CN107000837A - It is a kind of can ground running unmanned plane - Google Patents
It is a kind of can ground running unmanned plane Download PDFInfo
- Publication number
- CN107000837A CN107000837A CN201680002968.5A CN201680002968A CN107000837A CN 107000837 A CN107000837 A CN 107000837A CN 201680002968 A CN201680002968 A CN 201680002968A CN 107000837 A CN107000837 A CN 107000837A
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- 230000001154 acute effect Effects 0.000 claims abstract description 4
- 230000033001 locomotion Effects 0.000 claims description 20
- 239000013536 elastomeric material Substances 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 210000003739 neck Anatomy 0.000 description 5
- 230000001737 promoting effect Effects 0.000 description 2
- 241000272517 Anseriformes Species 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 244000144992 flock Species 0.000 description 1
- -1 for example Substances 0.000 description 1
- 238000010102 injection blow moulding Methods 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000003319 supportive effect Effects 0.000 description 1
- 210000003813 thumb Anatomy 0.000 description 1
Classifications
-
- 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
- B64U10/16—Flying platforms with five or more distinct rotor axes, e.g. octocopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D57/00—Vehicles characterised by having other propulsion or other ground- engaging means than wheels or endless track, alone or in addition to wheels or endless track
- B62D57/04—Vehicles characterised by having other propulsion or other ground- engaging means than wheels or endless track, alone or in addition to wheels or endless track having other than ground-engaging propulsion means, e.g. having propellers
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
- Crushing And Pulverization Processes (AREA)
Abstract
It is a kind of can ground running unmanned plane, including main casing (11), first rotor group (12) and the second rotor group (13), the first rotor group (12) is installed on faceted pebble and is symmetrically distributed in the both sides of the plane of symmetry with the second rotor group (13), the first rotor group (12) includes the first rotor (121) and the second rotor (122), the second rotor group (13) includes the 3rd rotor (131) and the 4th rotor (132), first rotor (121), second rotor (122), the shaft parallel of 3rd rotor (131) and the 4th rotor (132) in the end face plane of reference and is acute angle with the angle of the plane of symmetry, first rotor (121) and the 3rd rotor (131) are used to drive the unmanned plane to move towards first direction jointly, second rotor (122) and the 4th rotor (132) are used to drive the unmanned plane to move towards second direction jointly.Unmanned function realizes the function of ground running, strengthens the suitable environment of unmanned plane, improves the performance of unmanned plane.
Description
Technical field
The application is related to unmanned air vehicle technique field, more particularly to it is a kind of can ground running unmanned plane.
Background technology
With the continuous progress of scientific and technological society, the growth of unmanned plane industry progressively, multi-rotor unmanned aerial vehicle is due to machinery
Simple in construction, dynamical system is simple, can have developed rapidly the advantages of VTOL, a time researcher goes after like a flock of ducks, and opens one after another
The research of beginning multi-rotor unmanned aerial vehicle is used, and has one in global range by the commercialized upsurge of many rotors.
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 it is current it is air-ground integrated nobody
The research of machine is then less, therefore is difficult to meet increasingly complicated use environment requirement.
The content of the invention
The purpose of the application be provide it is a kind of can ground running unmanned plane, realize the amphibious work(in the vacant lot of unmanned plane
Energy.
To achieve the above object, the application provides following technical scheme：
The present invention provide it is a kind of can ground running unmanned plane, including main casing, the first rotor group and the second rotor group, institute
State that main casing is symmetrical along the plane of symmetry, the main casing includes two end face plane of references being oppositely arranged and is connected to described two ends
Faceted pebble between the plane of reference of face, the first rotor group is installed on the faceted pebble and is symmetrically distributed in institute with the second rotor group
The both sides of the plane of symmetry are stated, the first rotor group includes the first rotor and the second rotor, and the second rotor group includes the 3rd rotation
The wing and the 4th rotor, first rotor, second rotor, the 3rd rotor and the 4th rotor shaft parallel in
The end face plane of reference and be acute angle with the angle of the plane of symmetry, first rotor and the 3rd rotor are used for common band
Move the unmanned plane to move towards first direction, second rotor and the 4th rotor are used to drive the unmanned plane jointly
Towards second direction movement, the first direction and the second direction are opposite.
Wherein, the main casing is in positive six prismsby structure, and first rotor and the 3rd rotor are divided into two phases
On adjacent faceted pebble, second rotor and the 4th rotor are divided on two other adjacent faceted pebble, first rotor,
The rotating shaft of second rotor, the 3rd rotor and the 4th rotor is respectively parallel to the corresponding faceted pebble.
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, first rotor,
The rotating shaft of second rotor, the 3rd rotor and the 4th rotor is respectively parallel to the corresponding faceted pebble.
Wherein, in addition to the 5th rotor and the 6th rotor, the 5th rotor and the 6th rotor and the described first rotation
The wing, second rotor, the 3rd rotor and the 4th rotor belong on the different faceted pebbles, the 5th rotor
Positive towards identical with the rotating shaft of the 6th rotor, the shaft parallel of the 5th rotor and the 6th rotor is in corresponding
The faceted pebble and parallel to the main casing end face plane of reference.
Wherein, first rotor, the 3rd rotor, second rotor, the 4th rotor, the 5th rotor
It is in regular hexagon structure with the 6th rotor, the length of side of the hexagon is equal with the seamed edge length of the six prisms bottom surface.
Wherein, in addition to the first magnetic medium and the second magnetic medium, it is provided with described first on the main casing faceted pebble
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 and matches with the slot on first rotor, second rotor, the 3rd rotor and the 4th rotor
The latch of conjunction.
Wherein, the slot is in cross.
Wherein, in addition to base, neck and motion, the first rotor group and described are provided with the base
Two rotor groups are fixed in the neck.
Wherein, the base is made up of elastomeric material.
Wherein, the motion is universal wheel or spherical point contacts.
The unmanned plane of the application is real by dividing into the method that motion is provided with bottom set seat, base in Power Component
Function of the unmanned plane in ground running is showed, has strengthened the suitable environment of unmanned plane, improve the performance of unmanned plane.
Brief description of the drawings
, below will be to institute in embodiment in order to illustrate more clearly of the embodiment of the present application or technical scheme of the prior art
The accompanying drawing needed to use is briefly described, it should be apparent that, drawings in the following description are only some implementations of the application
Example, for those of ordinary skill in the art, on the premise of not paying creative work, can also be obtained according to these accompanying drawings
Obtain other accompanying drawings.
Fig. 1 be the application the first embodiment can ground running unmanned plane decomposing schematic representation.
Fig. 2 be shown in Fig. 1 can ground running unmanned plane structure diagram.
Fig. 3 for second of embodiment of the application provide can ground running unmanned plane structure diagram.
Fig. 4 for the application the third embodiment provide can ground running unmanned plane structure diagram.
Fig. 5 for the 4th kind of embodiment of the application provide can ground running unmanned plane structure diagram.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present application, the technical scheme in the embodiment of the present application is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only some embodiments of the present application, rather than whole embodiments.It is based on
Embodiment in the application, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of the application protection.
Ordinal determinative employed in the application following examples, first, second grade are merely to clearly demonstrate this
The distinctive term of similar feature in application, putting in order or using order for corresponding feature is not represented.
Referring to Fig. 1, the present invention can the unmanned plane of ground running include：Power Component 10 and base 20.The power
Component 10 includes main casing 11, the first rotor group 12 and the second rotor group 13, what the main casing 11 was oppositely arranged including two
The end face plane of reference and the faceted pebble for connecting described two end face plane of references, the main casing 11 are symmetrical structure, the main casing 11
The plane of symmetry (AA ' in such as Fig. 2) perpendicular to the end face.Here the end face plane of reference refer to the two ends of main casing 11 perpendicular to
The section of the faceted pebble.The first rotor group 12 is installed on the faceted pebble of the main casing 11 with the second rotor group 13.
The first rotor group 12 includes the first rotor 121 and the second rotor 122, and the second rotor group 13 includes the 3rd rotor 131
With the 4th rotor 132.First rotor 121 and the 3rd rotor 131 are set relative to the main casing 11 in mirror image, the second rotor
122 and the 4th rotor 132 relative to the main casing 11 in mirror image set.That is, the first rotor group 12 with it is described
Second rotor group 13 is symmetric relative to the plane of symmetry of the main casing 11.Please refer to Fig. 2, Fig. 2 is can ground in Fig. 1
Filled arrows direction is the rotating shaft of each rotor in the structure diagram of the first embodiment of the unmanned plane of face walking, figure
It is positive.First rotor 121, second rotor 122, the rotating shaft of the 3rd rotor 131 and the 4th rotor 132 are put down
The end face of row main casing 11 and be acute angle with the angle of the plane of symmetry AA ', first rotor 121 and the 3rd rotor
131 rotating shaft forward direction deviation first direction X, the rotating shaft forward direction deviation second of second rotor 122 and the 4th rotor 132
Direction.The first direction is opposite with the second direction.It is understood that heretofore described rotating shaft forward direction meets right
Hand corkscrew rule.When i.e. the right hand four is referred to along propeller direction of rotation, the signified direction of thumb is that rotating shaft is positive.First rotor
121 and the 3rd rotor 131 unmanned plane can be driven to be moved to first direction.Second rotor 122 and the 4th rotation
The wing 132 can drive unmanned plane to be moved to second direction.The Power Component 10 is installed on the base 20, the base 20
On be provided with motion 21.Can the unmanned plane of ground running placed on the ground by base 20, in the drive of Power Component 10
Under dynamic, it can walk on the ground.
Further specifically, the main casing 11 is in positive six prismsby structure, six faceted pebbles of the main casing 11 are set successively
Put.First rotor 121 and the 3rd rotor 131 are divided on two adjacent faceted pebbles, second rotor 122 and institute
The 4th rotor 132 is stated to be divided on two other adjacent faceted pebble.Fig. 2 is please referred to, each rotor is each secured to one
On faceted pebble, the rotorshaft of the faceted pebble is fixed on each parallel to the faceted pebble.It is described when unmanned plane is needed toward during first direction motion
First rotor 121 and the 3rd rotor 131 rotate, second rotor 122 and the stop motion of the 4th rotor 132 (or
Person's counter motion, to change rotating shaft positive direction)；When unmanned plane needs the right side turning into Fig. 2, the He of the second rotor 122
3rd rotor 131 rotates, first rotor 121 and the stop motion of the 4th rotor 132 (or counter motion, with
Change rotating shaft positive direction).
It is understood that working as unmanned plane needs to move toward second direction or is turned constantly toward left side in Fig. 2, each rotor
Working method it is contrary to the above.In other embodiments, all rotorshafts in Fig. 2 can also be rotated forward 180 °,
Its course of work is also similar with the above-mentioned course of work, and here is omitted.
Further, can ground running unmanned plane also include the 5th rotor 15 and the 6th rotor 16, the 5th rotor
15 and the 6th rotor 16 set up separately and be placed on the main casing 11 remaining two and be not provided with the faceted pebble of rotor.Namely
Say, the 5th rotor 15 and the 6th rotor 16 and first rotor 121, second rotor 122, the 3rd rotation
The wing 131 and the 4th rotor 132 belong on different faceted pebbles, the rotating shaft of the 5th rotor 15 and the 6th rotor 16
Positive identical, the shaft parallel of the 5th rotor 15 and the 6th rotor 16 is in corresponding faceted pebble and parallel to main casing 11
End face face.The rotating shaft of 5th rotor 15 and the 6th rotor 16 described in Fig. 2 is positive towards first direction, can ground for promoting
The unmanned plane of face walking is moved to first direction.When the positive court of the rotating shaft for changing the 5th rotor 15 and the 6th rotor 16
To, when making it towards second direction, can be used for promoting can the unmanned plane of ground running moved to second direction.
Further specifically, first rotor 121, the 3rd rotor 131, second rotor 122, the described 4th
Rotor 132, the 5th rotor 15 and the 6th rotor 16 all be in regular hexagon structure, and the length of side of the hexagon with
The seamed edge length of the six prisms bottom surface is equal.So set and be advantageous in that, when can ground running unmanned plane need be converted into
During offline mode, i.e., the rotor shaft direction of each rotor can be abutted between horizontal plane, now adjacent rotor, with
The stability of enhancing structure.
Further specifically, can ground running unmanned plane also include the first magnetic medium 17 and the second magnetic medium 18,
First magnetic medium 17, first rotor 121, second rotor are provided with each faceted pebble of the main casing 11
122nd, the 3rd rotor 131, the 4th rotor 132, the 5th rotor 15 and the 6th rotor 16 are provided with described
Second magnetic medium 18, first magnetic medium 17 attracts each other with second magnetic medium 18, to fix rotor and master
Housing 11.Slot 110, first rotor 121, second rotor 122, the described 3rd are additionally provided with the main casing faceted pebble
It is respectively equipped with and the slot 110 on rotor 131, the 4th rotor 132, the 5th rotor 15 and the 6th rotor 16
The latch 111 being engaged.By the cooperation of latch 111 and slot 110, positioning function is realized.
Further specifically, the slot 110 is substantially in cross, that is to say, that the latch 111 is in cross.So
Design is advantageous in that, according to different demands, can adjust the angle of rotor system 20, realize plurality of flight.For example,
The rotating shaft forward direction of all rotors can upward be set, to realize the offline mode of unmanned plane.
Further specifically, being provided with six necks 201 on the base 20, first rotor 121, the 3rd rotation
The wing 131, second rotor 122, the 4th rotor 132, the 5th rotor 15 and the 6th rotor 16 are all fixed on
In the neck 201.The base 20 is made up of elastomeric material, for example, rubber, elastoplast etc..It is preferred that, the base
20 can be made up of injection molding or blow molding, and certain intensity that base has plays support and protective effect.By inciting somebody to action
Rotor sticks into the thrust each other produced in neck 201, and Power Component 10 is integrally fixed with base 20.While this
Plant connected mode to also allow for dismantling base 20 from host component 10, to form different working modes.On the base 20
Motion 21 can be universal wheel or spherical point contacts.
Referring to Fig. 3, Fig. 3 for can ground running second of embodiment of unmanned plane structure diagram, solid arrow in figure
Head direction is that the rotating shaft of each rotor is positive, and each rotor is each secured on a faceted pebble.Specifically, described first
Rotor 121 and second rotor 122 are divided on two adjacent faceted pebbles, the 3rd rotor 131 and the 4th rotor
132 are divided on two other adjacent faceted pebble, are fixed on the rotorshaft of the faceted pebble each parallel to the faceted pebble.When unmanned plane is needed
Will be toward during first direction motion, first rotor 121 and the 3rd rotor 131 rotate, second rotor 122 and described
The stop motion of 4th rotor 132 (or counter motion, to change rotating shaft positive direction)；When unmanned plane needs the right side into Fig. 3 to turn
When curved, first rotor 121 and the 4th rotor 132 rotate, and second rotor 122 and the 3rd rotor 131 stop
Only move (or counter motion, to change rotating shaft positive direction).It is understood that when unmanned plane is needed toward second direction motion
Or turned constantly toward left side in Fig. 3, the working method of each rotor is contrary to the above.In other embodiments, can also be by Fig. 2
In all rotorshafts rotate forward 180 °, its course of work is also similar with the above-mentioned course of work, here is omitted.
Further, can ground running unmanned plane also include the 5th rotor 15 and the 6th rotor 16, the 5th rotor
15 and the 6th rotor 16 set up separately and be placed on the main casing 11 remaining two and be not provided with the faceted pebble of rotor, the described 5th
Rotor 15 is identical with the rotating shaft forward direction of the 6th rotor 16, the shaft parallel of the 5th rotor 15 and the 6th rotor 16
In corresponding faceted pebble and parallel to horizontal plane.The positive direction of the rotating shaft of 5th rotor 15 and the 6th rotor 16 described in Fig. 3
Vertical first direction, for promote can the unmanned plane of ground running moved to vertical first direction.
It is understood that being detachably connected due to being used between the rotor and main case 11 of the present invention.And hence it is also possible to
There is the motor pattern of the third embodiment as shown in Figure 4 and the 4th kind of embodiment shown in Fig. 5.Motion shown in Fig. 4
Pattern can realize that rotating in place either spiral advances.Fig. 5 motor pattern can be realized quickly to be moved to a direction.
The embodiment of the present application is described in detail above, specific case used herein to the principle of the application and
Embodiment is set forth, and the explanation of above example is only intended to help and understands the present processes and its core concept；
Simultaneously for those of ordinary skill in the art, according to the thought of the application, can in specific embodiments and applications
There is change part, in summary, this specification content should not be construed as the limitation to the application.
Claims (10)
1. it is a kind of can ground running unmanned plane, it is characterised in that including main casing, the first rotor group and the second rotor group, institute
State that main casing is symmetrical along the plane of symmetry, the main casing includes two end face plane of references being oppositely arranged and is connected to described two ends
Faceted pebble between the plane of reference of face, the first rotor group is installed on the faceted pebble and is symmetrically distributed in institute with the second rotor group
The both sides of the plane of symmetry are stated, the first rotor group includes the first rotor and the second rotor, and the second rotor group includes the 3rd rotation
The wing and the 4th rotor, first rotor, second rotor, the 3rd rotor and the 4th rotor shaft parallel in
The end face plane of reference and be acute angle with the angle of the plane of symmetry, first rotor and the 3rd rotor are used for common band
Move the unmanned plane to move towards first direction, second rotor and the 4th rotor are used to drive the unmanned plane jointly
Towards second direction movement, the first direction and the second direction are opposite.
2. as claimed in claim 1 can ground running unmanned plane, it is characterised in that the main casing be in positive six prismsby knot
Structure, first rotor and the 3rd rotor are divided on two adjacent faceted pebbles, second rotor and the 4th rotation
The wing is divided on two other adjacent faceted pebble, first rotor, second rotor, the 3rd rotor and the described 4th
The rotating shaft of rotor is respectively parallel to the corresponding faceted pebble.
3. as claimed in claim 1 can ground running unmanned plane, it is characterised in that the main casing be in positive six prismsby knot
Structure, first rotor and second rotor are divided on two adjacent faceted pebbles, the 3rd rotor and the 4th rotation
The wing is divided on two other adjacent faceted pebble, first rotor, second rotor, the 3rd rotor and the described 4th
The rotating shaft of rotor is respectively parallel to the corresponding faceted pebble.
4. as claimed in claim 2 or claim 3 can ground running unmanned plane, it is characterised in that also including the 5th rotor and the 6th
Rotor, the 5th rotor and the 6th rotor and first rotor, second rotor, the 3rd rotor and described
4th rotor belongs on the different faceted pebbles, and the rotating shaft of the 5th rotor and the 6th rotor is positive towards identical,
The shaft parallel of 5th rotor and the 6th rotor is in the corresponding faceted pebble and parallel to the main casing end face plane of reference.
5. as claimed in claim 4 can ground running unmanned plane, it is characterised in that first rotor, it is described 3rd rotation
The wing, second rotor, the 4th rotor, the 5th rotor and the 6th rotor are in regular hexagon structure, described six
The length of side of side shape is equal with the seamed edge length of the six prisms bottom surface.
6. as claimed in claim 1 can ground running unmanned plane, it is characterised in that also including the first magnetic medium and second
First magnetic medium, first rotor, second rotor, institute are provided with magnetic medium, the main casing faceted pebble
State the 3rd rotor and the 4th rotor is provided with second magnetic medium, first magnetic medium and second magnetic
Medium is attracted each other, and slot, first rotor, second rotor, the 3rd rotation are additionally provided with the main casing faceted pebble
The latch being engaged with the slot is respectively equipped with the wing and the 4th rotor.
7. as claimed in claim 6 can ground running unmanned plane, it is characterised in that the slot be in cross.
8. as claimed in claim 1 can ground running unmanned plane, it is characterised in that also including base, set on the base
Neck and motion are equipped with, the first rotor group and the second rotor group are fixed in the neck.
9. as claimed in claim 8 can ground running unmanned plane, it is characterised in that the base is made up of elastomeric material.
10. as claimed in claim 8 can ground running unmanned plane, it is characterised in that the motion be universal wheel or
Spherical point contacts.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/CN2016/082495 WO2017197601A1 (en) | 2016-05-18 | 2016-05-18 | Unmanned aerial vehicle capable of walking on ground |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107000837A true CN107000837A (en) | 2017-08-01 |
| CN107000837B CN107000837B (en) | 2020-10-13 |
Family
ID=59431737
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201680002968.5A Active CN107000837B (en) | 2016-05-18 | 2016-05-18 | Unmanned aerial vehicle capable of walking on ground |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN107000837B (en) |
| WO (1) | WO2017197601A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110641698A (en) * | 2019-10-06 | 2020-01-03 | 谌薏冰 | Multifunctional flying robot |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113148133A (en) * | 2021-04-02 | 2021-07-23 | 泉州中国兵器装备集团特种机器人研发中心 | Improved generation air-land dual-purpose four rotor unmanned aerial vehicle |
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| CN104608923A (en) * | 2015-01-31 | 2015-05-13 | 中南大学 | Honeycomb-type six-rotor transport aircraft |
| CN205632720U (en) * | 2016-05-18 | 2016-10-12 | 深圳市创客工场科技有限公司 | But unmanned aerial vehicle of ground walking |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110641698A (en) * | 2019-10-06 | 2020-01-03 | 谌薏冰 | Multifunctional flying robot |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2017197601A1 (en) | 2017-11-23 |
| CN107000837B (en) | 2020-10-13 |
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