CN106218884A - The portable multi-rotor aerocraft of Spliced type - Google Patents
The portable multi-rotor aerocraft of Spliced type Download PDFInfo
- Publication number
- CN106218884A CN106218884A CN201610859349.XA CN201610859349A CN106218884A CN 106218884 A CN106218884 A CN 106218884A CN 201610859349 A CN201610859349 A CN 201610859349A CN 106218884 A CN106218884 A CN 106218884A
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- China
- Prior art keywords
- horn
- rotor
- hexagon
- helicitic texture
- rotor aerocraft
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Automatic Assembly (AREA)
Abstract
The invention discloses a kind of portable multi-rotor aerocraft of Spliced type, including fuselage, rotor driver；Described rotor driver is arranged on described fuselage by the cylindrical horn (4) of helicitic texture, and described fuselage is polygon in its floor projection, on described polygonal each angle, is fixedly installed hexagon horn (1)；The cylindrical horn (4) of described helicitic texture forms the connection of threaded engagement with the embedded screw thread (5) on hexagon horn (1).Technique scheme is used to provide the benefit that: to overcome existing multi-rotor aerocraft by fixing mechanism size and rotor number quantitative limitation；Multi-rotor aerocraft can require to adjust topology layout according to different aerial missions, thus is applicable to wider application scope.
Description
Technical field
The invention belongs to the technical field of miniature self-service aviation aircraft, relate to the improvement of multi-rotor aerocraft.More specifically
Ground, the present invention relates to a kind of portable multi-rotor aerocraft of Spliced type.
Background technology
Microminiature multi-rotor aerocraft is a kind of simple in construction, and maneuverability is the highest, can nobody of VTOL fly
Row device, is taking photo by plane, and searches and rescues, and transport aspect has wide application.
But, now widely used multi-rotor aerocraft, all use fixing rotor quantity, the one of fixed structure size
Change structure design.This integrated structure design, to multi-rotor aerocraft institute vehicle equipment and size and weight all have strictly
Restriction, therefore limit the scope of application of multi-rotor aerocraft.
Summary of the invention
The present invention provides a kind of portable multi-rotor aerocraft of Spliced type, its objective is to overcome the many rotors of existing microminiature to fly
The defect of row device integrated structure design.
To achieve these goals, the technical scheme that the present invention takes is:
The portable multi-rotor aerocraft of Spliced type of the present invention, including fuselage, rotor driver；Described rotor driver passes through
The cylindrical horn of helicitic texture is arranged on described fuselage；Described fuselage is polygon in its floor projection, in institute
On the polygonal each angle stated, it is fixedly installed hexagon horn；The cylindrical horn of described helicitic texture and hexagon machine
Embedded screw thread on arm forms the connection of threaded engagement.
The profile of described hexagon horn is six prisms；One section of setting on the cylindrical horn of described helicitic texture
Six prisms；The cross section of the two six prism is essentially equal；Arrive when the cylindrical horn of helicitic texture is arranged on hexagon horn
After Wei, end contact and the corresponding side of the two six prism are in same plane.
Described aircraft arranges hexagon shackle member, the shape inside it and hexagon horn and the circle of helicitic texture
Six prisms of cylindricality horn match；Described hexagon shackle member is cut open along its axis, is divided into two pieces；Six described prisms
Shape shackle member is fixing with the cylindrical horn of hexagon horn and helicitic texture respectively by screw to be connected.
Described polygon is octagon.
The quantity of described rotor driver is four, is uniformly distributed on four angles of octagon.
The quantity of described rotor driver is eight, is distributed on eight angles of octagon.
The present invention uses technique scheme to provide the benefit that: overcome existing multi-rotor aerocraft by fixing mechanism
Size and rotor number quantitative limitation；Multi-rotor aerocraft can require to adjust topology layout according to different aerial missions, thus
It is applicable to wider application scope.
Accompanying drawing explanation
In accompanying drawing content and figure, labelling is briefly described as follows:
Fig. 1 is the schematic diagram of four rotor assemblys of separate type multi-rotor aerocraft of the present invention composition；
Fig. 2 is the schematic diagram of eight rotor assemblys of separate type multi-rotor aerocraft of the present invention composition；
Fig. 3 is separate type multi-rotor aerocraft of the present invention single rotor system organigram；
Fig. 4 is the center fuselage schematic diagram of separate type multi-rotor aerocraft of the present invention；
Fig. 5 is the hexagonal metallic part i.e. schematic diagram of hexagon shackle member of the high intensity of the present invention.
Figure is labeled as:
1, hexagon horn, 2, four rotor systems, 3, eight rotor systems, 4, the cylindrical horn of helicitic texture, 5, embedded
Screw thread, 6, screw fixing hole, 7, hexagon shackle member.
Detailed description of the invention
Below against accompanying drawing, by the description to embodiment, the detailed description of the invention of the present invention is made further details of
Illustrate, to help those skilled in the art that inventive concept, the technical scheme of the present invention are had more complete, accurate and deep reason
Solve.
The structure of the present invention as shown in Figure 4, for a kind of portable multi-rotor aerocraft of Spliced type, fills including fuselage, rotor
Put；Described rotor driver is arranged on described fuselage by the cylindrical horn 4 of helicitic texture.
In order to overcome the defect of existing microminiature multi-rotor aerocraft integrated structure design, the present invention proposes a kind of employing
The microminiature multi-rotor aerocraft of separate type structure.It is made up of multiple single rotor subsystems and connecting plate, can be according to different
Aerial mission requires to be assembled into different rotor quantity, the multi-rotor aerocraft of different structure layout.
Specifically, the technical scheme is that:
As shown in Figures 1 to 5, the portable multi-rotor aerocraft of Spliced type of the present invention, described fuselage is thrown in its level
It is polygon on shadow, on described polygonal each angle, is fixedly installed hexagon horn 1；The circle of described helicitic texture
Cylindricality horn 4 and embedded screw thread 5 form the connection of threaded engagement.
The cylindrical horn 4 of helicitic texture and the hexagon horn of hexagon horn 1 collectively constitute splicing body.
Separate type multi-rotor aerocraft is by connecting plate, and the some single rotor subsystem composition being arranged on connecting plate；
The most each single rotor subsystem includes: rotor, motor, electron speed regulator, battery, control circuit；By control signal, can be real
The now independent control to each single rotor subsystem.
Several single rotor subsystems in connecting plate, form many rotors assembly by connection floor installation.Can be selected for not
It is arranged on the connecting plate of different sizes and shapes with single rotor subsystem of quantity, is assembled into many rotors of different structure layout
Aircraft, thus meet the requirement of different aerial mission.In flight course, by control signal, adjust each rotor respectively
The rotor rotating speed of subsystem, different rotor rotating speeds produces different rotor lifts and anti-twisted moment, thus realizes many rotors
The gesture stability of assembly.
The profile of described hexagon horn 1 is six prisms；One section on the cylindrical horn 4 of described helicitic texture sets
Put six prisms；The cross section of the two six prism is essentially equal；When the cylindrical horn 4 of helicitic texture is arranged on hexagon horn 1
On put in place after, the end contact of the two six prism and corresponding side are in same plane.
Described aircraft arranges hexagon shackle member 7, the shape inside it and hexagon horn 1 and helicitic texture
Six prisms of cylindrical horn 4 match；Described hexagon shackle member 7 is cut open along its axis, is divided into two pieces；Described six
Prismatic shackle member 7 is fixing with the cylindrical horn 4 of hexagon horn 1 and helicitic texture respectively by screw to be connected.
The hexagonal metallic part of high intensity i.e. hexagon shackle member 7 (Fig. 5) can be tightly fastened the cylinder of helicitic texture
Shape horn (4) and the hexagon horn of embedded screw thread (5), make motor be in level.
In installation process, the cylindrical horn 4 of helicitic texture is rotatably mounted to the hexagon horn 1 of embedded screw thread 5
On, rotate to combining closely, the hexagon on cylindrical horn 4 ensured at grade with each face of hexagon horn 1,
Finally the hexagonal metallic part of high intensity i.e. hexagon shackle member 7 (as shown in Figure 5) is fixed on cylindrical horn 4 and hexagonal
Between shape horn 1, by screw through screw fixing hole, it is allowed to fixing, completes Fast Installation.
Described polygon is octagon.
The quantity of described rotor driver is four, is uniformly distributed on four angles of octagon.
The quantity of described rotor driver is eight, is distributed on eight angles of octagon.
Four rotor systems (Fig. 1) or eight rotor systems (Fig. 2) can be quickly formed by splicing.
As depicted in figs. 1 and 2, the present invention includes four rotor system 2, eight rotor systems 3 respectively.According to demand, in flight
In set-up procedure, single rotor system (Fig. 3) is installed to center fuselage (Fig. 4), form four rotor systems (Fig. 1) or eight rotations
Wing system (Fig. 2).
In sum, the portable multi-rotor aerocraft of Spliced type of the present invention, the cylindrical horn 4 including helicitic texture revolves
Turn and be arranged on rapid deformation on the hexagon horn 1 of embedded screw thread 5, become four rotor systems (Fig. 2) or eight rotor systems (figure
3)；By ensureing that each face level hexagonal realizes the level of each motor, then screw fixing hole 6 installs screw, is allowed to more
Add secure rigid to connect.
Above in conjunction with accompanying drawing, the present invention is exemplarily described, it is clear that the present invention implements not by aforesaid way
Restriction, as long as have employed the method design of the present invention and the improvement of various unsubstantialities that technical scheme is carried out, or without changing
Enter and design and the technical scheme of the present invention are directly applied to other occasion, all within protection scope of the present invention.
Claims (6)
1. the portable multi-rotor aerocraft of Spliced type, including fuselage, rotor driver；Described rotor driver is by helicitic texture
Cylindrical horn (4) is arranged on described fuselage, it is characterised in that: described fuselage is polygon in its floor projection,
On described polygonal each angle, it is fixedly installed hexagon horn (1)；The cylindrical horn (4) of described helicitic texture
With the connection that the embedded screw thread (5) on hexagon horn (1) forms threaded engagement.
2. according to the portable multi-rotor aerocraft of the Spliced type described in claim 1, it is characterised in that: described hexagon horn
(1) profile is six prisms；One section on the cylindrical horn (4) of described helicitic texture arranges six prisms；The two six rib
The cross section of post is essentially equal；After the cylindrical horn (4) of helicitic texture is arranged on and puts in place on hexagon horn (1), the two
End contact and the corresponding side of six prisms are in same plane.
3. according to the portable multi-rotor aerocraft of the Spliced type described in claim 2, it is characterised in that: described aircraft is arranged
Hexagon shackle member (7), the shape inside it and hexagon horn (1) and six ribs of the cylindrical horn (4) of helicitic texture
Post matches；Described hexagon shackle member (7) is cut open along its axis, is divided into two pieces；Described hexagon shackle member (7)
Fixed with the cylindrical horn (4) of hexagon horn (1) and helicitic texture respectively by screw and be connected.
4. according to the portable multi-rotor aerocraft of the Spliced type described in claim 1, it is characterised in that: described polygon is just
Octagon.
5. according to the portable multi-rotor aerocraft of the Spliced type described in claim 4, it is characterised in that: described rotor driver
Quantity is four, is uniformly distributed on four angles of octagon.
6. according to the portable multi-rotor aerocraft of the Spliced type described in claim 4, it is characterised in that: described rotor driver
Quantity is eight, is distributed on eight angles of octagon.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610859349.XA CN106218884B (en) | 2016-09-28 | 2016-09-28 | The portable multi-rotor aerocraft of Spliced type |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610859349.XA CN106218884B (en) | 2016-09-28 | 2016-09-28 | The portable multi-rotor aerocraft of Spliced type |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106218884A true CN106218884A (en) | 2016-12-14 |
| CN106218884B CN106218884B (en) | 2019-01-18 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610859349.XA Active CN106218884B (en) | 2016-09-28 | 2016-09-28 | The portable multi-rotor aerocraft of Spliced type |
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| Country | Link |
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| CN (1) | CN106218884B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106828863A (en) * | 2017-03-28 | 2017-06-13 | 深圳市创客火科技有限公司 | The Multi-axis aircraft that can freely assemble |
| CN106927032A (en) * | 2017-03-29 | 2017-07-07 | 镇江顺宇飞行器有限公司 | A kind of combined type quadrotor |
| CN108928469A (en) * | 2018-06-26 | 2018-12-04 | 西华大学 | A kind of modularized combination type multi-rotor unmanned aerial vehicle |
| CN112644683A (en) * | 2021-01-18 | 2021-04-13 | 傅荣 | Unmanned aerial vehicle frame construction that can freely assemble |
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| CN104477399A (en) * | 2014-11-26 | 2015-04-01 | 马鞍山市靓马航空科技有限公司 | Multi-rotor unmanned aerial vehicle (UAV) for searching and rescuing at night |
| CN104494805A (en) * | 2014-11-08 | 2015-04-08 | 常州神鹰碳塑复合材料有限公司 | Carbon fiber multi-rotor unmanned aircraft fuselage and method for manufacturing the same |
| CN204279941U (en) * | 2014-11-28 | 2015-04-22 | 广州极飞电子科技有限公司 | A kind of multi-rotor aerocraft |
| CN104787319A (en) * | 2015-04-23 | 2015-07-22 | 张�杰 | Four-rotor aircraft provided with telescopic and foldable undercarriages |
| CN204623831U (en) * | 2015-04-23 | 2015-09-09 | 张�杰 | The portable quadrotor of rotor arm replaceable |
| CN106081108A (en) * | 2016-08-10 | 2016-11-09 | 成都蜀尚星科技有限公司 | A kind of Combined unmanned machine |
| CN206050066U (en) * | 2016-09-28 | 2017-03-29 | 安徽工程大学机电学院 | A kind of portable multi-rotor aerocraft of Spliced type |
-
2016
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Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
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| JP2001026295A (en) * | 1999-07-13 | 2001-01-30 | Homare Shoji:Kk | Flying hotel or similar sleeping accomodation |
| CN104494805A (en) * | 2014-11-08 | 2015-04-08 | 常州神鹰碳塑复合材料有限公司 | Carbon fiber multi-rotor unmanned aircraft fuselage and method for manufacturing the same |
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| CN104787319A (en) * | 2015-04-23 | 2015-07-22 | 张�杰 | Four-rotor aircraft provided with telescopic and foldable undercarriages |
| CN204623831U (en) * | 2015-04-23 | 2015-09-09 | 张�杰 | The portable quadrotor of rotor arm replaceable |
| CN106081108A (en) * | 2016-08-10 | 2016-11-09 | 成都蜀尚星科技有限公司 | A kind of Combined unmanned machine |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106828863A (en) * | 2017-03-28 | 2017-06-13 | 深圳市创客火科技有限公司 | The Multi-axis aircraft that can freely assemble |
| CN106927032A (en) * | 2017-03-29 | 2017-07-07 | 镇江顺宇飞行器有限公司 | A kind of combined type quadrotor |
| CN106927032B (en) * | 2017-03-29 | 2023-11-24 | 淮北暴风工业设计有限公司 | Combined four-rotor aircraft |
| CN108928469A (en) * | 2018-06-26 | 2018-12-04 | 西华大学 | A kind of modularized combination type multi-rotor unmanned aerial vehicle |
| CN112644683A (en) * | 2021-01-18 | 2021-04-13 | 傅荣 | Unmanned aerial vehicle frame construction that can freely assemble |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106218884B (en) | 2019-01-18 |
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Address after: No. 8, Wen Jin Xi Road, Yijiang District, Wuhu, Anhui Province Applicant after: Anhui Institute of Information Engineering Address before: No. 8, Wen Jin Xi Road, Yijiang District, Wuhu, Anhui Province Applicant before: ANHUI POLYTECHNIC UNIVERSITY, MECHANICAL & ELECTRICAL COLLEGE |
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Address after: 241100 No.1, Yonghe Road, Wanzhe District, Wuhu City, Anhui Province Patentee after: ANHUI INSTITUTE OF INFORMATION TECHNOLOGY Address before: No. 8, Wen Jin Xi Road, Yijiang District, Wuhu, Anhui Province Patentee before: ANHUI INSTITUTE OF INFORMATION TECHNOLOGY |