CN205060003U - Low novel multiaxis unmanned aerial vehicle of power consumption cruises - Google Patents
Low novel multiaxis unmanned aerial vehicle of power consumption cruises Download PDFInfo
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- CN205060003U CN205060003U CN201520637996.7U CN201520637996U CN205060003U CN 205060003 U CN205060003 U CN 205060003U CN 201520637996 U CN201520637996 U CN 201520637996U CN 205060003 U CN205060003 U CN 205060003U
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Abstract
The utility model relates to a low novel multiaxis unmanned aerial vehicle of power consumption cruises, the device comprises a body, a plurality of vertical motor that provide lift for unmanned aerial vehicle are installed to organism both sides symmetry respectively, screw propeller blade is all installed to a plurality of vertical motor's output, and its technical characterstic is: installation no. 1 is used for the horizontal power take -off along horizontal direction output power for unmanned aerial vehicle in the organism. The utility model discloses an among the multiaxis unmanned aerial vehicle the horizontal power take -off cooperation vertical motor and the organism of installation in the organism can make multiaxis unmanned aerial vehicle need not artificially to make the inclination at the horizontal migration in -process to reduce the area that the organism bore aerodynamic drag, and then saved multiaxis unmanned aerial vehicle's energy loss, improvement multiaxis unmanned aerial vehicle's cruise mileage and cruising speed.
Description
Technical field
The utility model relates to a kind of unmanned vehicle, the Novel multi-shaft unmanned plane that especially a kind of power consumption of cruising is low.
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 both sides are uniform is symmetrically 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 carries out cruising operation, need unmanned plane state of kinematic motion interior is in the horizontal direction changed.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 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, because mounting means that the restriction of UAV flight's capacity of cell is above-mentioned greatly limit course continuation mileage and the flight time of multiaxis unmanned plane, reduce practicality and the field of application of multiaxis unmanned plane; In addition, because in the process of parallel motion, air resistance 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 that a kind of rational in infrastructure, speed is faster, Novel multi-shaft unmanned plane that comformability is stronger a kind of power consumption of cruising is low.
The utility model is achieved through the following technical solutions:
The Novel multi-shaft unmanned plane that a kind of power consumption of cruising is low, comprise a body, described body both sides are symmetrically installed with respectively and multiplely provide the motor vertical of lift for unmanned plane, the mouth of described multiple motor vertical is all provided with screw blade, it is characterized in that: in described body, install one for the horizontal power output unit for unmanned plane outputting power in the horizontal direction.
The utility model comprises five kinds of embodiments:
Embodiment 1 as shown in Figure 3, the Novel multi-shaft unmanned plane that a kind of power consumption of cruising is low, comprise a body, described body both sides are symmetrically installed with as depicted in figs. 1 and 24 respectively, 6 (or other even numbers than 0) as shown in Figure 3 provide the motor vertical of lift for unmanned plane, the mouth of described multiple motor vertical is all provided with screw blade, it is characterized in that: 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, 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.
Embodiment 2 as shown in Figure 4, described horizontal power output unit comprises a horizontal motor, the mouth of this horizontal motor is to body arranged outside, described mouth is provided with screw blade, described horizontal motor mouth and screw blade tilt upward to arrange and have angle with horizontal surface shape, and this angle is obtuse angle.
Embodiment 3 as shown in Figure 5, 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.
One anti-twisted power canceller is installed in described body.Described anti-twisted power canceller comprises an empennage, and this empennage bilateral symmetry is provided with the rudder sheet that can swing respectively, and described empennage is arranged on body one side end between multiple motor vertical, and the center bearing of trend of this empennage is provided with described horizontal motor.
Embodiment 4 as shown in Figure 6, 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.
One anti-twisted power canceller is installed in described body.Described anti-twisted power canceller comprises an anti-twisted force motor, and this anti-twisted force motor mouth is provided with another screw blade, the coaxial installation of screw blade that this screw blade and described horizontal motor mouth are installed.
Embodiment 5 as shown in Figure 7, 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.
One anti-twisted power canceller is installed in described body.Described anti-twisted power canceller comprises one second horizontal motor, the mouth of this second horizontal motor is provided with screw blade, described second horizontal motor and horizontal motor contraposition are arranged on the end side of described body, and mouth and the horizontal motor mouth of described second horizontal motor are arranged dorsad.
Advantage of the present utility model and good effect are:
1, in this multiaxis unmanned plane, the horizontal power output unit installed in described body coordinates motor vertical and body can make multiaxis unmanned plane in parallel motion process without the need to artificially manufacturing inclination angle, thus reduce the area that body bears air resistance, and then save the waste of power of multiaxis unmanned plane, improve cruise mileage and the cruising speed of multiaxis unmanned plane.
2, in this multiaxis unmanned plane, horizontal power output unit is a horizontal motor being provided with screw blade, such Power output mode physical construction is simple, successful, with low cost, be convenient to maintenance, not only can solve the problem that multiaxis unmanned plane produces inclination angle in parallel motion process, and this horizontal motor and level are the set-up mode at an obtuse angle, also can avoid horizontal motor at rotary course on the anti-twisted power impact produced in organism level face, thus it is more steady that multiaxis unmanned plane is flown in the process of parallel motion.
3, in this multiaxis unmanned plane, rudder sheet that empennage both sides can swing respectively coordinates can provide an anti-twisted power contrary with the screw blade that horizontal motor is installed to body, thus makes flying in the process of parallel motion of multiaxis unmanned plane more steady.
4, in this multiaxis unmanned plane, adopt anti-twisted force motor to coordinate the embodiment of the screw blade mounting structure of coaxial double-oar can not make the problem of the anti-twisted power of generation, thus make flying in the process of parallel motion of multiaxis unmanned plane more steady.
5, in this multiaxis unmanned plane, the direction of rotation of the screw blade that the second horizontal motor coordinates screw blade in use to fill with horizontal motor, thus the problem of the anti-twisted power produced in offset by the level of electric machine rotation process, thus make flying in the process of parallel motion of multiaxis unmanned plane more steady.
6, in the utility model, the horizontal power output unit installed in described body coordinates motor vertical and body can make multiaxis unmanned plane in parallel motion process without the need to artificially manufacturing inclination angle, and then save the waste of power of multiaxis unmanned plane, and do not increase due to area of thrust surface, therefore, under the prerequisite that horizontal motor power is certain, also add the speed that multiaxis unmanned plane level is advanced; In addition, because the screw blade of motor vertical installation is without the need to providing the power of horizontal direction for body, therefore in the process of multiaxis unmanned plane parallel motion, lift can not reduce, thus makes flight more steady; In addition, the anti-twisted power canceller installed in body can the anti-twisted power that causes under self slew mode of the screw blade installed of offset by the level of motor, thus ensure the flight safety under the horizontal high-speed moving state of multiaxis unmanned plane.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the birds-eye view of Fig. 1;
Fig. 3 is the structural representation of embodiment 1;
Fig. 4 is the structural representation of embodiment 2;
Fig. 5 is the structural representation of embodiment 3;
Fig. 6 is the structural representation of embodiment 4;
Fig. 7 is the structural representation of embodiment 5;
Fig. 8 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.
The Novel multi-shaft unmanned plane that a kind of power consumption of cruising is low, comprise a body 7, be provided with in described body lower surface in this body upper surface of alighting gear 6 to carry and battery 2 and flight control unit 3 are installed, both sides, described body upper surface are symmetrically installed with respectively and multiplely provide the motor vertical 4 of lift for unmanned plane, the mouth of described multiple motor vertical is all provided with screw blade 1, the utility model innovation is, installs one for the horizontal power output unit for unmanned plane outputting power in the horizontal direction in described body.
Above-mentioned multiaxis unmanned plane adopts five kinds of embodiments, is described in detail below respectively by embodiment 1,2,3,4,5.
Embodiment 1
As shown in Figures 2 and 3, the Novel multi-shaft unmanned plane that a kind of power consumption of cruising is low, comprise a body, described body both sides are symmetrically installed with 4 respectively, 6 (or other even numbers than 0) provide the motor vertical of lift for unmanned plane, the mouth of described multiple motor vertical is all provided with screw blade, installs one for the horizontal power output unit for unmanned plane outputting power in the horizontal direction in described body.Described horizontal power output unit comprises a horizontal motor 5, 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.
Embodiment 2
As shown in Figure 4, described horizontal power output unit comprises a horizontal motor, the mouth of this horizontal motor is to body arranged outside, described mouth is provided with screw blade, described horizontal motor mouth and screw blade tilt upward to arrange and to have angle α with horizontal surface shape, and this angle is obtuse angle.
Embodiment 3
As shown in Figure 5, 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.
One anti-twisted power canceller is installed in described body.Described anti-twisted power canceller comprises an empennage 8, and this empennage bilateral symmetry is provided with the rudder sheet 9 that can swing respectively, and described empennage is arranged on body one side end between multiple motor vertical, and the center bearing of trend of this empennage is provided with described horizontal motor.
Embodiment 4
As shown in Figure 6, 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.
One anti-twisted power canceller is installed in described body.Described anti-twisted power canceller comprises an anti-twisted force motor 10, and this anti-twisted force motor mouth is provided with another screw blade, the coaxial installation of screw blade that this screw blade and described horizontal motor mouth are installed.
Embodiment 5
As shown in Figure 7, 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.
One anti-twisted power canceller is installed in described body.Described anti-twisted power canceller comprises one second horizontal motor 11, the mouth of this second horizontal motor is provided with screw blade, described second horizontal motor and horizontal motor contraposition are arranged on the end side of described body, and mouth and the horizontal motor mouth of described second horizontal motor are arranged dorsad.
Working process of the present utility model is:
When adopting the structure as shown in Fig. 1 or Fig. 3, the lifting of operating personal by regulating the rotating speed of motor vertical can control multiaxis unmanned plane, when multiaxis unmanned plane needs to carry out parallel motion, operating personal only need control flight control unit can open horizontal motor, after horizontal motor rotates, body is provided to the propulsive force in a horizontal direction, thus under the state without the need to multiaxis unmanned plane inclination angle, change its state of flight, the flying speed of operating personal by regulating the rotating speed of horizontal motor can control multiaxis unmanned plane.
When adopting structure as shown in Figure 4, the lifting of operating personal by regulating the rotating speed of motor vertical can control multiaxis unmanned plane, when multiaxis unmanned plane needs to carry out parallel motion, operating personal only need control flight control unit can open horizontal motor, after horizontal motor rotates, body is provided to the propulsive force in a horizontal direction, thus under the state without the need to multiaxis unmanned plane inclination angle, change its state of flight, the flying speed of operating personal by regulating the rotating speed of horizontal motor can control multiaxis unmanned plane; In addition when horizontal motor rotates, screw blade also can produce to body the component that a summary arranges downwards, and then the anti-twisted power problem avoiding horizontal motor to be horizontally disposed with causing, and too increases the stability under multiaxis unmanned plane during flying state.
When adopting structure as shown in Figure 5, the lifting of operating personal by regulating the rotating speed of motor vertical can control multiaxis unmanned plane, when multiaxis unmanned plane needs to carry out parallel motion, operating personal only need control flight control unit can open horizontal motor, after horizontal motor rotates, body is provided to the propulsive force in a horizontal direction, thus under the state without the need to multiaxis unmanned plane inclination angle, change its state of flight, the flying speed of operating personal by regulating the rotating speed of horizontal motor can control multiaxis unmanned plane; In addition in the process of multiaxis unmanned plane parallel motion, the screw blade that horizontally disposed horizontal motor is installed rotates and inherently produces an anti-twisted power, now, the rudder sheet that the empennage cooperation activity that body end is installed is installed can swing voluntarily according to stressing conditions, regulate the air-flow flowing through empennage to offset anti-twisted power, thus ensure the smooth flight of multiaxis unmanned plane.
When adopting structure as shown in Figure 6, the lifting of operating personal by regulating the rotating speed of motor vertical can control multiaxis unmanned plane, when multiaxis unmanned plane needs to carry out parallel motion, operating personal only need control flight control unit can open horizontal motor, after horizontal motor rotates, body is provided to the propulsive force in a horizontal direction, thus under the state without the need to multiaxis unmanned plane inclination angle, change its state of flight, the flying speed of operating personal by regulating the rotating speed of horizontal motor can control multiaxis unmanned plane; Anti-twisted force motor coordinates the mounting means of coaxial double-oar can not produce anti-twisted power in flight course, thus ensures the smooth flight of multiaxis unmanned plane.
When adopting structure as shown in Figure 7, the lifting of operating personal by regulating the rotating speed of motor vertical can control multiaxis unmanned plane, when multiaxis unmanned plane needs to carry out parallel motion, operating personal only need control flight control unit can open horizontal motor, after horizontal motor rotates, body is provided to the propulsive force in a horizontal direction, thus its state of flight is changed under the state without the need to multiaxis unmanned plane inclination angle, the flying speed of operating personal by regulating the rotating speed of horizontal motor can control multiaxis unmanned plane, the screw blade meanwhile installed by control second horizontal motor and the horizontal motor screw blade contrarotation of installing, get final product the anti-twisted power produced in offset by the level of electric machine rotation process, thus ensure the smooth flight of multiaxis unmanned plane.
In the utility model, the horizontal power output unit installed in described body coordinates motor vertical and body can make multiaxis unmanned plane in parallel motion process without the need to artificially manufacturing inclination angle, and then save the waste of power of multiaxis unmanned plane, and do not increase due to area of thrust surface, therefore, under the prerequisite that horizontal motor power is certain, also add the speed that multiaxis unmanned plane level is advanced; In addition, because the screw blade of motor vertical installation is without the need to providing the power of horizontal direction for body, therefore in the process of multiaxis unmanned plane parallel motion, lift can not reduce, thus makes flight more steady; In addition, the anti-twisted power canceller installed in body can the anti-twisted power that causes under self slew mode of the screw blade installed of offset by the level of motor, thus ensure the flight safety under the horizontal high-speed moving state of multiaxis unmanned plane.
Claims (8)
1. the Novel multi-shaft unmanned plane that a power consumption of cruising is low, comprise a body, described body both sides are symmetrically installed with respectively and multiplely provide the motor vertical of lift for unmanned plane, the mouth of described multiple motor vertical is all provided with screw blade, it is characterized in that: in described body, install one for the horizontal power output unit for unmanned plane outputting power in the horizontal direction.
2. the Novel multi-shaft unmanned plane that a kind of power consumption of cruising according to claim 1 is low, 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.
3. the Novel multi-shaft unmanned plane that a kind of power consumption of cruising according to claim 1 is low, it is characterized in that: described horizontal power output unit comprises a horizontal motor, the mouth of this horizontal motor is to body arranged outside, described mouth is provided with screw blade, described horizontal motor mouth and screw blade tilt upward to arrange and have angle with horizontal surface shape, and this angle is obtuse angle.
4. the Novel multi-shaft unmanned plane that a kind of power consumption of cruising according to claim 2 is low, is characterized in that: be provided with an anti-twisted power canceller in described body.
5. the Novel multi-shaft unmanned plane that a kind of power consumption of cruising according to claim 4 is low, it is characterized in that: described anti-twisted power canceller comprises an empennage, this empennage bilateral symmetry is provided with the rudder sheet that can swing respectively, described empennage is arranged on body one side end between multiple motor vertical, and the center bearing of trend of this empennage is provided with described horizontal motor.
6. the Novel multi-shaft unmanned plane that a kind of power consumption of cruising according to claim 4 is low, it is characterized in that: described anti-twisted power canceller comprises an anti-twisted force motor, this anti-twisted force motor mouth is provided with another screw blade, the coaxial installation of screw blade that this screw blade and described horizontal motor mouth are installed.
7. the Novel multi-shaft unmanned plane that a kind of power consumption of cruising according to claim 4 is low, it is characterized in that: described anti-twisted power canceller comprises one second horizontal motor, the mouth of this second horizontal motor is provided with screw blade, described second horizontal motor and horizontal motor contraposition are arranged on the end side of described body, and mouth and the horizontal motor mouth of described second horizontal motor are arranged dorsad.
8. the Novel multi-shaft unmanned plane that a kind of power consumption of cruising according to Claims 2 or 3 is low, it is characterized in that: described motor vertical and horizontal motor are connected to motor control module, described motor control module is connected with the control end of flight control modules.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520637996.7U CN205060003U (en) | 2015-08-21 | 2015-08-21 | Low novel multiaxis unmanned aerial vehicle of power consumption cruises |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520637996.7U CN205060003U (en) | 2015-08-21 | 2015-08-21 | Low novel multiaxis unmanned aerial vehicle of power consumption cruises |
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| CN205060003U true CN205060003U (en) | 2016-03-02 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520637996.7U Expired - Fee Related CN205060003U (en) | 2015-08-21 | 2015-08-21 | Low novel multiaxis unmanned aerial vehicle of power consumption cruises |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105711825A (en) * | 2016-03-18 | 2016-06-29 | 吴李海 | Hybrid power unmanned aerial vehicle |
| CN107140185A (en) * | 2017-05-22 | 2017-09-08 | 程伯儒 | A kind of intelligent multi-rotor unmanned aerial vehicle |
| CN110065627A (en) * | 2019-04-30 | 2019-07-30 | 中北大学 | A kind of bionical unmanned vehicle of multifunctional rescue |
-
2015
- 2015-08-21 CN CN201520637996.7U patent/CN205060003U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105711825A (en) * | 2016-03-18 | 2016-06-29 | 吴李海 | Hybrid power unmanned aerial vehicle |
| CN107140185A (en) * | 2017-05-22 | 2017-09-08 | 程伯儒 | A kind of intelligent multi-rotor unmanned aerial vehicle |
| CN107140185B (en) * | 2017-05-22 | 2018-12-28 | 广东利美隆文化股份有限公司 | A kind of intelligence multi-rotor unmanned aerial vehicle |
| CN110065627A (en) * | 2019-04-30 | 2019-07-30 | 中北大学 | A kind of bionical unmanned vehicle of multifunctional rescue |
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Granted publication date: 20160302 Termination date: 20170821 |
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| CF01 | Termination of patent right due to non-payment of annual fee |