CN106794897A - A kind of multi-rotor unmanned aerial vehicle - Google Patents
A kind of multi-rotor unmanned aerial vehicle Download PDFInfo
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- CN106794897A CN106794897A CN201680002964.7A CN201680002964A CN106794897A CN 106794897 A CN106794897 A CN 106794897A CN 201680002964 A CN201680002964 A CN 201680002964A CN 106794897 A CN106794897 A CN 106794897A
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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
- B64U10/13—Flying platforms
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/26—Ducted or shrouded rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/296—Rotors with variable spatial positions relative to the UAV body
- B64U30/297—Tilting rotors
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- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
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Abstract
A kind of multi-rotor unmanned aerial vehicle (100),Including main casing (10),First rotor group (11),Second rotor group (12) and the 3rd rotor group (13),The main casing (10) includes two faceted pebbles of the end face plane of reference (101) of two end face plane of references being oppositely arranged and connection,The first rotor group (11) is symmetrically distributed in the both sides of the 3rd rotor group (13) with the second rotor group (12),The shaft parallel of rotor is in the end face plane of reference in the first rotor group (11) and the second rotor group (12),The first rotor group (11) and the second rotor group (12) are for driving the multi-rotor unmanned aerial vehicle (100) to be moved parallel to the end face plane of reference direction,The positive identical and vertical sub end face plane of reference of the rotating shaft of rotor in the 3rd rotor group (13).The multi-rotor unmanned aerial vehicle (100) is suspended in ground/water surface by the 3rd rotor group (13), so that the multi-rotor unmanned aerial vehicle (100) is in vacant state, the multi-rotor unmanned aerial vehicle (100) can be eliminated the frictional force for producing is contacted with ground/water surface, effectively reduce the resistance of motion.
Description
Technical field
The application is related to unmanned air vehicle technique field, more particularly to a kind of unmanned plane of many rotors.
Background technology
With the continuous progress of scientific and technological society, the growth progressively of unmanned plane industry, multi-rotor aerocraft is due to machinery
Simple structure, dynamical system is simple, can be have developed rapidly the advantages of VTOL, and a time researcher goes after like a flock of ducks, and opens one after another
The research of beginning multi-rotor aerocraft is used, and has one by the commercialized upsurge of many rotors in global range.
Unmanned plane of the prior art, more complicated task or unmanned plane is realized to unmanned plane can be gone complete
Multifunction, the scope of activities of unmanned plane be not confined to initial sky flight already.And current land, water and air integration nothing
Man-machine research is then less, therefore is difficult to meet increasingly complicated use environment requirement.
The content of the invention
The purpose of the application is that offer can be adapted to various working environments, particularly adapts to many rotors of land and water environment
Unmanned plane.
To achieve the above object, the application provides following technical scheme：
A kind of multi-rotor unmanned aerial vehicle, including main casing, the first rotor group, the second rotor group and the 3rd rotor group, the master
Housing includes two end face plane of references being oppositely arranged and the faceted pebble being connected between described two end face plane of references, described first
Rotor group, the second rotor group and the 3rd rotor group are arranged on the faceted pebble, the first rotor group and described
Two rotor groups are symmetrically distributed in the both sides of the 3rd rotor group, rotor in the first rotor group and the second rotor group
Shaft parallel is used to drive the unmanned plane flat in the end face plane of reference, the first rotor group and the second rotor group
, in end face plane of reference direction motion, the rotating shaft of rotor is positive identical and perpendicular to the end face in the 3rd rotor group for row
The plane of reference.
Wherein, the first rotor group includes the first rotor and the second rotor, and the second rotor group includes the 3rd rotor
With the 4th rotor, the shaft parallel of first rotor, second rotor, the 3rd rotor and the 4th rotor is in institute
The end face plane of reference is stated, first rotor and the 3rd rotor are symmetrical arranged and for common relative to the 3rd rotor group
Drive the unmanned plane to be moved towards first direction, second rotor and the 4th rotor be used to driving jointly it is described nobody
Machine is moved towards second direction, and the first direction and the second direction are conversely, the 3rd rotor group includes the 5th rotor
With the 6th rotor, the 5th rotor is positive with the rotating shaft of the 6th rotor identical and perpendicular to the end face plane of reference.
Wherein, the main casing is in positive six prismsby structure, and first rotor and second rotor are divided into two phases
On adjacent faceted pebble, the 3rd rotor and the 4th rotor are divided on two other adjacent faceted pebble, the 5th rotor
Belong to not with first rotor, second rotor, the 3rd rotor and the 4th rotor with the 6th rotor
On the same faceted pebble, first rotor, second rotor, the 3rd rotor, the 4th rotor, the 5th rotation
The rotating shaft of the wing and the 6th rotor is respectively parallel to the corresponding faceted pebble.
Wherein, the positive rotating shaft forward direction with second rotor of the rotating shaft of first rotor is located remotely from each other setting, described
The positive rotating shaft forward direction with the 4th rotor of rotating shaft of the 3rd rotor is located remotely from each other setting.
Wherein, first rotor, the 3rd rotor, second rotor, the 4th rotor, the 5th rotor
It is in regular hexagon structure, the seamed edge appearance of the length of side of the regular hexagon and the six prisms bottom surface with the 6th rotor
Deng.
Wherein, also including base, the base includes top surface and side wall, and the top surface and side wall form hollow cavity,
The cavity is in communication with the outside, and the top surface is provided with through hole and mounting groove, the through hole and the 5th rotor and the described 6th
Rotor is connected, and the main casing, the first rotor group, the second rotor group and the 3rd rotor group are installed on the peace
Tankage.
Wherein, the cavity is incremented by by top surface parallel to the area of section of the top surface along the vertical top surface direction.
Wherein, the base is made up of elastomeric material.
Wherein, also it is provided with described first on the main casing faceted pebble including the first magnetic medium and the second magnetic medium
Magnetic medium, first rotor, second rotor, the 3rd rotor and the 4th rotor are provided with second magnetic
Property medium, first magnetic medium is attracted each other with second magnetic medium, and slot is additionally provided with the main casing faceted pebble,
It is respectively equipped with first rotor, second rotor, the 3rd rotor and the 4th rotor and is matched with the slot
The latch of conjunction.
Wherein, the slot is in cross.
The shaft parallel of rotor is referred in the end face in heretofore described first rotor group and the second rotor group
Face, the first rotor group and the second rotor group drive the unmanned plane parallel to end face plane of reference direction fortune
Dynamic, the rotating shaft of rotor is positive identical and perpendicular to the end face plane of reference in the 3rd rotor group.By the 3rd rotor
The multi-rotor unmanned aerial vehicle is suspended in ground/water surface by group so that multi-rotor unmanned aerial vehicle vacant state, can eliminate many rotors without
It is man-machine that the frictional force for producing, the resistance of motion for effectively reducing are contacted with ground/water surface.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
The accompanying drawing to be used needed for having technology description is briefly described, it should be apparent that, drawings in the following description are only this
Some embodiments of invention, for those of ordinary skill in the art, on the premise of not paying creative work, can be with
Other accompanying drawings are obtained according to these accompanying drawings.
The multi-rotor unmanned aerial vehicle schematic diagram that Fig. 1 is provided for a kind of implementation method of the application.
Fig. 2 is the decomposition view of the multi-rotor unmanned aerial vehicle shown in Fig. 1.
Fig. 3 is the structure diagram of the multi-rotor unmanned aerial vehicle shown in Fig. 1.
Specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.Base
Embodiment in the present invention, it is all that those of ordinary skill in the art are obtained on the premise of creative work is not made
Other embodiments, belong to the scope of protection of the invention.
Additionally, the explanation of following embodiment is with reference to additional diagram, it is used to illustrate the spy that the present invention may be used to implement
Determine embodiment.The direction term being previously mentioned in the present invention, for example, " on ", D score, "front", "rear", "left", "right", " interior ",
" outward ", " side " etc., is only the direction with reference to annexed drawings, therefore, the direction term for using is to more preferably, more clearly say
The bright and understanding present invention, must be with specific orientation, with specific square rather than the device or element for indicating or infer meaning
Position construction and operation, therefore be not considered as limiting the invention.
In the description of the invention, it is necessary to illustrate, unless otherwise clearly defined and limited, term " installation ", " phase
Company ", " connection " should be interpreted broadly, for example, it may be being fixedly connected, or detachably connected, or integratedly connect
Connect；Can mechanically connect；Can be joined directly together, it is also possible to be indirectly connected to by intermediary, can be in two elements
The connection in portion.For the ordinary skill in the art, above-mentioned term tool in the present invention can be understood with concrete condition
Body implication.
Additionally, in the description of the invention, unless otherwise indicated, " multiple " is meant that two or more.If this
Occur the term of " operation " in specification, it refers not only to independent operation, when cannot clearly be distinguished with other operations, as long as
Can realize that the effect desired by the operation is then also included within this term.In addition, the numerical value model represented with "~" in this specification
Enclose the scope that the numerical value for referring to record before and after "~" is included as minimum value and maximum.In the accompanying drawings, structure
Similar or identical is indicated by the same numeral.
Fig. 1 and Fig. 2 is referred to, multi-rotor unmanned aerial vehicle of the invention 100 includes：Main casing 10, the first rotor group 11 and
Two rotor groups 12 and the 3rd rotor group 13.The main casing 10 includes two end face plane of references being oppositely arranged and connection described two
The faceted pebble 101 of the individual end face plane of reference, the end face plane of reference here refers to the two ends of main casing 10 perpendicular to the section of the faceted pebble.
The first rotor group 11, the second rotor group 12 and the 3rd rotor group 13 are installed on the faceted pebble of the main casing 10
On 101.The first rotor group 11 is symmetrically distributed in the both sides of the 3rd rotor group 13 with the second rotor group 12.It is described
First rotor group 11 and the second rotor group 12 include multiple rotors, the first rotor group 11 and second rotor respectively
The shaft parallel of rotor is used for band in the end face plane of reference, the first rotor group 11 and the second rotor group 12 in group 12
Move the unmanned plane to be moved parallel to the end face plane of reference direction, the rotating shaft forward direction phase of rotor in the 3rd rotor group 13
Together and perpendicular to the end face plane of reference.The effect of the 3rd rotor group 13 is that the multi-rotor unmanned aerial vehicle 100 suspends
In ground/water surface so that the vacant state of multi-rotor unmanned aerial vehicle 100, multi-rotor unmanned aerial vehicle 100 can be eliminated and connect with ground/water surface
Touch the frictional force for producing, the resistance of motion for effectively reducing.Then, multi-rotor unmanned aerial vehicle 100 is in the first rotor group 11 and described
Moved along the direction parallel to ground/water surface in the presence of two rotor groups 12.Multi-rotor unmanned aerial vehicle of the invention 100 can be applicable
In the low-latitude flying of ground and the water surface.
It is understood that heretofore described rotating shaft forward direction meets right-hand rule.I.e. the right hand four refers to along spiral
During oar direction of rotation, it is positive that the signified direction of thumb is rotating shaft.
Specifically, the first rotor group 11 includes the first rotor 111 and the second rotor 112, the second rotor group 12
Including the 3rd rotor 121 and the 4th rotor 122, the 3rd rotor group 13 includes the 5th rotor 131 and the 6th rotor 132.The
One rotor 111 and the 3rd rotor 121 are divided into the both sides of the 5th rotor 131 and the place straight line of the 6th rotor 132 and in symmetrically setting
Put, the second rotor 112 and the 4th rotor 122 are symmetricly set in the both sides of the 5th rotor 131 and the place straight line of the 6th rotor 132.
That is, the first rotor group 12 is distributed relative to the 3rd rotor group 13 with the second rotor group 13 in mirror image.
Fig. 3 is please referred to, Fig. 3 is the structure diagram of the first implementation method of multi-rotor unmanned aerial vehicle 100 in Fig. 1, filled arrows in figure
The rotating shaft that direction is each rotor is positive.First rotor 111, second rotor 112, the 3rd rotor
121 and the 4th rotor 122 shaft parallel main casing 10 reference end face and with the plane of symmetry AA's ' of the main casing 10
Angle is acute angle, and the line of the 5th rotor 131 and the 6th rotor 132 is located on the plane of symmetry AA '.Described first
The positive deflection first direction X of the rotating shaft of rotor 111 and the 3rd rotor 121, second rotor 112 and the 4th rotor
The positive deflection second direction of 122 rotating shaft.The first direction is opposite with the second direction.First rotor 111 and described
Three rotors 121 can drive unmanned plane to be moved to first direction.Second rotor 112 and the 4th rotor 122 can drive
Dynamic unmanned plane is moved to second direction.5th rotor 131 is identical with the rotating shaft forward direction of the 6th rotor 132 and described
The rotating shaft of the 5th rotor 131 and the 6th rotor 132 is perpendicular to the end face plane of reference (vertical paper is outside in Fig. 3).Enter
One step is specifically, the rotating shaft forward direction of the 5th rotor 131 and the 6th rotor 132 should be perpendicular to the end face plane of reference
Upwards so that the multi-rotor unmanned aerial vehicle 100 is suspended in ground/water surface.
Further specifically, the main casing 10 is in positive six prismsby structure, six faceted pebbles 101 of the main casing 10 are successively
Set.First rotor 111 and second rotor 112 are divided on two adjacent faceted pebbles 101, and first rotor
The 111 positive rotating shaft forward direction with second rotor 112 of rotating shaft is located remotely from each other setting.3rd rotor 121 and described
Four rotors 122 are divided on two other adjacent faceted pebble 101 and the rotating shaft of the 3rd rotor 121 is positive with the 4th rotation
The rotating shaft forward direction of the wing 122 is located remotely from each other setting.5th rotor 131 and the 6th rotor 132 are divided into two other not
On adjacent faceted pebble 101.That is, the 5th rotor 131 and the 6th rotor 132 and first rotor 111, institute
The second rotor 112, the 3rd rotor 121 and the 4th rotor 122 is stated to belong on the different faceted pebbles 101.It is described
First rotor 111, second rotor 112, the 3rd rotor 121, the 4th rotor 122, the and of the 5th rotor 131
The rotating shaft of the 6th rotor 132 is each parallel to the faceted pebble 101 at place.
When unmanned plane works, the 5th rotor 131 and the 6th rotor 132 keep rotation so that multi-rotor unmanned aerial vehicle 100 is hanged
It is empty；When multi-rotor unmanned aerial vehicle 100 needs to be moved toward first direction, first rotor 111 and the 3rd rotor 121 revolve
Turn, second rotor 112 and the 4th rotor 122 stop motion (or counter motion, to change rotating shaft positive direction)；When
When unmanned plane needs the right side turning toward Fig. 2, second rotor 112 and the 3rd rotor 121 rotate, first rotor
121 and the 4th rotor 132 stop motion (or counter motion, to change rotating shaft positive direction).
It is understood that when unmanned plane needs to be moved toward second direction, the working method and first direction of each rotor
Motion is opposite.When unmanned plane needs the left side turning toward Fig. 2, right side turning phase in the working method and Fig. 2 of each rotor
Instead.In other embodiments, it is also possible to which all rotorshafts in Fig. 2 are rotated forward 180 °, its course of work also with it is above-mentioned
What the course of work was similar to, here is omitted.
Further specifically, first rotor 111, the 3rd rotor 121, second rotor 112, the described 4th
Rotor 122, the 5th rotor 131 and the 6th rotor 132 all be in regular hexagon structure, and the hexagon the length of side
Seamed edge with the six prisms bottom surface is long equal.So set and be advantageous in that, when multi-rotor unmanned aerial vehicle 100 needs to be converted into flying
During row mode, i.e., the rotor shaft direction of each rotor can be abutted between horizontal plane, now adjacent rotor, to enter
The stability of one step enhancing structure.
It is described further specifically, multi-rotor unmanned aerial vehicle 100 also includes the first magnetic medium 17 and the second magnetic medium 18
First magnetic medium 17, first rotor 111, second rotor are provided with each faceted pebble 101 of main casing 10
112nd, the 3rd rotor 121, the 4th rotor 122, the 5th rotor 131 and the 6th rotor 132 are provided with institute
State the second magnetic medium 18, first magnetic medium 17 attracts each other with second magnetic medium 18, with fix rotor with
Main casing 10.Slot 110, first rotor 111, second rotor 112, institute are additionally provided with the main casing faceted pebble 101
State and be respectively equipped with and institute on the 3rd rotor 121, the 4th rotor 122, the 5th rotor 131 and the 6th rotor 132
State the latch 118 that slot 110 is engaged.By the cooperation of latch 118 and slot 110, positioning function is realized.
Further specifically, the slot 110 is substantially in cross, that is to say, that the latch 118 is in cross.So
Design and be advantageous in that, the angle of rotor according to different demands, can be adjusted, realize plurality of flight.For example, can be by
The rotating shaft forward direction of all rotors is set upward, to realize the offline mode of unmanned plane.
Further specifically, multi-rotor unmanned aerial vehicle 100 also includes base 30, the base 30 includes top surface 31 and side wall
32, the top surface 31 and side wall 32 form hollow cavity 301, and the cavity 301 is in communication with the outside.That is, the bottom
Seat 30 is without bottom surface.The top surface 31 is provided with through hole 310 and mounting groove 311, the through hole 310 and the 5th rotor 131 and institute
State the 6th rotor 132 to connect, the main casing 10, first rotor 111, the 3rd rotor 121, second rotor
112nd, the 4th rotor 122, the 5th rotor 131 and the 6th rotor 132 are mounted on the mounting groove 311.
The effect of the base is, when the 5th rotor 131 and the 6th rotor 132 earthward/water surface be vented when, gas meeting
It is pressurized in the cavity 301 of base 30, so as to multi-rotor unmanned aerial vehicle 100 is hanging.
Further, in order to reach preferably pressurized effect.Preferably, the cavity 301 is parallel to the top surface 31
Area of section is incremented by by top surface along the vertical direction of the top surface 31.That is, the cross-sectional area at top surface 31 is minimum.This knot
The pressurized effect of structure is optimal.Preferably, the base 30 is made of elastomeric material, for example, rubber, elastoplast etc..It is preferred that
, the base can be made up of injection moulding or blow molding.The phase produced in mounting groove 311 is sticked into by by rotor
Thrust between mutually, base 30 and miscellaneous part are integrally fixed.Simultaneously this connected mode also allow for by base 30 from
Dismantled on miscellaneous part, to form different working modes.
It is understood that in other embodiment of the invention, can also be by by the 5th rotor 131 and described
The rotating shaft of six rotors 132 is positive to be pointed near the side of the side wall 32 of base 30.So that the 5th rotor 131 and the 6th rotation
The wing 132 extracts the gas in cavity 301 out.This implementation method can cause that multi-rotor unmanned aerial vehicle 100 is pasted wall and flown, specifically
, provide row by first rotor 111, the 3rd rotor 121, second rotor 112 and the 4th rotor 122
The power for entering, the 5th rotor 131 and the 6th rotor 132 are used to adsorb wall so that multi-rotor unmanned aerial vehicle 100 pastes wall
Flight.Control multi-rotor unmanned aerial vehicle can be reached by adjusting the rotating speed of the 5th rotor 131 and the 6th rotor 132
100 with the purpose in wall gap.
In the description of this specification, reference term " one embodiment ", " some embodiments ", " example ", " specifically show
The description of example " or " some examples " etc. means to combine specific features, structure, material or feature that the embodiment or example are described
It is contained at least one embodiment of the invention or example.In this manual, the schematic representation to above-mentioned term differs
Surely identical embodiment or example are referred to.And, the specific features of description, structure, material or feature can be any one
Combined in an appropriate manner in individual or multiple embodiments or example.
Embodiments described above, does not constitute the restriction to the technical scheme protection domain.It is any in above-mentioned implementation
Modification, equivalent and improvement made within the spirit and principle of mode etc., should be included in the protection model of the technical scheme
Within enclosing.
Claims (10)
1. a kind of multi-rotor unmanned aerial vehicle, it is characterised in that including main casing, the first rotor group, the second rotor group and the 3rd rotor
Group, the main casing includes two end face plane of references being oppositely arranged and the rib being connected between described two end face plane of references
Face, the first rotor group, the second rotor group and the 3rd rotor group are arranged on the faceted pebble, first rotor
Group is symmetrically distributed in the both sides of the 3rd rotor group, the first rotor group and second rotor with the second rotor group
The shaft parallel of rotor is in the end face plane of reference in group, and the first rotor group and the second rotor group are described for driving
, parallel to end face plane of reference direction motion, the rotating shaft of rotor is positive identical and vertical in the 3rd rotor group for unmanned plane
In the end face plane of reference.
2. multi-rotor unmanned aerial vehicle as claimed in claim 1, it is characterised in that the first rotor group includes the first rotor and the
Two rotors, the second rotor group includes the 3rd rotor and the 4th rotor, first rotor, second rotor, described the
The shaft parallel of three rotors and the 4th rotor is in the end face plane of reference, and first rotor and the 3rd rotor are relative
It is symmetrical arranged in the 3rd rotor group and for driving the unmanned plane to be moved towards first direction jointly, second rotor
It is used to drive the unmanned plane towards second direction movement, the first direction and the second party jointly with the 4th rotor
To conversely, the 3rd rotor group includes the 5th rotor and the 6th rotor, the rotating shaft of the 5th rotor and the 6th rotor
Forward direction is identical and perpendicular to the end face plane of reference.
3. multi-rotor unmanned aerial vehicle as claimed in claim 2, it is characterised in that the main casing is in positive six prismsby structure, described
First rotor and second rotor are divided on two adjacent faceted pebbles, and the 3rd rotor and the 4th rotor are divided into
On two other adjacent faceted pebble, the 5th rotor and the 6th rotor and first rotor, second rotor, institute
State the 3rd rotor and the 4th rotor belongs on the different faceted pebbles, it is first rotor, second rotor, described
The rotating shaft of the 3rd rotor, the 4th rotor, the 5th rotor and the 6th rotor is respectively parallel to corresponding described
Faceted pebble.
4. multi-rotor unmanned aerial vehicle as claimed in claim 3, it is characterised in that the rotating shaft of first rotor is positive with described
The rotating shaft forward direction of two rotors is located remotely from each other setting, the positive rotating shaft forward direction phase with the 4th rotor of rotating shaft of the 3rd rotor
Mutually it is arranged distant from.
5. multi-rotor unmanned aerial vehicle as claimed in claim 3, it is characterised in that first rotor, the 3rd rotor, described
Second rotor, the 4th rotor, the 5th rotor and the 6th rotor are in regular hexagon structure, the regular hexagon
The length of side it is long equal with the seamed edge of the six prisms bottom surface.
6. multi-rotor unmanned aerial vehicle as claimed in claim 2, it is characterised in that be also situated between including the first magnetic medium and the second magnetic
Matter, is provided with first magnetic medium, first rotor, second rotor, the described 3rd on the main casing faceted pebble
Rotor and the 4th rotor are provided with second magnetic medium, first magnetic medium and the second magnetic medium phase
Mutually attract, slot, first rotor, second rotor, the 3rd rotor and institute are additionally provided with the main casing faceted pebble
State and be respectively equipped with the latch being engaged with the slot on the 4th rotor.
7. multi-rotor unmanned aerial vehicle as claimed in claim 6, it is characterised in that the slot is in cross.
8. multi-rotor unmanned aerial vehicle as claimed in claim 2, it is characterised in that also including base, the base include top surface and
Side wall, the top surface and side wall form hollow cavity, and the cavity is in communication with the outside, and the top surface is provided with through hole and installation
Groove, the through hole is connected with the 5th rotor and the 6th rotor, the main casing, the first rotor group, described
Two rotor groups and the 3rd rotor group are installed on the mounting groove.
9. multi-rotor unmanned aerial vehicle as claimed in claim 8, it is characterised in that section face of the cavity parallel to the top surface
Product is incremented by by top surface along the vertical top surface direction.
10. multi-rotor unmanned aerial vehicle as claimed in claim 8, it is characterised in that the base is made up of elastomeric material.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/CN2016/082497 WO2017197603A1 (en) | 2016-05-18 | 2016-05-18 | Multi-rotor unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106794897A true CN106794897A (en) | 2017-05-31 |
| CN106794897B CN106794897B (en) | 2019-12-13 |
Family
ID=58952274
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201680002964.7A Active CN106794897B (en) | 2016-05-18 | 2016-05-18 | Multi-rotor unmanned aerial vehicle |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN106794897B (en) |
| WO (1) | WO2017197603A1 (en) |
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| CN110691190A (en) * | 2019-09-09 | 2020-01-14 | 苏州臻迪智能科技有限公司 | Switching method and device, unmanned aerial vehicle and readable storage medium |
| CN112124590A (en) * | 2020-10-15 | 2020-12-25 | 长沙中部翼天智能装备科技有限公司 | Strong crosswind interference resistant multi-rotor unmanned aerial vehicle |
| CN112319161A (en) * | 2020-08-31 | 2021-02-05 | 南京航空航天大学 | Rotor unmanned aerial vehicle capable of sailing underwater at high speed and control method thereof |
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| CN108394242A (en) * | 2018-05-15 | 2018-08-14 | 西南交通大学 | A kind of air-ground amphibious modularization robot |
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| CN112124590A (en) * | 2020-10-15 | 2020-12-25 | 长沙中部翼天智能装备科技有限公司 | Strong crosswind interference resistant multi-rotor unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
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| WO2017197603A1 (en) | 2017-11-23 |
| CN106794897B (en) | 2019-12-13 |
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