CN106827992A - Land and air double-used six rotorcraft device - Google Patents
Land and air double-used six rotorcraft device Download PDFInfo
- Publication number
- CN106827992A CN106827992A CN201710132521.6A CN201710132521A CN106827992A CN 106827992 A CN106827992 A CN 106827992A CN 201710132521 A CN201710132521 A CN 201710132521A CN 106827992 A CN106827992 A CN 106827992A
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- CN
- China
- Prior art keywords
- rotorcraft
- land
- athey wheel
- trapezoid support
- air double
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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
- 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
Abstract
The invention discloses a kind of land and air double-used six rotorcraft device, it includes six rotorcraft flight instruments and trapezoidal creeper undercarriage；Including rotation oar brushless electric machine etc., the output shaft of the rotation oar brushless electric machine is fixedly connected and is positioned in six shaft end motor cabinets of six rotorcraft the six rotorcraft flight instruments with a propeller；The brushless control panel is positioned over the center of aircraft frame, and is fixed brushless control panel by six rotations of drops tight locking button；Including trapezoid support etc., trapezoid support is connected the trapezoidal creeper undercarriage of six rotorcraft by a cylindric connecting rod with aircraft frame bottom；The Athey wheel is fixed in the race of each endpoint location of trapezoid support by axle；The crawler belt and an Athey wheel cooperatively form land walking device；Aircraft provided by the present invention has simple structure, easy to operate, is relatively easy to complete various aerial and land operations.
Description
Technical field
The present invention relates to a kind of aircraft device, more particularly to a kind of land and air double-used six rotorcraft device.
Background technology
First unmanned plane made a successful trial flight in 1933 in the world, had opened the prelude of unmanned plane；With domestic and international science and technology
Development continuous progress, in recent years in civil area, unmanned air vehicle technique the disaster relief, take photo by plane, agricultural, investigation every field in obtain
Extensive concern and research；Afield, unmanned plane avoids casualties due to it, possesses execution task ability higher
Feature, has obtained substantial amounts of application；Many rotor type unmanned planes are due to excellent mobility, simple mechanical structure, side
Just the characteristics of deployment is with safeguarding, has obtained many applications；Research outside Now Domestic just to six rotorcraft is all located
In quick developing stage；In recent years, with nanosecond science and technology and manufacturing fast development, new material, micro electronmechanical (MEMS), micro-
The progress of the technology such as inertial navigation (MIMU) and flight control, the research of six rotorcraft is sent out towards more and more practical road
Exhibition, has turned into the hot fields of industry research concern at present；Six rotorcraft be adapted to it is near the ground it is middle perform monitoring, investigation,
The task such as take photo by plane, with extensive military and civilian prospect.
At present, due to the difference of aircraft type, produced expense is also different；For example shake big also with helicopter aerial photography
Need Ground take off with land, large-scale fixed wing aircraft carries out very flexible of taking photo by plane, visual angle is small, in addition it is also necessary to runway rise
Expense needed for the winged both the above aircraft with landing is more than hundred times of telecontrolled aircraft, and formality is complicated；And six rotor flyings
Device can meet small area ground can realize vertical lift, and without formality；Six rotorcraft installs upper trapezoid crawler belt land additional
The good flying quality that ground walking mechanism matches somebody with somebody the six rotorcraft flight instruments that closes is to realize the ability of land operation；And it is existing
Technology in land and air double-used aircraft there is the defect problem that airflight is dumb, road surface running gear is not perfect etc. enough；
The land and air double-used six rotorcraft, can also rise to the sky when barrier is run into, easily leap, and headstock is provided with high-definition camera
Head, records its various Wonderland Travels；Research and develop one kind and possess larger road surface earth-grasping force, empty two necks in energy flexible approach land in this area
The six rotorcraft of domain task.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of land and air double-used six rotorcraft device, and it possesses larger
Land face walking earth-grasping force, can flexible approach land Kong Liangge fields task.
The present invention is to solve above-mentioned technical problem by following technical proposals：A kind of land and air double-used six rotorcraft
Device, it is characterised in that it includes six rotorcraft flight instruments and trapezoidal creeper undercarriage；
The six rotorcraft flight instruments includes rotation oar brushless electric machine, aircraft frame, brushless control panel, described
The output shaft for revolving oar brushless electric machine is fixedly connected with a propeller and is positioned over six shaft end motor cabinets of six rotorcraft
In；The brushless control panel is positioned over the center of aircraft frame, and will by six rotations of drops tight locking button
Brushless control panel is fixed；
The trapezoidal creeper undercarriage of six rotorcraft includes trapezoid support, crawler belt, Athey wheel, crawler belt wheel drive electricity
Machine and lithium battery, trapezoid support are connected by a cylindric connecting rod with aircraft frame bottom；The Athey wheel leads to
Axle is crossed to be fixed in the race of each endpoint location of trapezoid support；The crawler belt cooperatively forms land walking dress with Athey wheel
Put；
The output shaft of the Athey wheel motor is fixedly connected with an Athey wheel and is fixed on by motor casing trapezoidal
The inner side on support base；The lithium battery is positioned in the five of trapezoid support base battery cases.
Preferably, the aircraft frame, trapezoid support and Athey wheel select ABS type 3D printing materials.
Preferably, the rotation oar brushless electric machine from a diameter of 10mm, length 35mm, the diameter of axle be 2.0mm, rotating speed be 5W with
On brshless DC motor.
Preferably, the airscrew diameter selects 50mm.
Preferably, the bottom edge lengths of the trapezoid support are 160mm, a length of 100mm such as trapezoidal two waist, and bottom with
The angle of waist is 135 °.
Preferably, a diameter of 18mm of Athey wheel of the trapezoidal creeper undercarriage, and be placed on trapezoid support and respectively hold
U-shaped race in.
Preferably, the Athey wheel of lower end two is driving wheel in the trapezoidal creeper undercarriage, by crawler belt wheel drive electricity
Machine drives, and Athey wheel motor is fixed on trapezoid support base Inner Front End by motor casing.
Preferably, the aircraft frame and trapezoid support periphery are all rounding corner structure.
Positive effect of the invention is：The present invention is connected to coordinate by mechanical structure and realized with motor rotation driving
The airflight pattern and land walking pattern of six rotorcraft so that six rotorcraft is with good airflight
Also there is the ability for performing land walking simultaneously in the case of performance, six rotors in the prior art are solved to a certain extent and is flown
Some existed when complex environment task is performed of going can not process the problem of road barrier；Aircraft provided by the present invention is also
There is simple structure, easy to operate, be relatively easy to complete various aerial and land operations.
Brief description of the drawings
Fig. 1 is the structural representation of land and air double-used six rotorcraft of the invention.
Fig. 2 is land and air double-used six rotorcraft flight instruments structural representation of the invention.
Fig. 3 is the structural representation of trapezoidal creeper undercarriage of the invention.
Fig. 4 is the part-structure schematic diagram of trapezoidal creeper undercarriage of the invention.
Specific embodiment
Present pre-ferred embodiments are given below in conjunction with the accompanying drawings, to describe technical scheme in detail.
As shown in figure 1, the present invention provides a kind of land and air double-used six rotorcraft, including six rotorcraft flight instruments
1 and trapezoidal creeper undercarriage 2.
As shown in Fig. 2 the six rotorcraft flight instruments 1 includes rotation oar brushless electric machine 11, aircraft frame 13, nothing
Brush control panel 14, the output shaft of the rotation oar brushless electric machine 11 is fixedly connected with a propeller 12 and is positioned over six rotors and flies
In six shaft end motor cabinets of row device；The brushless control panel 14 is positioned over the center of aircraft frame 13, and passes through
Brushless control panel 14 is fixed in six rotations of drops tight locking button 15；
As shown in figure 3, the trapezoidal creeper undercarriage 2 includes trapezoid support 18, crawler belt and Athey wheel 20, trapezoid support
18 are connected by a cylindric connecting rod 21 with the bottom of aircraft frame 13；The Athey wheel 20 is fixed on ladder by axle
In the race of each endpoint location of shape support 18；The crawler belt 19 cooperatively forms land walking device with Athey wheel 20；
As shown in Figure 4；The trapezoidal creeper undercarriage 2 also includes Athey wheel motor 16 and lithium battery 17, described
The output shaft of Athey wheel motor 16 is fixedly connected with an Athey wheel 20 and is fixed on trapezoid support by a motor casing
The inner side on 18 bases；The lithium battery 17 is positioned in five battery cases 22 on the base of trapezoid support 18.
Used as a kind of preferred scheme, (ABS is from ABS for the aircraft frame 13, trapezoid support 18 and Athey wheel 20
Acrylonitrile, butadiene, the synthetic plastic acrylonitrile of styrene, butadiene, the graft copolymerization product of three kinds of monomers of styrene) type
3D printing material, so improves intensity.
Used as a kind of preferred scheme, the rotation oar brushless electric machine 11 is from a diameter of 10mm, length 35mm, the diameter of axle
2.0mm, rotating speed are the brshless DC motor of more than 5W, and such reduces cost increases the service life.
Used as a kind of preferred scheme, the diameter of the propeller 12 selects 50mm, such reduces cost.
As a kind of preferred scheme,
Used as a kind of preferred scheme, in the trapezoid support 18, the bottom edge lengths of trapezoid support are 160mm, trapezoidal two
A length of 100mm such as waist, and bottom and the angle of waist are 135 °, such reduces cost.
As a kind of preferred scheme, a diameter of 18mm of Athey wheel 20 of the trapezoidal creeper undercarriage 2, and it is placed on ladder
It is so easy to use on shape support 18 in the U-shaped race at each end, prevent from removing.
Used as a kind of preferred scheme, the Athey wheel 20 of lower end two is driving wheel in the trapezoidal creeper undercarriage 2, is passed through
Athey wheel motor 16 drives, and Athey wheel motor 16 is fixed on the base Inner Front End of trapezoid support 18 by motor casing, this
Sample prescription just drives.
Used as a kind of preferred scheme, the bottom of the trapezoid support 18 is provided with five battery cases 22, the power of whole device
Source is the lithium battery 17 in five battery cases 22.
Used as a kind of preferred scheme, the six rotorcraft frame periphery is all rounding corner structure, specifically described
Aircraft frame 13 and the periphery of trapezoid support 18 are all rounding corner structure, so prevent from breaking.
The present invention is connected by mechanical structure and matched somebody with somebody by ingenious utilization six rotorcraft and the advantage of creeper undercarriage
The airflight pattern and land walking pattern of six rotorcraft are realized in conjunction with motor rotation driving so that six rotorcraft
Also there is the ability for performing land walking simultaneously in the case of with good airflight performance, solve to a certain extent
In the prior art six rotor flyings exist when complex environment task is performed some can not process the problem of road barrier.Separately
Outward, aircraft provided by the present invention also has simple structure, easy to operate, can be relatively easy to complete various aerial and land
The advantage of operation.Six drops retaining mechanisms can be fixed control panel with 360 ° of rotations to brushless control panel top.
Particular embodiments described above, technical problem, technical scheme and beneficial effect to solution of the invention are carried out
Further describe, should be understood that and the foregoing is only specific embodiment of the invention, be not limited to
The present invention, all any modification, equivalent substitution and improvements within the spirit and principles in the present invention, done etc., should be included in this
Within the protection domain of invention.
Claims (8)
1. a kind of land and air double-used six rotorcraft device, it is characterised in that it includes six rotorcraft flight instruments and ladder
Shape creeper undercarriage；
The six rotorcraft flight instruments includes rotation oar brushless electric machine, aircraft frame, brushless control panel, the rotation oar
The output shaft of brushless electric machine is fixedly connected and is positioned in six shaft end motor cabinets of six rotorcraft with a propeller；Institute
State the center that brushless control panel is positioned over aircraft frame, and by six rotations of drops tight locking button by brushless control
Panel processed is fixed；
The trapezoidal creeper undercarriage of six rotorcraft include trapezoid support, crawler belt, Athey wheel, Athey wheel motor and
Lithium battery, trapezoid support is connected by a cylindric connecting rod with aircraft frame bottom；The Athey wheel passes through axle
It is fixed in the race of each endpoint location of trapezoid support；The crawler belt cooperatively forms land walking device with Athey wheel；
The output shaft of the Athey wheel motor is fixedly connected with an Athey wheel and is fixed on trapezoid support by motor casing
The inner side on base；The lithium battery is positioned in the five of trapezoid support base battery cases.
2. land and air double-used six rotorcraft device as claimed in claim 1, it is characterised in that the aircraft frame, ladder
Shape support selects ABS type 3D printing materials with Athey wheel.
3. land and air double-used six rotorcraft device as claimed in claim 1, it is characterised in that the rotation oar brushless electric machine choosing
With the brshless DC motor that a diameter of 10mm, length 35mm, the diameter of axle are 2.0mm, rotating speed is more than 5W.
4. land and air double-used six rotorcraft device as claimed in claim 1, it is characterised in that the airscrew diameter is selected
50mm。
5. land and air double-used six rotorcraft device as claimed in claim 1, it is characterised in that the bottom of the trapezoid support
Edge lengths are 160mm, a length of 100mm such as trapezoidal two waist, and bottom and the angle of waist are 135 °.
6. land and air double-used six rotorcraft device as claimed in claim 1, it is characterised in that the trapezoidal crawler travel machine
The a diameter of 18mm of Athey wheel of structure, and be placed on trapezoid support in the U-shaped race at each end.
7. land and air double-used six rotorcraft device as claimed in claim 1, it is characterised in that the trapezoidal crawler travel machine
The Athey wheel of lower end two is driving wheel in structure, is driven by Athey wheel motor, and Athey wheel motor is solid by motor casing
It is scheduled on trapezoid support base Inner Front End.
8. land and air double-used six rotorcraft device as claimed in claim 1, it is characterised in that the aircraft frame and ladder
Shape support perimeter is all rounding corner structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710132521.6A CN106827992A (en) | 2017-03-07 | 2017-03-07 | Land and air double-used six rotorcraft device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710132521.6A CN106827992A (en) | 2017-03-07 | 2017-03-07 | Land and air double-used six rotorcraft device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106827992A true CN106827992A (en) | 2017-06-13 |
Family
ID=59138583
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710132521.6A Pending CN106827992A (en) | 2017-03-07 | 2017-03-07 | Land and air double-used six rotorcraft device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106827992A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109466261A (en) * | 2018-11-15 | 2019-03-15 | 甘乾盛 | A kind of land and air double-used multi-functional unmanned plane |
| CN111469617A (en) * | 2020-03-23 | 2020-07-31 | 中国人民解放军军事科学院国防科技创新研究院 | Unmanned plane |
| CN111516443A (en) * | 2020-05-08 | 2020-08-11 | 中国人民解放军陆军炮兵防空兵学院 | Hollow wheel multi-rotor aerocar |
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|---|---|---|---|---|
| CN104401487A (en) * | 2014-11-19 | 2015-03-11 | 中国航空工业经济技术研究院 | Logistics unmanned rotor wing aircraft capable of walking on ground |
| US20160130000A1 (en) * | 2014-11-11 | 2016-05-12 | Jon RIMANELLI | Unmanned air-ground vehicle |
| CN105691600A (en) * | 2015-12-31 | 2016-06-22 | 重庆楠婧琳科技开发有限公司 | Multi-rotor unmanned aerial vehicle |
| CN105752320A (en) * | 2016-04-01 | 2016-07-13 | 陈方平 | Duct type unmanned aerial vehicle and control method thereof |
| CN205395679U (en) * | 2016-03-01 | 2016-07-27 | 安徽理工大学 | Four rotor track aircraft |
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2017
- 2017-03-07 CN CN201710132521.6A patent/CN106827992A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160130000A1 (en) * | 2014-11-11 | 2016-05-12 | Jon RIMANELLI | Unmanned air-ground vehicle |
| CN104401487A (en) * | 2014-11-19 | 2015-03-11 | 中国航空工业经济技术研究院 | Logistics unmanned rotor wing aircraft capable of walking on ground |
| CN105691600A (en) * | 2015-12-31 | 2016-06-22 | 重庆楠婧琳科技开发有限公司 | Multi-rotor unmanned aerial vehicle |
| CN205395679U (en) * | 2016-03-01 | 2016-07-27 | 安徽理工大学 | Four rotor track aircraft |
| CN105752320A (en) * | 2016-04-01 | 2016-07-13 | 陈方平 | Duct type unmanned aerial vehicle and control method thereof |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109466261A (en) * | 2018-11-15 | 2019-03-15 | 甘乾盛 | A kind of land and air double-used multi-functional unmanned plane |
| CN111469617A (en) * | 2020-03-23 | 2020-07-31 | 中国人民解放军军事科学院国防科技创新研究院 | Unmanned plane |
| CN111516443A (en) * | 2020-05-08 | 2020-08-11 | 中国人民解放军陆军炮兵防空兵学院 | Hollow wheel multi-rotor aerocar |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170613 |
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| RJ01 | Rejection of invention patent application after publication |