CN205381395U - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
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- CN205381395U CN205381395U CN201620091515.1U CN201620091515U CN205381395U CN 205381395 U CN205381395 U CN 205381395U CN 201620091515 U CN201620091515 U CN 201620091515U CN 205381395 U CN205381395 U CN 205381395U
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- 230000000694 effects Effects 0.000 claims description 5
- 230000005489 elastic deformation Effects 0.000 claims description 5
- 230000005484 gravity Effects 0.000 claims description 3
- 239000003381 stabilizer Substances 0.000 abstract 1
- 230000013011 mating Effects 0.000 description 8
- 238000005516 engineering process Methods 0.000 description 2
- 230000001154 acute effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Abstract
The utility model provides an unmanned aerial vehicle, its include the mount pad and with a plurality of horns that the mount pad is connected, a plurality of horns include first horn, be provided with power device on the first horn. First horn can for the mount pad warp to the deformation state is worked as including bearing state and foot rest state during unmanned aerial vehicle flight, first horn is in the state that bears, makes power device does unmanned aerial vehicle provides flight power, when when unmanned aerial vehicle lands, first horn is in the foot rest state, makes first horn uses as the stabilizer blade.
Description
Technical field
This utility model relates to a kind of unmanned vehicle.
Background technology
Generally, rising and falling of unmanned vehicle is required for the safety and stability that undercarriage ensures to land.But unmanned vehicle is when airflight, described undercarriage can increase the complete machine weight of described unmanned vehicle, makes shorten the cruising time of described unmanned vehicle.When unmanned vehicle be used for carrying video camera carry out taking photo by plane operation time, above-mentioned undercarriage also can stop to take photo by plane work in the shooting visual field of the video camera being arranged on described unmanned vehicle, impact.Even if adopt can the undercarriage of folding and unfolding, still can increase the complete machine weight of unmanned vehicle, and can cause that the structure of unmanned vehicle is complicated.
Utility model content
In view of this, it is necessary to a kind of lighter in weight, the relatively simple unmanned vehicle of structure are provided.
A kind of unmanned vehicle, it includes mounting seat and the multiple horns being connected with described mounting seat, and the plurality of horn includes the first horn, and described first horn is provided with power set.Described first horn can deform relative to described mounting seat, and deformation state includes loaded state and foot rest state, when described unmanned vehicle flight, described first horn is in loaded state, makes described power set provide flying power for described unmanned vehicle；When described unmanned vehicle lands, described first horn is in foot rest state, makes described first horn use as leg.
Further, described power set include motor and are arranged at the propeller on described motor, and the rotation that described motor is described propeller provides power；And/or,
The quantity of described first horn is multiple, and multiple described first horns are symmetrical arranged.
Further, described first horn could alter that its bearing of trend relative to described mounting seat at least partially.
Further, described power set are arranged at described first horn one end away from described mounting seat, and described power set can drive described first horn deformation, to change at least some of bearing of trend relative to described mounting seat of described first horn.
Further, described power set can drive described first horn to be deformed into described loaded state from described foot rest state.
Further, described first horn deformation time, it is possible to change described power set relative to described mounting seat towards.
Further, described first horn being additionally provided with deformation power set, described deformation power set can drive at least some of rotation of described first horn, to change at least some of bearing of trend relative to described mounting seat of described first horn；And/or,
Described first horn is perpendicular to the area of the cross section of the length direction of described first horn away from the area of one end of described mounting seat more than the remainder of described first horn.
Further, described first horn is connected to an auxiliary supports away from one end of described mounting seat, when described first horn carries the weight of described unmanned vehicle as leg, described auxiliary supports, for abutting with landing face, makes described first horn be stablely supported on described landing face.
Further, can there is elastic deformation in described auxiliary supports, to cushion described first horn impact force.
Further, sleeved part that described auxiliary supports includes housing described first horn one end and the axial vertically extending extension along described sleeved part, stability when described extension is in landing state for ensureing described unmanned vehicle.
Further, being arranged on described auxiliary supports on described first horn and described power set and be positioned at the homonymy of described first horn, described extension can protect described power set.
Further, described unmanned vehicle includes controller, and described controller can produce and send control signals to described power set, to control described power set.
Further, described controller controls described unmanned vehicle and responds the instruction of user side of described unmanned vehicle, and generates and sends described control signal to described power set according to described instruction；Or,
Described unmanned vehicle also includes the sensing component of the deformation state for detecting described first horn, and described controller generates and sends described control signal to described power set according to the sensitive information that described sensing component senses.
Further, described first horn includes linkage section and the supporting section being rotationally connected with described linkage section, and described supporting section can rotate relative to described linkage section, so that described supporting section can use as leg.
Further, described unmanned vehicle also includes exchanging structure, and described exchanging structure is rotationally connected described linkage section and described supporting section；Described exchanging structure is for limiting the described supporting section slewing area relative to described linkage section.
Further, described exchanging structure includes elastic component, and one end of described elastic component connects described linkage section, and the other end connects described supporting section, is used for providing an elastic restoring force to described supporting section.
Further, described elastic component is arranged at the not homonymy of corresponding described first horn with corresponding described power set, described supporting section can rotate along a predetermined direction under described elastic restoring force effect, simultaneously, when described unmanned vehicle is in landing state, described elastic component makes described first horn entirety be introversion state.
Further, described supporting section can rotate along described predetermined direction relative to described mounting seat under described elastic restoring force and action of gravity, carries the weight of described unmanned vehicle using the leg as described unmanned vehicle；Described supporting section rotates with described predetermined direction opposite direction along one relative to described linkage section, to allow described power set to provide flying power for described unmanned vehicle.
Further, the plurality of horn also includes the second horn；The length of described first horn is more than the length of described second horn.
Further, the quantity of described first horn is equal with the quantity of described second horn, and described second horn is arranged alternately along the periphery of described mounting seat successively with described first horn.
Further, described second horn is provided with described power set, is arranged on the power set on described second horn for providing flying power for this unmanned vehicle.
Further, the power of the described power set being arranged on described first horn is less than the power of the described power set being arranged on described second horn.
A kind of unmanned vehicle, it includes mounting seat and is connected to multiple horns of described mounting seat, and each described horn is provided with power set, and described power set can provide flying power for the flight of described unmanned vehicle.The second horn that the plurality of horn includes multiple first horn and multiple and the plurality of first horn is arranged alternately, the length of described first horn is more than the length of described second horn；Described first horn can deform, and deformation state includes loaded state and foot rest state.When described unmanned vehicle flight, described first horn is in loaded state, makes described power set provide flying power for described unmanned vehicle；When described unmanned vehicle lands, described first horn is in foot rest state, makes described first horn use as leg.
Wherein, the described power set being arranged on described second horn provide main flying power for described unmanned vehicle；It is arranged on the described power set on described first horn and can provide flying power for described unmanned vehicle, or drive described first horn to rotate so that described first horn deforms.
Above-mentioned unmanned vehicle, described first horn can deform relative to described mounting seat, and deformation state includes loaded state and foot rest state, when described unmanned vehicle flight, described first horn is in loaded state, makes described power set provide flying power for described unmanned vehicle；When described unmanned vehicle lands, described first horn is in foot rest state, makes described first horn use as leg.Described first horn can be provided simultaneously with the function of horn and leg, saves leg so that the overall weight of described unmanned vehicle is relatively light, and structure is by a relatively simple.
Accompanying drawing explanation
Fig. 1 is the structural representation of the horn of unmanned vehicle that provides of this utility model one embodiment and mounting seat.
Fig. 2 is the decomposing schematic representation of the exchanging structure in Fig. 1.
Main element symbol description
| Mounting seat | 10 |
| Horn | 20 |
| First horn | 21 |
| Linkage section | 211 |
| Supporting section | 212 |
| Second horn | 22 |
| Power set | 30 |
| Motor | 31 |
| Propeller | 32 |
| Blade | 321 |
| Exchanging structure | 40 |
| Fixed part | 41 |
| Holding tank | 411 |
| First axis hole | 412 |
| First mating holes | 413 |
| Movable part | 42 |
| Accepting groove | 421 |
| Second axis hole | 422 |
| Second mating holes | 423 |
| Rotating shaft | 43 |
| Sleeve | 44 |
| Elastic component | 45 |
| Auxiliary supports | 50 |
| Sleeved part | 51 |
| Extension | 52 |
Following detailed description of the invention will further illustrate this utility model in conjunction with above-mentioned accompanying drawing.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model, rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of this utility model protection.
It should be noted that be referred to as " being fixed on " another assembly when assembly, it can directly on another assembly or can also there is assembly placed in the middle.When an assembly is considered as " connection " another assembly, it can be directly to another assembly or may be simultaneously present assembly placed in the middle.When an assembly is considered as " being arranged at " another assembly, it can be set directly on another assembly or may be simultaneously present assembly placed in the middle.
Unless otherwise defined, all of technology used herein and scientific terminology are identical with belonging to the implication that those skilled in the art of the present utility model are generally understood that.The purpose describing specific embodiment it is intended merely to herein, it is not intended that in restriction this utility model at term used in the description of the present utility model.Term as used herein " and/or " include the arbitrary and all of combination of one or more relevant Listed Items.
Below in conjunction with accompanying drawing, embodiments more of the present utility model are elaborated.When not conflicting, the feature in following embodiment and embodiment can be mutually combined.
Seeing also Fig. 1 and Fig. 2, the unmanned vehicle that this utility model one embodiment provides, it includes mounting seat 10, horn 20, power set 30, exchanging structure 40 and auxiliary supports 50.Being appreciated that in other embodiments, described unmanned vehicle can include more or less assembly.Described horn 20 is connected to described mounting seat 10.Described power set 30 are arranged on described horn 20, and the flight that described power set 30 are described unmanned vehicle provides flying power.The quantity of described horn 20 is multiple, and each described horn 20 is provided with described power set 30.In present embodiment, the quantity of the quantity of described horn 20 and described power set 30 is eight.Being appreciated that in other embodiments, several in the horn 20 of described unmanned vehicle can be not provided with described power set 30.
Described horn 20 includes the first horn 21 and the second horn 22, and the length of described first horn 21 is more than the length of described second horn 22.Being appreciated that in other embodiments, described first horn 21 can be leg, makes described first horn 21 be in foot rest state.
Described first horn 21 can deform relative to described mounting seat 10, and deformation state includes loaded state and described foot rest state, when described unmanned vehicle flight, described first horn 21 is in loaded state, makes described power set 30 provide flying power for described unmanned vehicle；When described unmanned vehicle lands, described first horn 21 is in foot rest state, makes described first horn 21 use as leg.
It is arranged on the described power set 30 on described first horn 21 and can provide flying power for described unmanned vehicle, or drive described first horn 21 to rotate, so that described first horn 21 deforms.It is appreciated that, in other embodiments, the rotation of described first horn 21 can not be driven by described power set 30, but is driven so that described first horn 21 deforms relative to described mounting seat 10 by deformation power set, and described deformation power set are arranged on described first horn 21.
When described unmanned vehicle is converted to landing state by state of flight or is converted to state of flight by landing state, at least some of bearing of trend relative to described mounting seat 10 of described first horn 21 is along with changing.Described exchanging structure 40 can limit the change scope of at least some of bearing of trend relative to described mounting seat 10 of described first horn 21.In present embodiment, the quantity of described first horn 21 is equal with the quantity of described second horn 22, is four, and four described first horns 21 and four described second horns 22 are arranged alternately successively along the periphery of described mounting seat 10.
Described first horn 21 includes linkage section 211 and the supporting section 212 being rotationally connected with described linkage section 211, and one end of described linkage section 211 is removably attachable to described mounting seat 10, and the other end and described supporting section 212 are rotationally connected.In present embodiment, described linkage section 211 is rotationally connected by described exchanging structure 40 with described supporting section 212.The described power set 30 being arranged at described first horn 21 are positioned at described supporting section 212 one end away from described mounting seat 10, and described supporting section 212 can pass through corresponding described power set 30 and change self bearing of trend relative to described linkage section 211.The power set 30 being arranged on described second horn 22 are positioned at described second horn 22 one end away from described mounting seat 10.Being appreciated that in other embodiments, described first horn 21 can be structure as a whole, and described first horn 21 is rotationally connected described mounting seat 10.In present embodiment, the quantity of described exchanging structure 40 is four, and four described exchanging structures 40 are respectively used to four the described supporting sections 212 of the restriction slewing area relative to described mounting seat 10.Being appreciated that in other embodiments, described exchanging structure 40 can omit, and by together with described linkage section 211 is directly rotationally connected with by rotating shaft or other attachment structure with described supporting section 212.
Being appreciated that in other embodiments, described unmanned vehicle can include several Flexible Connector (not shown), and one end of described Flexible Connector connects described linkage section 211, and the other end connects described supporting section 212；Described Flexible Connector and the described opposing setting of power set 30, described Flexible Connector is for providing elastic restoring force for described supporting section 212, to assist described supporting section 212 along the rotation of a predetermined direction.When described first horn 21 is in loaded state, described linkage section 211 is identical relative to the direction of described mounting seat 10 with described supporting section 212, i.e. described linkage section 211 is extended substantially in the same direction from described mounting seat 10 with described supporting section 212；When described first horn 21 is in foot rest state, described linkage section 211 is different relative to the direction of described mounting seat 10 from described supporting section 212, i.e. arrange in a predetermined angle between described linkage section 211 and described supporting section 212.
Described power set 30 could alter that its relative to described mounting seat 10 towards.Described power set 30 include motor 31 and are arranged at the propeller 32 on described motor 31, and the rotation that described motor 31 is described propeller 32 provides power.Described power set 30 by regulate the rotating speed of described motor 31 with change its relative to described mounting seat 10 towards.Described propeller 32 includes blade 321.Turning to of the described blade 321 of the described power set 30 being arranged on described first horn 21 is different from turning to of the described blade 321 of the described power set 30 being arranged on described second horn 22, to offset gyroscopic effect and air force moment of torsion effect.
nullIn present embodiment，The motor 31 of the described power set 30 being arranged on described first horn 21 is small machine relative to the motor 31 of the described power set 30 being arranged on described second horn 22，The power of the motor 31 of the described power set 30 being namely arranged on described first horn 21 is less than the power of the motor 31 of the described power set 30 being arranged on described second horn 22，Described small machine rotates to drive described supporting section 212 to launch for driving the described blade 321 of correspondence，And the flight for described unmanned vehicle provides flying power to assist the flight of described unmanned vehicle，Or described self rotating speed of small machine adjustment make the relatively described linkage section 211 of described supporting section 212 tilt and as leg carry described unmanned vehicle weight，Described unmanned vehicle is made to have enough power when there being leg，And extra foot rest driving mechanism need not be set，Simplify structure，Alleviate the overall weight of described unmanned vehicle；It is arranged on the main power source that described power set 30 are described unmanned vehicle on described second horn 22, is arranged on the auxiliary power source that power set 30 are described unmanned vehicle on described first horn 21.
Described power set 30 are by control signal control.Described unmanned vehicle also includes controller (not shown), and described controller controls the instruction that described unmanned vehicle responds the user side of described unmanned vehicle, and generates and sends the described control signal described power set 30 to correspondence according to described instruction.It is appreciated that, in other embodiments, described unmanned vehicle could be included for detecting the sensing component (not shown) of the deformation state of described first horn 21, described controller responds the sensitive information of described sensing component, and generates and sends described control signal to described power set 30 according to described sensitive information.
Described exchanging structure 40 includes fixed part 41, movable part 42, rotating shaft 43, sleeve 44 and elastic component 45, and described fixed part 41 is rotatably connected at described movable part 42 by described rotating shaft 43.Described fixed part 41 is connected to described linkage section 211 one end away from described mounting seat 10, and described movable part 42 is connected to one end of the contiguous described mounting seat 10 of described supporting section 212.Described elastic component 45 is enclosed within described rotating shaft 43 and between described fixed part 41 and described movable part 42.One end of described elastic component 45 supports on described fixed part 41, and the other end supports on described movable part 42.Described sleeve 44 is enclosed within described rotating shaft 43, and described sleeve 44 houses described rotating shaft 43 and described rotating shaft 43 is positioned on described fixed part 41.
One end of described fixed part 41 offers holding tank 411, and described holding tank 411 is used for housing described rotating shaft 43, the described elastic component of part 45 and the described movable part 42 of part.Described fixed part 41 is further opened with the first axis hole 412 being connected with described holding tank 411, and described first axis hole 412 is used for housing the described sleeve of part 44 and described rotating shaft 43.In present embodiment, the quantity of described first axis hole 412 is two.The other end of described fixed part 41 offers the first mating holes 413, and one end of described linkage section 211 is arranged in described first mating holes 413, makes described linkage section 211 socket-connect with described fixed part 41.
One end of described movable part 42 offers accepting groove 421 and the second axis hole 422 being connected with described accepting groove 421, and described accepting groove 421 is used for housing the described rotating shaft 43 of part.In present embodiment, the quantity of described second axis hole 422 is two.The other end of described movable part 42 offers the second mating holes 423, and described supporting section 212 is arranged in described second mating holes 423, makes described supporting section 212 socket-connect with described movable part 42.
Described rotating shaft 43 is arranged in described first mating holes 413 and described second mating holes 423, makes described fixed part 41 be rotationally connected with described movable part 42.Described sleeve 44 is enclosed within the end of described rotating shaft 43, and described elastic component 45 is enclosed within described rotating shaft 43.
When described unmanned vehicle is in landing state, described elastic component 45 is original state, and described supporting section 212 tilts relative to described linkage section 211, and the angle formed between described linkage section 211 and described supporting section 212 is acute angle；When described unmanned vehicle is changed into state of flight by landing state, the motor 31 of the described power set 30 being arranged on described supporting section 212 drives described propeller 32 to rotate, to drive described supporting section 212 to rotate along with described predetermined direction opposite direction, described supporting section 212 gradually spreads out relative to described linkage section 211, until described supporting section 212 extends substantially along same direction with described linkage section 211, there is elastic deformation in described elastic component 45.When described unmanned vehicle needs to be converted to landing state by state of flight, described elastic component 45 recovers elastic deformation gradually, and described elastic component 45 is used for providing elastic restoring force to described supporting section 212 to assist described supporting section 212 to rotate along described predetermined direction；Simultaneously, described elastic component 45 makes described first horn 21 overall in introversion state, to prevent described first horn 21 from serving as when leg carries the weight of described unmanned vehicle to while marking, it is ensured that stability when described first horn 21 carries described unmanned vehicle and reliability.
Described auxiliary supports 50 is arranged on described supporting section 212 one end away from described mounting seat 10.Sleeved part 51 that described auxiliary supports 50 includes housing described supporting section 212 and to the extension 52 extended away from described sleeved part 51.Described extension 52 may be located at the same side or the not homonymy of described supporting section 212 with corresponding described power set 30.Described extension 52 is for ensureing stablizing when described first horn 21 supports described unmanned vehicle；When described extension 52 is positioned at the same side of described supporting section 212 with corresponding described power set 30, described extension 52 is additionally operable to protect described power set 30.It is arranged on the contiguous described auxiliary supports 50 of the described power set 30 on described first horn 21 to arrange.In present embodiment, described auxiliary supports 50 can produce elastic deformation, and it is used for cushioning described supporting section 212 impact force during the landing of described unmanned vehicle.It is appreciated that, in other embodiments, can omitting described auxiliary supports 50, described first horn 21 is perpendicular to the area of the cross section of described first horn 21 length direction away from the area of one end of described mounting seat 10 more than the remainder of described first horn 21.
Described power set 30 by regulate described motor 31 rotating speed change its relative to described mounting seat 10 towards.When described unmanned vehicle is in state of flight, described power set 30 provide flying power for described unmanned vehicle.Described power set 30 regulate the speed of described motor 31, described supporting section 212 rotates towards the direction deviating from the described power set 30 being arranged on described second horn 22 around corresponding described rotating shaft 43 under the elastic restoring force effect of gravity and described elastic component 45, described unmanned vehicle is in landing state, and described first horn 21 carries the weight of described unmanned vehicle as leg.Described first horn 21 can be provided simultaneously with the function of horn and leg, saves leg so that the weight of described unmanned vehicle is less, simple in construction.In present embodiment, described second horn 22 cannot function as leg and supports the weight of described unmanned vehicle.It is appreciated that, in other embodiments, described unmanned vehicle can include auxiliary member, such as spring damper, described auxiliary member, for assisting the rotation relative to described linkage section 211 of the described supporting section 212, makes described first horn 21 carry the weight of described unmanned vehicle as leg.
Described unmanned vehicle also includes the The Cloud Terrace (not shown) being arranged on fuselage and the load (not shown) being arranged on described The Cloud Terrace, and described The Cloud Terrace could alter that the described load direction relative to described mounting seat 10.
Above-mentioned unmanned vehicle, described first horn can deform relative to described mounting seat, and deformation state includes loaded state and foot rest state, when described unmanned vehicle flight, described first horn is in loaded state, makes described power set provide flying power for described unmanned vehicle；When described unmanned vehicle lands, described first horn is in foot rest state, makes described first horn use as leg.Described first horn can be provided simultaneously with the function of horn and leg, saves leg so that the overall weight of described unmanned vehicle is relatively light, and structure is by a relatively simple.
Additionally; those skilled in the art will be appreciated that; embodiment above is intended merely to explanation this utility model; and it is not used as to restriction of the present utility model; as long as within spirit of the present utility model, above example is made suitably change and change all drops within the scope that this utility model claims.
Claims (23)
1. a unmanned vehicle, it includes mounting seat and the multiple horns being connected with described mounting seat, the plurality of horn includes the first horn, described first horn is provided with power set, it is characterized in that: described first horn can deform relative to described mounting seat, and deformation state includes loaded state and foot rest state, when described unmanned vehicle flight, described first horn is in loaded state, makes described power set provide flying power for described unmanned vehicle；When described unmanned vehicle lands, described first horn is in foot rest state, makes described first horn use as leg.
2. unmanned vehicle as claimed in claim 1, it is characterised in that: described power set include motor and are arranged at the propeller on described motor, and the rotation that described motor is described propeller provides power；And/or,
The quantity of described first horn is multiple, and multiple described first horns are symmetrical arranged.
3. unmanned vehicle as claimed in claim 1, it is characterised in that: described first horn could alter that its bearing of trend relative to described mounting seat at least partially.
4. unmanned vehicle as claimed in claim 3, it is characterized in that: described power set are arranged at described first horn one end away from described mounting seat, described power set can drive described first horn deformation, to change at least some of bearing of trend relative to described mounting seat of described first horn.
5. unmanned vehicle as claimed in claim 4, it is characterised in that: described power set can drive described first horn to be deformed into described loaded state from described foot rest state.
6. unmanned vehicle as claimed in claim 4, it is characterised in that: during described first horn deformation, it is possible to change described power set relative to described mounting seat towards.
7. unmanned vehicle as claimed in claim 1, it is characterized in that: described first horn is additionally provided with deformation power set, described deformation power set can drive at least some of rotation of described first horn, to change at least some of bearing of trend relative to described mounting seat of described first horn；And/or,
Described first horn is perpendicular to the area of the cross section of the length direction of described first horn away from the area of one end of described mounting seat more than the remainder of described first horn.
8. unmanned vehicle as claimed in claim 1, it is characterized in that: described first horn is connected to an auxiliary supports away from one end of described mounting seat, when described first horn carries the weight of described unmanned vehicle as leg, described auxiliary supports, for abutting with landing face, makes described first horn be stablely supported on described landing face.
9. unmanned vehicle as claimed in claim 8, it is characterised in that: can there is elastic deformation in described auxiliary supports, to cushion described first horn impact force.
10. unmanned vehicle as claimed in claim 8, it is characterized in that: described auxiliary supports includes housing the sleeved part of described first horn one end and along the axial vertically extending extension of described sleeved part, stability when described extension is in landing state for ensureing described unmanned vehicle.
11. unmanned vehicle as claimed in claim 10, it is characterised in that: being arranged on described auxiliary supports on described first horn and described power set and be positioned at the homonymy of described first horn, described extension can protect described power set.
12. unmanned vehicle as claimed in claim 1, it is characterised in that: described unmanned vehicle includes controller, and described controller can produce and send control signals to described power set, to control described power set.
13. unmanned vehicle as claimed in claim 12, it is characterised in that: described controller controls the instruction that described unmanned vehicle responds the user side of described unmanned vehicle, and generates and sends described control signal to described power set according to described instruction；Or,
Described unmanned vehicle also includes the sensing component of the deformation state for detecting described first horn, and described controller generates and sends described control signal to described power set according to the sensitive information that described sensing component senses.
14. unmanned vehicle as claimed in claim 1, it is characterized in that: described first horn includes linkage section and the supporting section being rotationally connected with described linkage section, described supporting section can rotate relative to described linkage section, so that described supporting section can use as leg.
15. unmanned vehicle as claimed in claim 14, it is characterised in that: described unmanned vehicle also includes exchanging structure, and described exchanging structure is rotationally connected described linkage section and described supporting section；Described exchanging structure is for limiting the described supporting section slewing area relative to described linkage section.
16. unmanned vehicle as claimed in claim 15, it is characterised in that: described exchanging structure includes elastic component, and one end of described elastic component connects described linkage section, and the other end connects described supporting section, is used for providing an elastic restoring force to described supporting section.
17. unmanned vehicle as claimed in claim 16, it is characterized in that: described elastic component is arranged at the not homonymy of corresponding described first horn with corresponding described power set, described supporting section can rotate along a predetermined direction under described elastic restoring force effect, simultaneously, when described unmanned vehicle is in landing state, described elastic component makes described first horn entirety be introversion state.
18. unmanned vehicle as claimed in claim 17, it is characterized in that: described supporting section can rotate relative to described mounting seat along described predetermined direction under described elastic restoring force and action of gravity, carry the weight of described unmanned vehicle using the leg as described unmanned vehicle；Described supporting section rotates with described predetermined direction opposite direction along one relative to described linkage section, to allow described power set to provide flying power for described unmanned vehicle.
19. unmanned vehicle as claimed in claim 1, it is characterised in that: the plurality of horn also includes the second horn；The length of described first horn is more than the length of described second horn.
20. unmanned vehicle as claimed in claim 19, it is characterised in that: the quantity of described first horn is equal with the quantity of described second horn, and described second horn is arranged alternately along the periphery of described mounting seat successively with described first horn.
21. unmanned vehicle as claimed in claim 19, it is characterised in that: described second horn is provided with described power set, is arranged on the power set on described second horn for providing flying power for this unmanned vehicle.
22. unmanned vehicle as claimed in claim 21, it is characterised in that: the power of the described power set being arranged on described first horn is less than the power of the described power set being arranged on described second horn.
23. a unmanned vehicle, it includes mounting seat and is connected to multiple horns of described mounting seat, each described horn is provided with power set, described power set can provide flying power for the flight of described unmanned vehicle, it is characterized in that: the second horn that the plurality of horn includes multiple first horn and multiple and the plurality of first horn is arranged alternately, the length of described first horn is more than the length of described second horn；Described first horn can deform, and deformation state includes loaded state and foot rest state, and when described unmanned vehicle flight, described first horn is in loaded state, makes described power set provide flying power for described unmanned vehicle；When described unmanned vehicle lands, described first horn is in foot rest state, makes described first horn use as leg；
Wherein, the described power set being arranged on described second horn provide main flying power for described unmanned vehicle；It is arranged on the described power set on described first horn and can provide flying power for described unmanned vehicle, or drive described first horn to rotate so that described first horn deforms.
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| CN201620091515.1U CN205381395U (en) | 2016-01-29 | 2016-01-29 | Unmanned aerial vehicle |
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| CN201620091515.1U CN205381395U (en) | 2016-01-29 | 2016-01-29 | Unmanned aerial vehicle |
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| CN106240813A (en) * | 2016-08-15 | 2016-12-21 | 张琬彬 | A kind of unmanned plane rotor anti-collision structure |
| WO2017128318A1 (en) * | 2016-01-29 | 2017-08-03 | SZ DJI Technology Co., Ltd. | Uav with transformable arms |
| WO2018076470A1 (en) * | 2016-10-27 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN107985574A (en) * | 2017-11-22 | 2018-05-04 | 安徽天鹰兄弟无人机科技创新有限公司 | A kind of auxiliary liter of unmanned plane of buoyancy |
| CN109305350A (en) * | 2018-11-05 | 2019-02-05 | 深圳市金鑫城纸品有限公司 | A kind of quadrotor drone |
| CN109923035A (en) * | 2017-08-30 | 2019-06-21 | 深圳市大疆创新科技有限公司 | The horn component and unmanned vehicle of unmanned vehicle |
-
2016
- 2016-01-29 CN CN201620091515.1U patent/CN205381395U/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
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| WO2017128318A1 (en) * | 2016-01-29 | 2017-08-03 | SZ DJI Technology Co., Ltd. | Uav with transformable arms |
| US10549846B2 (en) | 2016-01-29 | 2020-02-04 | SZ DJI Technology Co., Ltd. | UAV with transformable arms |
| CN105947208A (en) * | 2016-05-04 | 2016-09-21 | 无锡觅睿恪科技有限公司 | Multi-axis unmanned aerial vehicle |
| CN106240813A (en) * | 2016-08-15 | 2016-12-21 | 张琬彬 | A kind of unmanned plane rotor anti-collision structure |
| WO2018076470A1 (en) * | 2016-10-27 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN109153439A (en) * | 2016-10-27 | 2019-01-04 | 深圳市大疆创新科技有限公司 | Unmanned vehicle |
| CN109153439B (en) * | 2016-10-27 | 2022-05-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| CN109923035A (en) * | 2017-08-30 | 2019-06-21 | 深圳市大疆创新科技有限公司 | The horn component and unmanned vehicle of unmanned vehicle |
| CN107985574A (en) * | 2017-11-22 | 2018-05-04 | 安徽天鹰兄弟无人机科技创新有限公司 | A kind of auxiliary liter of unmanned plane of buoyancy |
| CN109305350A (en) * | 2018-11-05 | 2019-02-05 | 深圳市金鑫城纸品有限公司 | A kind of quadrotor drone |
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