CN108438206B - Unmanned aerial vehicle capable of self-balancing according to wind direction - Google Patents
Unmanned aerial vehicle capable of self-balancing according to wind direction Download PDFInfo
- Publication number
- CN108438206B CN108438206B CN201810095250.6A CN201810095250A CN108438206B CN 108438206 B CN108438206 B CN 108438206B CN 201810095250 A CN201810095250 A CN 201810095250A CN 108438206 B CN108438206 B CN 108438206B
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- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- rotor wing
- adjusting
- wind direction
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
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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
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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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C2009/005—Ailerons
Abstract
The invention discloses an unmanned aerial vehicle capable of self-balancing according to wind direction, which comprises a bottom shock pad, an adjusting web plate, a mechanical rotor wing and a microcontroller, wherein a folding support leg is arranged above the bottom shock pad, a web plate steering rod is arranged above the adjusting web plate, the mechanical rotor wing is connected above a telescopic adjusting shaft, a shaft part protecting bearing is arranged below the mechanical rotor wing, an all-metal protective shell is arranged below the shaft part protecting bearing, a signal receiver is communicated below the all-metal protective shell, the microcontroller is arranged above the signal receiver, a holographic camera is arranged below the microcontroller, a telescopic lens is arranged inside the holographic camera, and a high-energy lithium battery is arranged inside the all-metal protective shell. The invention can adjust the flight direction of the unmanned aerial vehicle according to the wind direction, greatly saves the operation energy of the unmanned aerial vehicle, and has longer flight time of the unmanned aerial vehicle.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle equipment, in particular to an unmanned aerial vehicle capable of self-balancing according to wind direction.
Background
An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology. Chinese patent No. 201710158178.2 discloses an unmanned aerial vehicle, including frame and a plurality of angle bead, angle bead detachable fixes the corner of frame, the angle bead towards the one side of frame has been seted up at least one and has been used for with the angle bead card is put first draw-in groove in the frame. The above patent can not adjust the wing, and the energy consumption is great.
Disclosure of Invention
The invention aims to solve the problems and provide the unmanned aerial vehicle capable of self-balancing according to the wind direction.
The invention realizes the purpose through the following technical scheme:
an unmanned aerial vehicle capable of self-balancing according to wind direction comprises a bottom shock pad, an adjusting web plate, a mechanical rotor and a microcontroller, wherein a folding supporting leg is installed above the bottom shock pad, an unmanned aerial vehicle aileron is installed above the folding supporting leg, the adjusting web plate is installed above the unmanned aerial vehicle aileron, a web plate direction adjusting rod is arranged above the adjusting web plate, a rotor installation seat is installed above the web plate direction adjusting rod, a telescopic adjusting shaft is installed above the rotor installation seat, the mechanical rotor is connected above the telescopic adjusting shaft, a shaft part protecting bearing is installed below the mechanical rotor, an all-metal protective shell is installed below the shaft part protecting bearing, a signal receiver is communicated below the all-metal protective shell, the microcontroller is installed above the signal receiver, and a holographic camera is installed below the microcontroller, the holographic camera internally mounted has telescopic camera lens, full metal protective housing internally mounted has the high energy lithium cell.
Further, the bottom shock pad is glued with the foldable landing leg, and the unmanned aerial vehicle aileron is connected with the adjusting web through a bolt.
Further, the web steering rod with the rotor mount pad passes through bolted connection, flexible regulating spindle with mechanical rotor passes through bolted connection.
Further, the shaft part protection bearing is connected with the telescopic adjusting shaft in a nested mode, and the signal receiver is connected with the microcontroller through a lead.
Further, the holographic camera is connected with the microcontroller through a wire.
Furthermore, the mechanical rotor wing is formed by pressing alloy steel, and the surface of the mechanical rotor wing is subjected to plastic spraying treatment.
Further, the holographic camera is connected with the telescopic lens in a nested mode.
Further, the microcontroller is connected with the high-energy lithium battery through a lead.
The invention has the beneficial effects that: can adjust unmanned aerial vehicle flight direction according to the wind direction, practice thrift the unmanned aerial vehicle running energy in a large number, unmanned aerial vehicle flight time is longer.
Drawings
Fig. 1 is a front view of a self-balancing drone according to the invention;
FIG. 2 is a holographic camera diagram of an unmanned aerial vehicle according to the invention, which can be self-balanced according to wind direction;
fig. 3 is a diagram of an all-metal protective shell of the unmanned aerial vehicle capable of self-balancing according to wind direction.
Wherein: 1. a bottom cushion; 2. folding legs; 3. an unmanned aerial vehicle aileron; 4. an adjusting web; 5. a web direction adjusting rod; 6. a rotor mounting base; 7. a telescopic adjusting shaft; 8. a mechanical rotor; 9. a shaft portion protection bearing; 10. an all-metal protective case; 11. a signal receiver; 12. a microcontroller; 13. a holographic camera; 14. a retractable lens; 15. high-energy lithium battery.
Detailed Description
The invention will be further described with reference to the accompanying drawings in which:
as shown in fig. 1-3, an unmanned aerial vehicle capable of self-balancing according to wind direction comprises a bottom shock pad 1, an adjusting web 4, a mechanical rotor 8 and a microcontroller 12, a foldable leg 2 is installed above the bottom shock pad 1, an unmanned aerial vehicle aileron 3 is installed above the foldable leg 2, the adjusting web 4 is installed above the unmanned aerial vehicle aileron 3, a web steering rod 5 is arranged above the adjusting web 4, a rotor mount 6 is installed above the web steering rod 5, a telescopic adjusting shaft 7 is installed above the rotor mount 6, the mechanical rotor 8 is connected above the telescopic adjusting shaft 7, a shaft portion protecting bearing 9 is installed below the mechanical rotor 8, an all-metal protective shell 10 is installed below the shaft portion protecting bearing 9, a signal receiver 11 is communicated below the all-metal protective shell 10, the microcontroller 12 is installed above the signal receiver 11, and a holographic camera 13 is installed below the microcontroller 12, the holographic camera 13 is internally provided with a telescopic lens 14, and the all-metal protective shell 10 is internally provided with a high-energy lithium battery 15.
The bottom shock pad 1 is used for shock absorption protection of the foldable landing leg 2, the foldable landing leg 2 is used for fixing and supporting the unmanned aerial vehicle, the unmanned aerial vehicle aileron 3 is used for assisting flight and direction adjustment of the unmanned aerial vehicle, the adjusting web 4 is used for adjusting the unmanned aerial vehicle according to the wind direction, the operation energy of the unmanned aerial vehicle is saved, the adjusting web 4 is adjusted by the web adjusting rod 5, the rotor wing mounting seat 6 is used for fixing and mounting the mechanical rotor wing 8, the telescopic adjusting shaft 7 is used for adjusting the height of the mechanical rotor wing 8, the mechanical rotor wing 8 is used for driving the unmanned aerial vehicle to fly, the shaft part protecting bearing 9 is used for protecting the telescopic adjusting shaft 7, the signal receiver 11 is used for receiving a control signal of the unmanned aerial vehicle, the microcontroller 12 is used for automatic control of the unmanned aerial vehicle, the holographic camera 13 is used for shooting external scenery, the telescopic lens 14 is used for focusing adjustment of the holographic camera 13, high-energy lithium battery 15 is used for providing power for unmanned aerial vehicle work.
Bottom shock pad 1 is sticky with foldable landing leg 2, unmanned aerial vehicle aileron 3 passes through bolted connection with adjusting web 4, web turn to pole 5 and rotor mount pad 6 pass through bolted connection, flexible regulating spindle 7 passes through bolted connection with mechanical rotor 8, axial region protection bearing 9 and flexible regulating spindle 7 nested connection, signal receiver 11 passes through the wire with microcontroller 12 and is connected, holographic camera 13 passes through the wire with microcontroller 12 and is connected, mechanical rotor 8 forms for alloy steel suppression, the surface is spouted plastics and is handled, holographic camera 13 and telescopic camera 14 nested connection, microcontroller 12 passes through the wire with high energy lithium cell 15 and is connected.
It should be noted that the above embodiments are only used for illustrating the technical solutions of the present invention, and not for limiting the same; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions of the embodiments of the present invention.
Claims (5)
1. The utility model provides a can be according to unmanned aerial vehicle of wind direction self-adjusting balance which characterized in that: comprises a bottom shock pad (1), an adjusting web (4), a mechanical rotor wing (8) and a microcontroller (12), wherein a folding landing leg (2) is installed above the bottom shock pad (1), an unmanned aerial vehicle aileron (3) is installed above the folding landing leg (2), the adjusting web (4) is installed above the unmanned aerial vehicle aileron (3), a web steering rod (5) is arranged above the adjusting web (4), a rotor wing installation seat (6) is installed above the web steering rod (5), a telescopic adjusting shaft (7) is installed above the rotor wing installation seat (6), the mechanical rotor wing (8) is connected above the telescopic adjusting shaft (7), a shaft part protection bearing (9) is installed below the mechanical rotor wing (8), an all-metal protection shell (10) is installed below the shaft part protection bearing (9), and a signal receiver (11) is communicated below the all-metal protection shell (10), the micro controller (12) is installed above the signal receiver (11), the holographic camera (13) is installed below the micro controller (12), the telescopic lens (14) is installed inside the holographic camera (13), and the high-energy lithium battery (15) is installed inside the all-metal protective shell (10); the web plate direction adjusting rod (5) is connected with the rotor wing mounting seat (6) through a bolt, and the telescopic adjusting shaft (7) is connected with the mechanical rotor wing (8) through a bolt; the mechanical rotor wing (8) is formed by pressing alloy steel, and the surface of the mechanical rotor wing is subjected to plastic spraying treatment; the bottom shock pad (1) is glued with the folding support leg (2), and the unmanned aerial vehicle aileron (3) is connected with the adjusting web (4) through a bolt.
2. An unmanned aerial vehicle capable of self-balancing according to wind direction according to claim 1, wherein: the shaft part protection bearing (9) is connected with the telescopic adjusting shaft (7) in a nested mode, and the signal receiver (11) is connected with the microcontroller (12) through a lead.
3. An unmanned aerial vehicle capable of self-balancing according to wind direction according to claim 1, wherein: the holographic camera (13) is connected with the microcontroller (12) through a lead.
4. An unmanned aerial vehicle capable of self-balancing according to wind direction according to claim 1, wherein: the holographic camera (13) is connected with the telescopic lens (14) in a nested mode.
5. An unmanned aerial vehicle capable of self-balancing according to wind direction according to claim 1, wherein: the microcontroller (12) is connected with the high-energy lithium battery (15) through a lead.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810095250.6A CN108438206B (en) | 2018-01-31 | 2018-01-31 | Unmanned aerial vehicle capable of self-balancing according to wind direction |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810095250.6A CN108438206B (en) | 2018-01-31 | 2018-01-31 | Unmanned aerial vehicle capable of self-balancing according to wind direction |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108438206A CN108438206A (en) | 2018-08-24 |
| CN108438206B true CN108438206B (en) | 2022-03-15 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810095250.6A Active CN108438206B (en) | 2018-01-31 | 2018-01-31 | Unmanned aerial vehicle capable of self-balancing according to wind direction |
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| CN (1) | CN108438206B (en) |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IT1391165B1 (en) * | 2008-08-04 | 2011-11-18 | Cilli | AERODYNAMIC CONTROL SYSTEM FOR HELICOPTER WITH POSITIONS WITH COUNTER-COUNTER-WHEEL LOADS AND WITHOUT CYCLIC VARIATION OF THE STEP |
| CN105000174A (en) * | 2014-12-05 | 2015-10-28 | 上海交通大学 | Tiltrotor mixed multi-state aircraft with operational control surfaces |
| CN205837224U (en) * | 2016-07-15 | 2016-12-28 | 张宇川 | A kind of scalable is taken photo by plane unmanned plane |
| CN106428524B (en) * | 2016-11-25 | 2019-09-13 | 南京柯尔航空科技有限公司 | A kind of multi-rotor aerocraft with the free wing |
| CN106628162A (en) * | 2016-12-21 | 2017-05-10 | 曹萍 | Composite unmanned aerial vehicle |
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2018
- 2018-01-31 CN CN201810095250.6A patent/CN108438206B/en active Active
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| Publication number | Publication date |
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| CN108438206A (en) | 2018-08-24 |
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