head is installed on spherical housing.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510619038.1A CN105129088B (en) | 2015-09-25 | 2015-09-25 | Spherical uniaxial rudder oriented intelligent aircraft |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510619038.1A CN105129088B (en) | 2015-09-25 | 2015-09-25 | Spherical uniaxial rudder oriented intelligent aircraft |
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| CN105129088B true CN105129088B (en) | 2017-03-22 |
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Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105480406B (en) | 2015-12-31 | 2017-07-21 | 歌尔科技有限公司 | A kind of single shaft aircraft |
| CN105527382B (en) * | 2016-01-05 | 2018-03-02 | 杭州潮流玩具有限公司 | A kind of fly able air detection equipment and use its mobile terminal |
| CN107539466B (en) * | 2016-06-29 | 2021-04-27 | 北京末元科技有限公司 | A unmanned aerial vehicle for panorama shooting |
| CN107028566B (en) * | 2017-03-21 | 2019-10-11 | 上海大学 | The clean robot of variable appearance flight |
| CN110040246B (en) * | 2018-01-15 | 2022-05-24 | 江尚峰 | Single-shaft double-rotor unmanned aerial vehicle device, system with same and remote control method |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102785775A (en) * | 2012-08-08 | 2012-11-21 | 中国科学院长春光学精密机械与物理研究所 | Multi-rotor aircraft with rolling function |
| CN202777799U (en) * | 2012-09-07 | 2013-03-13 | 广东佳奇塑胶有限公司 | Infrared remote control toy fire balloon |
| CN202896880U (en) * | 2012-10-08 | 2013-04-24 | 西北工业大学 | Spherical micro unmanned aerial vehicle |
| CN203876983U (en) * | 2014-05-02 | 2014-10-15 | 李佳辉 | Spherical flight device |
| CN204399482U (en) * | 2014-12-26 | 2015-06-17 | 郑州中电新能源汽车有限公司 | The electronic unmanned fog machine of a kind of DCB Specimen close coupled type anticollision |
| CN205060017U (en) * | 2015-09-25 | 2016-03-02 | 高翔宇 | Intelligent aircraft of spherical unipolar rudder direction |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2804936B1 (en) * | 2000-02-15 | 2002-06-07 | Bertin Technologies Sa | REMOTE CONTROL FLYING VEHICLE, IN PARTICULAR FOR SURVEILLANCE OR INSPECTION |
| US20050029397A1 (en) * | 2003-07-21 | 2005-02-10 | Yearwood Charles Christopher | Flying saucer |
-
2015
- 2015-09-25 CN CN201510619038.1A patent/CN105129088B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102785775A (en) * | 2012-08-08 | 2012-11-21 | 中国科学院长春光学精密机械与物理研究所 | Multi-rotor aircraft with rolling function |
| CN202777799U (en) * | 2012-09-07 | 2013-03-13 | 广东佳奇塑胶有限公司 | Infrared remote control toy fire balloon |
| CN202896880U (en) * | 2012-10-08 | 2013-04-24 | 西北工业大学 | Spherical micro unmanned aerial vehicle |
| CN203876983U (en) * | 2014-05-02 | 2014-10-15 | 李佳辉 | Spherical flight device |
| CN204399482U (en) * | 2014-12-26 | 2015-06-17 | 郑州中电新能源汽车有限公司 | The electronic unmanned fog machine of a kind of DCB Specimen close coupled type anticollision |
| CN205060017U (en) * | 2015-09-25 | 2016-03-02 | 高翔宇 | Intelligent aircraft of spherical unipolar rudder direction |
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