CN205060014U - Novel multiaxis unmanned aerial vehicle - Google Patents
Novel multiaxis unmanned aerial vehicle Download PDFInfo
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- CN205060014U CN205060014U CN201520638801.0U CN201520638801U CN205060014U CN 205060014 U CN205060014 U CN 205060014U CN 201520638801 U CN201520638801 U CN 201520638801U CN 205060014 U CN205060014 U CN 205060014U
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- steering wheel
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Abstract
The utility model relates to a novel multiaxis unmanned aerial vehicle, including the organism, its technical characterstic is: the vertical motor that screw propeller blade was installed to a plurality of outputs is installed to the organism bilateral symmetry, and every vertical motor all is connected with a draw gear's drawing end hinge dress, draw gear can drive a plurality ofly vertical motor carries out the while to be changeed with the angle pendulum. The utility model discloses an among this multiaxis unmanned aerial vehicle, steering wheel and steering wheel rocking arm, connecting rod and mounting panel cooperate and to accomplish the control to the vertical motor angle, at multiaxis unmanned aerial vehicle horizontal migration's in -process since the screw propeller blade that the vertical motor output was installed with the horizontal plane angulation, therefore the organism need not to produce the inclination and can accomplish horizontal migration to reduce the aerodynamic drag that the organism bore, and then reduce the loss of battery, the continuation of the journey mileage and the flight time of improving multiaxis unmanned aerial vehicle.
Description
Technical field
The utility model relates to a kind of unmanned vehicle, especially a kind of Novel multi-shaft unmanned plane.
Background technology
Along with development and the innovation of technology, multiaxis unmanned plane is with its small volume and less weight, and the feature being easy to control is widely used in the middle of domestic life field.Reconnoitre at some regional feature, the figure of multiaxis unmanned plane in the process that flight is taken a crane shot and even small freight is transported, can be seen.
The structure of existing multiaxis unmanned plane generally comprises body, battery and flight control unit is equipped with in described body, described body bilateral symmetry is installed with multiple motor vertical, the mouth of each motor vertical is all provided with screw blade, and multiple described motor verticals independently connect the control end of flight control unit.Above-mentioned mounting means makes unmanned plane in flight course, can be completed the various flare maneuvers of unmanned plane by the rotating speed adjusting different vertical motor respectively, facilitates the control of multiple unmanned plane, but adopts above-mentioned mounting structure also to there is certain problem.
Such as, when unmanned plane needs to carry out the motion in horizontal direction, operating personal needs the motor speed regulating unmanned plane side, this side motor speed is made to be greater than the rotating speed of opposite side motor, thus certain inclination angle makes screw blade provide the power of a horizontal direction for body to make unmanned plane occur, but adopt such embodiment can increase multiaxis unmanned plane body to be undoubtedly subject to the area of air resistance and then to cause unnecessary waste of power.Due to the restriction of UAV flight's capacity of cell, adopt above-mentioned embodiment greatly can limit course continuation mileage and the flight time of multiaxis unmanned plane, and then reduce practicality and the field of application of multiaxis unmanned plane; In addition, because body tilts, the air resistance that body bears can apply a downward antagonistic force to body, therefore such mounting structure often increases the fugitiveness in multiaxis unmanned plane during flying process, especially in the state of low-latitude flying, because antagonistic force is uncontrollable, when ambient wind is excessive or flying speed is too fast, very easily there is the situation that body contacts to earth or body damages.
Utility model content
The purpose of this utility model is to overcome the deficiencies in the prior art, provides a kind of rational in infrastructure, a kind of Novel multi-shaft unmanned plane that horizontal flight speed sooner, more reduces energy consumption.
The utility model is achieved through the following technical solutions:
A kind of Novel multi-shaft unmanned plane, comprise body, it is characterized in that: described body bilateral symmetry is provided with the motor vertical that multiple mouth is provided with screw blade, each motor vertical all cuts with scissors load with the traction end of a draw gear and connects, with angle rotation while that described draw gear driving multiple described motor vertical to carry out.
And, before and after in described body lower surface, both side ends is along being hinged with an adapter plate respectively with body vertical direction, this two adapter plate vertically can carry out angle rotation relative to body lower surface, described two adapter plates both side ends stretch out from body both sides respectively, described both ends are all installed with the described motor vertical upwards arranged.
And, in described body, install one for the horizontal power output unit for unmanned plane outputting power in the horizontal direction.
And, described draw gear is a steering wheel, and this steering wheel is arranged in described body lower surface, and the traction end that described steering wheel is made is provided with a steering wheel rocking arm, the end of this steering wheel rocking arm is hinged with a pipe link, and the both side ends of this pipe link cuts with scissors dress mutually with two adapter plates respectively.
And, described horizontal power output unit comprises a horizontal motor, the mouth of this horizontal motor is provided with screw blade, described horizontal motor is fixedly mounted in the body end face between described motor vertical in the horizontal direction, and the mouth of this horizontal motor is in the horizontal direction to body arranged outside.
And described steering wheel is connected with servos control module, described motor vertical and horizontal motor are connected to motor control module, and described servos control module and motor control module are connected to the control end of flight control modules.
Advantage of the present utility model and good effect are:
1, in this multiaxis unmanned plane, steering wheel and steering wheel rocking arm, pipe link and adapter plate match the control that can complete motor vertical angle, in the process of multiaxis unmanned plane parallel motion, the screw blade installed due to motor vertical mouth with horizontal surface angulation, therefore body can complete parallel motion without the need to producing inclination angle, thus reduces the air resistance that bears of body, and then reduce the loss of battery, improve course continuation mileage and the flight time of multiaxis unmanned plane; In addition, due in horizontal motion process, keeping inclination angle without the need to being tuned up by the motor vertical rotating speed of side, therefore, the battery loss that motor vertical high speed rotating causes can be lowered further.
2, in this multiaxis unmanned plane, the participation of horizontal motor can provide an extra propulsive force to the horizontal motion of multiaxis unmanned plane, thus make body in the horizontal direction in can complete high-speed flight operation.
3, in the utility model, draw gear matches with multiple motor vertical and carries out in the process of parallel motion at multiaxis unmanned plane, angle between the screw blade regulating motor vertical mouth to install by adjustment draw gear and horizontal surface, body in parallel motion process without the need to artificially producing angle, can be considered and to parallel with horizontal surface, thus the maximum air resistance reducing body and bear, save the loss of battery, increase flyer miles and the flight time of multiaxis unmanned plane; Horizontal power output unit can provide an auxiliary propulsive force for the parallel motion process of multiaxis unmanned plane, thus the horizontal movement velocity of multiaxis unmanned plane is got a promotion.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the upward view of Fig. 1;
Fig. 3 is the electronic control module schematic diagram in the utility model.
Detailed description of the invention
Elaborate to the utility model below by embodiment, described embodiment is illustrative, and nonrestrictive, can not limit protection domain of the present utility model with this.
A kind of Novel multi-shaft unmanned plane, comprise body 5, battery 3 and flight control unit 4 is equipped with in described body, in this body lower surface, alighting gear 9 is installed, the utility model innovation is, described body bilateral symmetry is provided with the motor vertical 2 that multiple mouth is provided with screw propeller 1, and each motor vertical all cuts with scissors load with the traction end of a draw gear and connects, with angle rotation while that described draw gear driving multiple described motor vertical to carry out.
In the present embodiment, an adapter plate 13 is hinged with respectively by hinge 6 for regulating both side ends edge and body vertical direction before and after in described body lower surface to the rotation of motor vertical, this two adapter plate vertically can carry out angle rotation relative to body lower surface, described two adapter plates both side ends stretch out from body both sides respectively, described both ends are all installed with the described motor vertical upwards arranged.
Described draw gear is a steering wheel 11, this steering wheel is arranged in described body lower surface, the traction end that described steering wheel is made is provided with a steering wheel rocking arm 12, and the end of this steering wheel rocking arm is hinged with a pipe link 10, and the both side ends of this pipe link cuts with scissors dress mutually by rotation bar 8 and two adapter plates respectively.
In the present embodiment, for body in the horizontal direction in auxiliary power is provided, in described body, install one for the horizontal power output unit for unmanned plane outputting power in the horizontal direction.
Described horizontal power output unit comprises a horizontal motor 7, the mouth of this horizontal motor is provided with screw blade, described horizontal motor is fixedly mounted in the body end face between described motor vertical in the horizontal direction, and the mouth of this horizontal motor is in the horizontal direction to body arranged outside.
Described steering wheel is connected with servos control module, and described motor vertical and horizontal motor are connected to motor control module, and described servos control module and motor control module are connected to the control end of flight control modules.
Working process of the present utility model is:
When the utility model carries out vertical takeoff and landing, operating personal only need be opened motor vertical and keep motor vertical mouth to arrange the manipulation can carried out multiaxis unmanned plane in vertical direction straight up, when to need to carry out in horizontal direction mobile for multiaxis unmanned plane, operating personal need be adjusted servos control module by flight control modules, according to real-time environment, the factors such as wind direction regulate cuts with scissors with steering wheel the adapter plate angle filled, thus same angular adjustment is carried out to each motor vertical mouth, the screw blade that motor vertical is installed and horizontal surface angulation, produce the component of a horizontal direction, and then promote body under state inclination angle not occurring at body and carry out horizontal motion, when multiaxis unmanned plane needs to carry out high speed horizontal motion, operating personal only need maintain motor vertical and horizontal surface angulation, unlatching horizontal motor can produce the propulsive force in a horizontal direction afterwards, thus complete the high speed horizontal motion of multiaxis unmanned plane.
In the utility model, draw gear matches with multiple motor vertical and carries out in the process of parallel motion at multiaxis unmanned plane, angle between the screw blade regulating motor vertical mouth to install by adjustment draw gear and horizontal surface, body in parallel motion process without the need to artificially producing angle, can be considered and to parallel with horizontal surface, thus the maximum air resistance reducing body and bear, save the loss of battery, increase flyer miles and the flight time of multiaxis unmanned plane; Horizontal power output unit can provide an auxiliary propulsive force for the parallel motion process of multiaxis unmanned plane, thus the horizontal movement velocity of multiaxis unmanned plane is got a promotion.
Claims (4)
1. a Novel multi-shaft unmanned plane, comprise body, it is characterized in that: described body bilateral symmetry is provided with the motor vertical that multiple mouth is provided with screw blade, each motor vertical all cuts with scissors load with the traction end of a draw gear and connects, before and after in described body lower surface, both side ends is along being hinged with an adapter plate respectively with body vertical direction, the both side ends of described two adapter plates is stretched out from body both sides respectively, described both ends are all installed with the described motor vertical upwards arranged, described draw gear comprises a steering wheel, this steering wheel is arranged in described body lower surface, the traction end that described steering wheel is made is provided with a steering wheel rocking arm, the end of this steering wheel rocking arm is hinged with a pipe link, the both side ends of this pipe link cuts with scissors dress mutually with two adapter plates respectively.
2. a kind of Novel multi-shaft unmanned plane according to claim 1, is characterized in that: in described body, install one for the horizontal power output unit for unmanned plane outputting power in the horizontal direction.
3. a kind of Novel multi-shaft unmanned plane according to claim 2, it is characterized in that: described horizontal power output unit comprises a horizontal motor, the mouth of this horizontal motor is provided with screw blade, described horizontal motor is fixedly mounted in the body end face between described motor vertical in the horizontal direction, and the mouth of this horizontal motor is in the horizontal direction to body arranged outside.
4. a kind of Novel multi-shaft unmanned plane according to claim 1, it is characterized in that: described steering wheel is connected with servos control module, described motor vertical and horizontal motor are connected to motor control module, and described servos control module and motor control module are connected to the control end of flight control modules.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520638801.0U CN205060014U (en) | 2015-08-21 | 2015-08-21 | Novel multiaxis unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520638801.0U CN205060014U (en) | 2015-08-21 | 2015-08-21 | Novel multiaxis unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205060014U true CN205060014U (en) | 2016-03-02 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520638801.0U Expired - Fee Related CN205060014U (en) | 2015-08-21 | 2015-08-21 | Novel multiaxis unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205060014U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105882953A (en) * | 2016-05-17 | 2016-08-24 | 亿航智能设备（广州）有限公司 | Aircraft |
| CN106527463A (en) * | 2016-12-07 | 2017-03-22 | 深圳市元征科技股份有限公司 | Direction control method for unmanned aerial vehicle and unmanned aerial vehicle |
| CN107364572A (en) * | 2017-08-11 | 2017-11-21 | 红河学院 | Fixed-wing vector unmanned plane |
| TWI610850B (en) * | 2015-07-28 | 2018-01-11 | 英華達股份有限公司 | Unmanned vehicle |
-
2015
- 2015-08-21 CN CN201520638801.0U patent/CN205060014U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI610850B (en) * | 2015-07-28 | 2018-01-11 | 英華達股份有限公司 | Unmanned vehicle |
| CN105882953A (en) * | 2016-05-17 | 2016-08-24 | 亿航智能设备（广州）有限公司 | Aircraft |
| CN106527463A (en) * | 2016-12-07 | 2017-03-22 | 深圳市元征科技股份有限公司 | Direction control method for unmanned aerial vehicle and unmanned aerial vehicle |
| CN107364572A (en) * | 2017-08-11 | 2017-11-21 | 红河学院 | Fixed-wing vector unmanned plane |
| CN107364572B (en) * | 2017-08-11 | 2024-01-30 | 昆明学院 | Fixed wing vector unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160302 Termination date: 20170821 |