CN205770109U - Housing assembly and use the unmanned plane of this housing assembly - Google Patents
Housing assembly and use the unmanned plane of this housing assembly Download PDFInfo
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- CN205770109U CN205770109U CN201620584001.XU CN201620584001U CN205770109U CN 205770109 U CN205770109 U CN 205770109U CN 201620584001 U CN201620584001 U CN 201620584001U CN 205770109 U CN205770109 U CN 205770109U
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- horn
- joint portion
- lining
- housing assembly
- frame
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- 238000010586 diagram Methods 0.000 description 2
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- 235000007164 Oryza sativa Nutrition 0.000 description 1
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Abstract
A kind of housing assembly, including frame and horn, described horn is connected with one end of described frame, it is provided with power set on described horn, described frame is connected with described horn by a joint portion, and one end, described joint portion is connected with described gantry rotation, and the other end is set on described horn, being provided with the lining with damping action between described joint portion and described horn, described lining supports between described horn outer surface and described joint portion inner surface.This utility model also provides for a kind of unmanned plane using this housing assembly.Described housing assembly and unmanned plane arrange the lining of tool damping action at the binding site of horn Yu frame, it is possible to be delivered in frame the intensity of vibration during reducing aircraft flight, also ensure that the technical problem of the preferable maneuverability of aircraft simultaneously.
Description
Technical field
This utility model relates to a kind of housing assembly, particularly relates to a kind of housing assembly for unmanned plane and uses this machine
The unmanned plane of frame assembly.
Background technology
Unmanned vehicle is mainly made up of housing assembly, flight control system, power unit and load at present, and housing assembly is main
Body, remaining each several part all passes through frame and installs fixing intercoupling.Wherein power unit be several high speed rotating motor and
Blade, due to some defect in motor, the power imbalance of blade and rack construction, aircraft can be held in flight course
Continuous vibration.Cause flight control system can not collect correct attitude information if this vibration intensity crosses conference, thus cause flight
Device and entrained loaded work piece are abnormal, affect the normal use of user.
Utility model content
In view of this, it is necessary to provide a kind of can the preferably housing assembly of vibration damping and unmanned plane.
A kind of housing assembly, including frame and horn, described horn is connected with one end of described frame, on described horn
Being provided with power set, described frame is connected with described horn by a joint portion, one end, described joint portion and described frame
Being rotationally connected, the other end is set on described horn, is provided with and has damping action between described joint portion and described horn
Lining, described lining supports between described horn outer surface and described joint portion inner surface.
Further, described lining is set on described horn outer surface, and described lining is towards table outside described horn
The medial wall in face is provided with groove.
Further, described lining is provided with at least two fins towards the medial wall of described horn outer surface, adjacent convex
Described groove is formed between rib.
Further, the grease of tool damping action it is filled with in described groove.
Further, medial wall, described joint portion is provided with the groove corresponding to described lining, the shape of described groove
Adapt with described lining with position.
Further, described joint portion includes the first joint portion and the second joint portion that can be separated from each other, described first
Joint portion is arranged on described Frame end, can match with described first joint portion fixing connection and shape in described second joint portion
Becoming a substantially receiving space in cylinder barrel shaped, described horn is fixed in described receiving space.
Further, described lining quantity is even number, and the corresponding setting of each two lining is to form a substantial cylindrical
Enclose and be located on described horn lateral wall.
Further, the quantity of described lining is four, is separately positioned on medial wall and the institute at both ends, described joint portion
State between the lateral wall of horn.
Further, described joint portion includes the first joint portion, the face matched in described first joint portion with described horn
For cambered surface.
Further, the quantity of described lining is multiple, arranges along described horn bearing of trend uniform intervals, and institute relatively
State the asymmetric setting of horn bearing of trend.
Further, described lining is the cylindrical shape of hollow, and described horn includes connecting separated from each other
First horn and the second horn.
Further, the position that described joint portion is set in described first horn and described second horn combines.
Further, described joint portion includes that the cylindrical drum of hollow, the cylindrical drum of described hollow can be set in described machine
On arm, fixing horn is to described frame.
Further, the quantity of described lining is 2, is separately positioned on the medial wall at both ends, described joint portion with described
Between the lateral wall of horn.
Further, described lining is towards the one side substantially cambered surface of described horn outer surface so that described lining can
It is set on described horn.
Further, described joint portion is connected to the middle part of described horn, in the two of described horn distal portion relatively
It is respectively arranged with described power set.
A kind of unmanned plane, including central part and housing assembly as above, the close end of described housing assembly is with described
Central part is connected, and described central part is provided with control system, is used for controlling described unmanned plane and moves.
Further, the quantity of described housing assembly is two, and two described housing assemblies are symmetric around described center
Portion is arranged.
Described housing assembly and unmanned plane arrange the lining of tool damping action at the coupling position of horn Yu frame, it is possible to fall
Low aircraft flight course is delivered in frame the intensity of vibration, also ensure that the technology of the preferable maneuverability of aircraft simultaneously
Problem.
Accompanying drawing explanation
Fig. 1 is the axonometric chart of a kind of unmanned plane that this utility model embodiment provides.
Fig. 2 is the partially disassembled state figure of the unmanned plane of this utility model the first embodiment.
Fig. 3 is the state diagram at another visual angle of Fig. 2.
Fig. 4 is the axonometric chart of the lining of this utility model one embodiment.
Fig. 5 is the axonometric chart of the unmanned plane of this utility model the second embodiment.
Fig. 6 is the decomposed figure of the unmanned plane of this utility model the second embodiment.
Fig. 7 is the state diagram at another visual angle of Fig. 6.
Fig. 8 is the axonometric chart of the lining of another embodiment of this utility model.
Main element symbol description
| Unmanned plane | 1 |
| Central part | 10 |
| Housing assembly | 20 |
| Frame | 21 |
| Horn | 22 |
| First horn | 220 |
| Second horn | 222 |
| Joint portion | 30,60 |
| Lining | 40,70 |
| Fin | 400,700 |
| Groove | 402,702 |
| Power unit | 50 |
| First joint portion | 300 |
| Second joint portion | 302,602 |
| Connecting portion | 600 |
| Cylindrical drum | 602 |
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 carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole
Embodiment.Based on the embodiment in this utility model, those of ordinary skill in the art are not under making creative work premise
The every other embodiment obtained, broadly falls into the scope of this utility model protection.
It should be noted that when assembly is referred to as " being fixed on " another assembly, and it can be directly on another assembly
Or assembly placed in the middle can also be there is.When an assembly is considered as " connection " another assembly, and it can be to be directly connected to
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 to be set directly on another assembly or may be simultaneously present assembly placed in the middle.Term as used herein is " vertical
", " level ", "left", "right" and similar statement for illustrative purposes only.
Unless otherwise defined, all of technology used herein and scientific terminology are led with belonging to technology of the present utility model
The implication that the technical staff in territory is generally understood that is identical.At term used in the description of the present utility model it is simply herein
The purpose of specific embodiment is described, it is not intended that in limiting this utility model.Term as used herein " and/or " include
Arbitrary and all of combination of one or more relevant Listed Items.
This utility model provides a kind of unmanned plane, and described unmanned plane can be used for any suitable environment, (example the most aloft
The aircraft mixed with rotor such as rotor craft, Fixed Wing AirVehicle or fixed-wing), in water (example, ship or submarine), on ground
On face (example, motorcycle, automobile, truck, bus, train etc.), in space (example, space shuttle, satellite or detector), or
At underground (such as subway), or the combination in any of above-mentioned environment.
Below in conjunction with the accompanying drawings, embodiments more of the present utility model are elaborated.In the case of not conflicting, under
Feature in the embodiment stated and embodiment can be mutually combined.
Refer to Fig. 1, unmanned plane 1 include housing assembly 20 that central part 10 and multiple and described central part 10 be connected,
And multiple power set 50.Multiple power set 50 are separately positioned on multiple described housing assembly 20.
The central part 10 of described unmanned plane 1 can be used for supporting load.Described load is connectable to appointing of described central part 10
Meaning is suitable for position, such as, the bottom of described central part 10 or downside.Connection between described load and described central part 10 is permissible
It is fixing connection, or, described load can the activity of the most described central part 10.
Described load could be for performing the load of specific function, such as, sensor, emitter, instrument, instrument, behaviour
Vertical device, or other functional devices.Such as, described load can be a video capturing device.In some situations, described image obtains
Fetching puts the camera can being in below described central part 10.Described camera can rotate (such as, logical relative to described central part 10
Cross a carrier or other mounting platforms, concrete such as The Cloud Terrace) to obtain the image at multiple visual angle.
Described power set 50 can be used for making described unmanned plane 1 take off, land, hover, and aloft about three translations
Degree of freedom and three rotary freedom motions.In certain embodiments, described power set 50 can include one or more rotation
Wing (not shown) and drive mechanism (such as motor).Described rotor can include the one or more rotor leaves being connected to a rotating shaft
Sheet.Described rotor blade or rotating shaft can be driven by a suitable drive mechanism and rotate.Although the most described unmanned plane 1
Power set 50 be described as including 4 rotors, but other suitable quantity, type or the deploying of power set are all can
Implement.Such as, described rotor can be one, two, three, five, six, seven, eight or more.Described rotor can
With relative to described unmanned plane 1 level, vertical or other any suitable angles setting.The angle of described rotor can be fixing
Or it is variable.Distance between the described rotorshaft being oppositely arranged can be any appropriately distance, e.g., less than equal to 2
Rice, or less than or equal to 5 meters.Alternatively, described distance can between 40 centimetres to 1 meters, from 10 centimetres to 2 meters, or from
Between 5cm to 5 meter.Described power set 50 can be driven by the most suitable motor, such as direct current generator (example: brush motor
Or brushless electric machine) or alternating current generator.In certain embodiments, described motor can be configured to drive rotor blade.
Control system (such as, flight control system) can be set on described central part 10 and control flying of described unmanned plane 1
OK.In certain embodiments, described control system is based on the most one or more: the position of described unmanned plane 1, described unmanned plane
The number being sensed acquisition towards, the current state of described unmanned plane 1, time or the sensor of described unmanned plane 1 or load of 1
According to, automatically control described unmanned plane 1.
Alternatively or can in combination, described control system can include the receptor being arranged on described unmanned plane 1
Or other communication module, it is used for receiving user instruction, such as, from remote terminal reception user instruction.By described receptor
The described user instruction received is for controlling described power set 50, and described power set 50 are used for driving described unmanned plane to transport
OK, such as take off, fly, spiral or landing etc..
Described housing assembly 20 can be used for carrying described power set 50.Each housing assembly 20 is connected to described central part
One end of 10 is close end, and the other end opposing with described close end is distal portion.
It is understood that described power set 50 also can mount to the most applicable position of described housing assembly 20, example
Described housing assembly 20 distal portion or near as described in the position of distal portion.Alternatively, described power set 50 can be pacified
It is contained in described close end or the position near described close end.Described power set 30 may be mounted at or near described distal portion
About 1/10,1/5,1/4,1/3,1/2,3/4,2/3,4/5, or the position of housing assembly length described in 9/10.In some embodiments
In, described unmanned plane 100 can include any an appropriate number of deformable housing assembly 20, such as, 2,3,4 or more.
In the present embodiment, described unmanned plane 1 includes two housing assemblies 20.Described housing assembly 20 can symmetrically or asymmetrically enclose
Arrange around described central part 10.In the present embodiment, two described housing assemblies 20 are arranged symmetric around described central part 10.Often
One housing assembly 20 can be used for supporting single or multiple power set 50.Described power set 50 can averagely deploying in described frame
On assembly 20.Alternatively, each housing assembly 20 can include the power set 50 of varying number.Alternatively, described frame
Assembly 20 can be connected with described central part 10 rotationally so that the power set 50 on each housing assembly 20 are relative to described
The height adjustable of central part 10.
Each described housing assembly 20 all includes frame 21 and horn 22.Described frame 21 is connected with described central part 10
One end is close end, and the other end opposing with this close end is distal portion, the distal portion of described frame 21 and described horn 22
Being connected, each frame 21 forms an inverted " t " font with corresponding horn 22.In the present embodiment, two described horns 22 are arranged on
It is substantially parallel to each other between the two ends of described central part 10, and two described horns 22.In the present embodiment, the two of described horn 22
End is respectively arranged with power unit 50 described in.
Seeing also shown in Fig. 2 and Fig. 3, described frame 21 is connected by joint portion 30 with described horn 22.Described
The distal portion of described frame 21 is connected to described horn 22 by joint portion 30.In the present embodiment, the distal portion of described frame 21
It is connected to the middle part of described horn 22, two relative distal portion of described horn 22 are respectively arranged with power set
50.In certain embodiments, described joint portion 30 is connected to the distal portion of described frame 21 rotationally, so that described horn
22 can be rotated relative to described frame 21 by described joint portion 30.
Described joint portion 30 includes that the first joint portion 300 and second being fixedly installed on described frame 21 distal portion combines
Portion 302.Described second joint portion 302 can be covered and be located on described horn 22 and can be connected with described first joint portion 300
And fix described horn 22 to described frame 21.Described first joint portion 300 and the second joint portion 300 are respectively half arc knot
Structure, described first joint portion 300 combines with described second joint portion 302 and fixing when being connected, can form a cylindricality and house empty
Between make described horn 22 part be located in this receiving space.Described first joint portion 300 can lead to described second joint portion 302
Cross the fixing connection of the fixing devices such as screw.It is appreciated that in other embodiments, described first joint portion 300 and described the
Two joint portions 302 can also connect by any other suitable connected modes are fixing, such as, snaps connection.
In order to promote effectiveness in vibration suppression, between described horn 22 and described joint portion 30, it is provided with at least one lining 40.Institute
Stating the first joint portion 300 and be provided with the first accepting groove 3000 towards the medial wall of the side of described horn 22, described second combines
Portion 302 arranges the second accepting groove 3020 towards the medial wall of the side of described horn 22.Described first accepting groove 3000 and described
Second accepting groove 3020 shape all adapts with described lining 40 shape, houses described lining 40 in the inner for common.Work as institute
Stating the first joint portion 300 and described second joint portion 302 combines and fixing when connecting, described lining 40 is supported at described machine
Between the medial wall of arm 22 and described first joint portion 300 and described second joint portion 302.
Seeing also shown in Fig. 4, described lining 40 is the partial cylinder shape of hollow, arranges inside described lining 40
Having at least two fins 400, form groove 402 between adjacent fin 400, described groove 402 is used for accommodating oils and fats in the inner.Institute
State lining 40 to be made up of damping material, the most resilient plastics, rubber or nylon material etc..When lining 40 is supported described
Time between joint portion 30 and described horn 22, when there is vibration due to the driving of power set 50 in horn, described vibration warp
By the fat absorption in the lining 40 being arranged between described joint portion 30 and described horn 22 and lining 40 so that via horn
The 22 vibration force impacts being transferred to described frame 21 are substantially reduced, thus reduce the center being arranged on described frame 21 close end
The vibration force impact in portion 10.It is understood that described fin 400 can omit, and can directly arrange inside described lining 40 to
A few groove, is used for accommodating oils and fats in the inner.
Institute in the embodiment shown in Fig. 2 and Fig. 3, between each described horn 22 and corresponding described joint portion 30
The quantity stating lining 40 is 4, and described lining 40 is symmetricly set on described horn 22 two opposite sides.Described first joint portion
300 quantity arranging the first accepting groove 3000 are two, and the second accepting groove 3020 arranged on described second joint portion 302
Quantity is also two.Two described first accepting grooves 3000 are separately positioned on two opposite ends of described first joint portion 300, two
Described second accepting groove 3020 is separately positioned on two opposite ends of described second joint portion 302.It is understood that described first
Accepting groove 3000 and the second accepting groove 3020 may be provided at any of described first joint portion 300 and the second joint portion 302 respectively
Suitable location, such as adjacent distal end portion, close pars intermedia etc..The quantity of described lining 40 is also not necessarily limited to 4, it is also possible to be 2,
6,8 etc., symmetrical and be disposed in an evenly spaced relation on described horn 22 both sides, accordingly, described first groove 3000 and described
The quantity of the second groove 3020 and position also with the corresponding setting of quantity and position of described lining 40.Described lining 40 is alternatively
1,2,3, the varying numbers such as 4, be provided only between horn 22 and described first joint portion 300, when for more than one
Time, can arrange along the bearing of trend uniform intervals of described horn 22 or non-uniform spacing is arranged on described horn 22.
Preferably, the first groove 3000 when the quantity more than one of described lining 40, on described first joint portion 300
Corresponding with the position of the second groove 3020 on described second joint portion 302, lining 40 substantially in 1/2 semicylinder shape, thus
When two relative lining 40 rings are located on the lateral wall of described horn 22, substantially can form a complete cylindrical
Shape.It is understood that described lining 40 can also be less than 1/2 semicylinder, such as 1/3 semicylinder, 2/5 semicylinder
Deng.It is understood that it is second recessed on the first groove 3000 on described first joint portion 300 and described second joint portion 302
The position of groove 3020 can also be not correspond to so that the asymmetric setting of bearing of trend of the described the most described horn of lining 40 22.
It is understood that described second joint portion 302 can be omitted, as long as described first joint portion 300 can be set in
On described horn 22 and described horn 22 can be fixed on described first joint portion 300.Now, described lining 40 is arranged on
Between described first joint portion 300 and described horn 22.The one side that described first joint portion 300 coordinates with described horn 22 is arc
Face structure, thus can be set on described horn 22.In certain embodiments, for avoiding described horn 22 to combine from described first
Portion 300 departs from, it is possible to arranges suitable fixed structure, the such as fixing device such as buckle or screw and fixes described first joint portion
300 and described horn 22.
It is understood that described first groove 3000 and the second groove 3020 can also omit, and at described horn 22
Corresponding position arranges the groove being installed with described lining 40.
Refer to shown in Fig. 5, for the housing assembly structure of this utility model the second embodiment, described housing assembly structure
Substantially similar with the housing assembly structure of the first embodiment, difference is horn and the structure of joint portion and the structure of lining.
Describe for simplifying, be not repeated to describe with the description of the element of identical label in the first embodiment, only describe and implement with first
The part that mode is different.Described frame 21 is connected with horn 22 by joint portion 60.Described horn 22 includes being separated from each other
The first horn 220 and the second horn 222.The close end of described first horn 220 and the close end phase of described second horn 222
Connecting, the mode of connection can be buckle combination, be screwed or the mode such as screw locking.The distal portion of described first horn 220
It is respectively arranged with power set 50 with the distal portion of described second horn 222.
Seeing also shown in Fig. 6 and Fig. 7, described joint portion 60 is arranged on the distal portion of described frame 21, including connecting
Portion 600 and the cylindrical drum 602 of a hollow, described cylindrical drum 602 is set on described horn 22.At described horn 22 and described circle
Column casing 602 is provided with lining 70 between medial wall.Described lining 70 is circular, is set on described horn 22.Described cylindrical drum
602 medial walls are provided with the groove for accommodating this lining 70 corresponding to the position of this lining 70.The quantity of described lining is permissible
It it is 1,2,3,4 or more.When the quantity of described lining 70 is 1, this lining 70 may be provided at described cylindrical drum
The middle part of medial wall.When described lining 70 is 2 or more than 2, can be evenly or unevenly spaced described in being arranged on
Between cylindrical drum medial wall and described horn 22.
See also shown in Fig. 8, described lining 70 substantially cylinder in hollow, its medial wall is provided with fin 700,
Forming groove 702 between adjacent lugs 700, described groove 702 can be used for filling the grease of tool damping.Described lining 70
Similar with described lining 40, damping material can be used to make, such as Elastic plastic-rubber or rubber or nylon etc..The height of described lining 70
Degree, quantity, spacing, position can adjust to meet different damping requirements as required.
It is understood that the horn in described first embodiment can also use such as the second embodiment in separable
Structure, i.e. the first horn and the second horn by being separated from each other form.What the design of such horn structure can promote horn can
Maintainability.
It is understood that the lining in described first embodiment can also use such as the second embodiment in lining
Structure, the most complete hollow circular cylinder structure.The lining of described complete hollow circular cylinder structure can promote damping further
Performance And Reliability.
It is understood that the bush structure in described second embodiment can also use the portion in the first embodiment
Cyclotomy column structure.In other embodiments, described bush structure is also not necessarily limited to described part cylindrical structure or circle
Column structure, it is also possible to be other any suitable shapes, as long as can support in described horn outer surface and described joint portion
Between inner surface, play damping action.
It addition, for the person of ordinary skill of the art, can be made it according to technology of the present utility model design
Its various corresponding changes and deformation, and all these change all should belong to the protection model of this utility model claim with deformation
Enclose.
Claims (18)
1. a housing assembly, including frame and horn, described horn is connected with one end of described frame, and described horn sets
Be equipped with power set, it is characterised in that: described frame is connected with described horn by a joint portion, one end, described joint portion with
Described gantry rotation connects, and the other end is set on described horn, is provided with and has between described joint portion and described horn
The lining of damping action, described lining supports between described horn outer surface and described joint portion inner surface.
2. housing assembly as claimed in claim 1, it is characterised in that: described lining is set on described horn outer surface,
Described lining is provided with groove towards the medial wall of described horn outer surface.
3. housing assembly as claimed in claim 2, it is characterised in that: described lining is towards the inner side of described horn outer surface
Wall is provided with at least two fins, forms described groove between adjacent lugs.
4. housing assembly as claimed in claim 2, it is characterised in that: it is filled with the lubrication of tool damping action in described groove
Fat.
5. housing assembly as claimed in claim 1, it is characterised in that: described joint portion is provided with corresponding to described on medial wall
The groove of lining, shape and the position of described groove adapt with described lining.
6. housing assembly as claimed in claim 1, it is characterised in that: described joint portion includes the first knot that can be separated from each other
Conjunction portion and the second joint portion, described first joint portion is arranged on described Frame end, and described second joint portion can be with described
Matching fixing connection and form a substantially receiving space in cylinder barrel shaped in one joint portion, described horn is fixed on described collecting
In space.
7. housing assembly as claimed in claim 6, it is characterised in that: described lining quantity is even number, each two lining phase
It is correspondingly arranged to be formed a substantial cylindrical to enclose and be located on described horn lateral wall.
8. housing assembly as claimed in claim 7, it is characterised in that: the quantity of described lining is four, is separately positioned on institute
State between the medial wall at both ends, joint portion and the lateral wall of described horn.
9. housing assembly as claimed in claim 1, it is characterised in that: described joint portion includes the first joint portion, described first
The face matched with described horn in joint portion is cambered surface.
10. housing assembly as claimed in claim 1, it is characterised in that: the quantity of described lining is multiple, prolongs along described horn
Stretch direction uniform intervals to arrange, and the most described asymmetric setting of horn bearing of trend.
11. housing assemblies as claimed in claim 1, it is characterised in that: described lining is the cylindrical shape of hollow, described machine
Arm includes the first horn and the second horn that can connect separated from each other.
12. housing assemblies as claimed in claim 10, it is characterised in that: described joint portion is set in described first horn and institute
State the position that the second horn combines.
13. housing assemblies as claimed in claim 10, it is characterised in that: described joint portion includes the cylindrical drum of hollow, described
The cylindrical drum of hollow can be set on described horn fixing horn to described frame.
14. housing assemblies as claimed in claim 10, it is characterised in that: the quantity of described lining is 2, is separately positioned on institute
State between the medial wall at both ends, joint portion and the lateral wall of described horn.
15. housing assemblies as claimed in claim 1, it is characterised in that: described lining is towards the one of described horn outer surface
Face substantially cambered surface so that described lining can be set on described horn.
16. housing assemblies as claimed in claim 1, it is characterised in that: described joint portion is connected to the pars intermedia of described horn
Position, the two of described horn distal portion relatively is respectively arranged with described power set.
17. 1 kinds of unmanned planes, including central part and the housing assembly as described in any one of claim 1 ~ 15, described housing assembly
Close end be connected with described central part, described central part is provided with control system, is used for controlling described unmanned plane and moves.
18. unmanned planes as claimed in claim 16, it is characterised in that: the quantity of described housing assembly is two, described in two
Housing assembly is arranged symmetric around described central part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620584001.XU CN205770109U (en) | 2016-06-16 | 2016-06-16 | Housing assembly and use the unmanned plane of this housing assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620584001.XU CN205770109U (en) | 2016-06-16 | 2016-06-16 | Housing assembly and use the unmanned plane of this housing assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205770109U true CN205770109U (en) | 2016-12-07 |
Family
ID=58132645
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620584001.XU Expired - Fee Related CN205770109U (en) | 2016-06-16 | 2016-06-16 | Housing assembly and use the unmanned plane of this housing assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205770109U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017214934A1 (en) * | 2016-06-16 | 2017-12-21 | 深圳市大疆创新科技有限公司 | Frame assembly and unmanned aerial vehicle using frame assembly |
| WO2018196298A1 (en) * | 2017-04-26 | 2018-11-01 | 深圳市道通智能航空技术有限公司 | Arm, power assembly and unmanned aerial vehicle |
| US10730619B2 (en) | 2017-04-26 | 2020-08-04 | Autel Robotics Co., Ltd. | Arm and unmanned aerial vehicle |
| CN113335516A (en) * | 2021-06-19 | 2021-09-03 | 国网浙江省电力有限公司浦江县供电公司 | Be applied to unmanned aerial vehicle that electric power cruises |
-
2016
- 2016-06-16 CN CN201620584001.XU patent/CN205770109U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017214934A1 (en) * | 2016-06-16 | 2017-12-21 | 深圳市大疆创新科技有限公司 | Frame assembly and unmanned aerial vehicle using frame assembly |
| WO2018196298A1 (en) * | 2017-04-26 | 2018-11-01 | 深圳市道通智能航空技术有限公司 | Arm, power assembly and unmanned aerial vehicle |
| US10730619B2 (en) | 2017-04-26 | 2020-08-04 | Autel Robotics Co., Ltd. | Arm and unmanned aerial vehicle |
| CN113335516A (en) * | 2021-06-19 | 2021-09-03 | 国网浙江省电力有限公司浦江县供电公司 | Be applied to unmanned aerial vehicle that electric power cruises |
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