CN107042886A - A kind of disc-shaped unmanned machine - Google Patents
A kind of disc-shaped unmanned machine Download PDFInfo
- Publication number
- CN107042886A CN107042886A CN201611222168.2A CN201611222168A CN107042886A CN 107042886 A CN107042886 A CN 107042886A CN 201611222168 A CN201611222168 A CN 201611222168A CN 107042886 A CN107042886 A CN 107042886A
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- CN
- China
- Prior art keywords
- disc
- wind vane
- unmanned machine
- shaped
- motor
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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
- B64C39/00—Aircraft not otherwise provided for
- B64C39/001—Flying saucers
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of disc-shaped unmanned machine, including body, the body fuselage is disc shaped shell, the internal body sets control storehouse, wind vane key-course, motor, propeller, the wind vane key-course is located at control storehouse top, and the motor is located at wind vane key-course top, and the motor is connected to propeller.The disc-shaped unmanned machine small volume of the present invention, safety can be widely popularized consumer and use.
Description
Technical field
The present invention relates to unmanned plane field, more particularly, to a kind of disc-shaped unmanned machine.
Background technology
Development of UAV is rapid in recent years, and what most of unmanned planes were used is all many rotor type unmanned planes, many rotors nobody
Rotor needed for machine is generally four wings or eight wings, and wing excessively causes aircraft weight larger, and in control unmanned plane during flying direction
When need weight to be controlled, further increase unmanned plane weight, cause aircraft flying time shorter, because wing is exposed outside
Face, which cannot be protected, easily to be smashed, and potential safety hazard can be caused outside because wing is exposed, simultaneously because multi-rotor unmanned aerial vehicle
Horn structure cause that unmanned plane volume is larger, structure is complex, while multi-rotor unmanned aerial vehicle aeroperformance is inefficient.
The content of the invention
In order to overcome the above-mentioned deficiencies of the prior art, it is an object of the invention to provide a kind of disc-shaped unmanned machine.
In order to solve the above technical problems, the technical scheme is that：A kind of disc-shaped unmanned machine, including body, the machine
Body case is disc shaped shell, and the internal body sets control storehouse, wind vane key-course, motor, propeller, the wind vane control
Preparative layer is located at control storehouse top, and the motor is located at wind vane key-course top, and the motor is connected to propeller.
The wind vane key-course includes wind vane and controls storehouse and wind vane group, and the wind vane group is by least one left and right
Wind vane and at least one front and rear wind vane right-angled intersection are constituted, and front and rear wind vane connects together synchronous turn by universal driving shaft
Dynamic, the left and right wind direction mark connects together synchronous axial system by universal driving shaft, and described disc-shaped unmanned machine shell is engraved structure,
The wind vane junction uses Figure of eight structure, and described unmanned plane motor is coaxially is total to oar motor, and described propeller is double
Paddle structure.
The beneficial effects of the invention are as follows：The unmanned plane pneumatic efficiency that the present invention is used is high, it is not necessary to which weight controls center of gravity, flies
The row time is longer, simultaneously because protected using disc shaped shell, it is stronger to unmanned plane protectiveness, while reducing potential safety hazard.
Brief description of the drawings：Fig. 1 is the disc-shaped unmanned machine embodiment schematic diagram that the present invention is provided, and Fig. 2 is the reality that the present invention is provided
A top view is applied, Fig. 3 is the embodiment Figure of eight structure schematic diagram that the present invention is provided, and Fig. 4 is wind vane key-course schematic diagram.
Embodiment：Furtherly face is made to the present invention with implementation row below in conjunction with the accompanying drawings.
Such as Fig. 1：A kind of disc-shaped unmanned machine, including shell 8, cabin, wing 71,72, GPS module 11, as shown in Fig. 2 outside
Shell 8 is disc shaped shell, the upper outside of shell 8 connection GPS module 11, the enclosure bottom connection control storehouse 2, control storehouse 2
Top is connected to wind vane control storehouse 3, and wind vane control is connected to wind vane key-course 16 around storehouse 3, as shown in figure 4, in Fig. 4
16 each horizontal lines of wind vane key-course and each vertical line all represent a wind vane, and Fig. 1 and Fig. 2 are three wind vane controls
Situation, as shown in figure 3, wind vane side slidable connection is on fixed mount, in Fig. 4, wind direction indicates left and right wind direction
Mark group and front and rear wind vane group are constituted, and all left and right wind direction mark groups are connected by universal driving shaft, and all front and rear wind vane groups pass through connection
Moving axis is connected, as shown in Fig. 2 left and right wind direction mark and front and rear wind vane joint use Figure of eight structure, Fig. 3 is that Figure of eight structure is detailed
Figure；The wind vane layer top is connected to motor 6, and the top of motor 6 is connected to wing；As shown in figure 1, what propeller was used
It is double paddle structures, twin screw includes lower propeller 71 and upper propeller 72.When unmanned plane during flying by controlling storehouse control electricity
The rotating speed of machine realizes the raising and lowering of unmanned plane, when unmanned plane needs movable by controlling the angle of wind vane, control
The rotation direction of steering wheel processed controls the airflow direction of unmanned plane, so as to control aircraft flight direction.
The embodiments of the present invention described above are not intended to limit the scope of the present invention.It is any in the present invention
Spirit and principle within the modifications, equivalent substitutions and improvements made etc., should be included in the claim protection model of the present invention
Within enclosing.
Claims (8)
1. a kind of disc-shaped unmanned machine, including body, it is characterised in that the internal body, which is set, controls storehouse, wind vane key-course,
Motor, propeller, the wind vane key-course is located at control storehouse top, and the motor is located at wind vane key-course top, described
Motor is connected to propeller.
2. a kind of disc-shaped unmanned machine according to claim 1, it is characterised in that the wind vane key-course includes wind vane
Control storehouse and wind vane group.
3. a kind of disc-shaped unmanned machine according to claim 2, it is characterised in that the wind vane group is by least one left and right
Wind vane and at least one front and rear wind vane right-angled intersection are constituted, and front and rear wind vane connects together synchronous turn by universal driving shaft
Dynamic, the left and right wind direction mark connects together synchronous axial system by universal driving shaft.
4. a kind of disc-shaped unmanned machine according to claim 1, it is characterised in that described disc-shaped unmanned machine shell is hollow out
Structure.
5. a kind of disc-shaped unmanned machine according to claim 3, it is characterised in that the wind vane junction uses Figure of eight
Structure.
6. a kind of disc-shaped unmanned machine according to claim 1, it is characterised in that described unmanned plane motor is coaxial oar altogether
Motor.
7. a kind of disc-shaped unmanned machine according to claim 1, it is characterised in that described propeller is double paddle structures.
8. a kind of disc-shaped unmanned machine according to claim 1, it is characterised in that the body fuselage is disc shaped shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611222168.2A CN107042886A (en) | 2016-12-27 | 2016-12-27 | A kind of disc-shaped unmanned machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611222168.2A CN107042886A (en) | 2016-12-27 | 2016-12-27 | A kind of disc-shaped unmanned machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107042886A true CN107042886A (en) | 2017-08-15 |
Family
ID=59543817
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611222168.2A Pending CN107042886A (en) | 2016-12-27 | 2016-12-27 | A kind of disc-shaped unmanned machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107042886A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2856378B1 (en) * | 2003-06-18 | 2006-03-17 | Gaudeffroy Charles Mic Guilhot | REINFORCED SAFETY GYROPTER |
| CN102582834A (en) * | 2012-03-09 | 2012-07-18 | 北京工业大学 | Saucer-shaped aircraft |
| CN202593856U (en) * | 2012-01-14 | 2012-12-12 | 河南科技大学 | Triphibian saucer-shaped unmanned aircraft |
-
2016
- 2016-12-27 CN CN201611222168.2A patent/CN107042886A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2856378B1 (en) * | 2003-06-18 | 2006-03-17 | Gaudeffroy Charles Mic Guilhot | REINFORCED SAFETY GYROPTER |
| CN202593856U (en) * | 2012-01-14 | 2012-12-12 | 河南科技大学 | Triphibian saucer-shaped unmanned aircraft |
| CN102582834A (en) * | 2012-03-09 | 2012-07-18 | 北京工业大学 | Saucer-shaped aircraft |
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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 | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170815 |