CN205872439U - Retractable unmanned aerial vehicle - Google Patents
Retractable unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205872439U CN205872439U CN201620852792.XU CN201620852792U CN205872439U CN 205872439 U CN205872439 U CN 205872439U CN 201620852792 U CN201620852792 U CN 201620852792U CN 205872439 U CN205872439 U CN 205872439U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- extension type
- type unmanned
- chute
- slide block
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model discloses a retractable unmanned aerial vehicle, be equipped with the organism of spout and be used for launching and the flexible arm that shrinks etc. The rotor including rotor, inside. The utility model discloses flexible arm is deployable to the size of flying in the use, and collapsible a grade unmanned aerial vehicle compares flexible arm with ordinary consumption to accomodating the size when not using, the utility model discloses change to accomodate and carry, can carry fine protection paddle of in -process and foot rest etc. Simultaneously.
Description
Technical field
This utility model relates to unmanned plane field, is specially a kind of extension type unmanned plane.
Background technology
Along with progress and the growth in the living standard of technology, unmanned plane enters daily life gradually.Traditional nothing
Man-machine being often made up of some groups of fixed horns and foot rest, small product size is relatively big, not readily portable, and in carrying process
In well protect owing to blade be cannot be carried out, generally require and be equipped with special case and bag, this adds the burden gone out undoubtedly；
Simultaneously because the feature of unmanned plane product, its stability requirement to structure in flight course is higher, but, the most on the market
More existing Portable unmanned machines, because the stability of movable part is inadequate, cause flight effect poor.Therefore, to unmanned plane
The portability of product improves, it is provided that a kind of reliable, stable Portable unmanned machine, just can meet the demand in market.
Utility model content
The purpose of this utility model be in order to overcome above-mentioned not enough provide a kind of reliable, stable and portable extension type without
Man-machine.
This utility model include rotor 02, inside be provided with chute 15 body 01 and for rotor 02 is launched and
The telescopic arm 03 shunk, rod member 10 one end of described telescopic arm 03 is provided with slide block 11, and described slide block 11 is located in chute 15, described
Rotor 02 includes that rod member 10 other end described in oar folder 06, blade 07 and motor 08 is provided with motor cabinet 12, and described motor 08 is arranged on
On motor cabinet 12, described blade 07 is arranged on motor 08 by oar folder 06.
Further, described chute 15 inwall is provided with a plurality of convex tendon 16, and described chute 15 is respectively arranged at two ends with the first locking
Shell fragment 17 and the second locking spring plate 32, described slide block 11 is provided with and coordinates with the first locking spring plate 17 and the second locking spring plate 32
Latch recess 14.
Further, also including foot rest, two legs of described foot rest 04 are provided with rotating shaft 19, described body 01 both sides set
Foot rest shaft hole 20, described rotating shaft 19 is had to be arranged in foot rest shaft hole 20；Buckle 22 it is provided with, separately in the rotating shaft 19 of one leg
It is provided with in the rotating shaft 19 of one leg for increasing foot rest 04 damping abrasion resistant cushion rubber 21 of resistance during rotary folding.
Further, also include the The Cloud Terrace 05 being arranged on bottom body 01, described The Cloud Terrace 05 is provided with the first buckle 23,
One draw-in groove 24, locating dowel 25 and line joint 26, be provided with second draw-in groove the 27, second buckle 28, determine bottom described body 01
Hole 29, position and plinth 30, described first buckle 23 is arranged in the second draw-in groove 27, and described second buckle 28 is arranged on first
In draw-in groove 24, described locating dowel 25 is arranged in hole 29, location, and described line joint 26 is connected with plinth 30.
Further, the cross section of described slide block 11 and chute 15 is polygon.
Further, described convex tendon 16 increases along chute 15 gradual change the most from inside to outside.
Further, described slide block (11) and motor cabinet (12) at least one of which are formed in one with rod member (10).
Further, described body 01 is provided with multiple blade fixing hole 09.
Further, described blade 07 afterbody is provided with pin hole 31, is provided with pivot pin 18, described blade in described pin hole 31
07 is connected the collapsible blade of formation by pin hole 31 and pivot pin 18 with oar folder 06.
Further, described slide block (11) and motor cabinet (12) at least one of which are that tightening is connected with rod member (10).
This utility model in use telescopic arm is deployable to flight size, and when not using, telescopic arm may contract to receive
Receiving size, compared with ordinary consumption level unmanned plane, this utility model is more easily contained to be carried, simultaneously can in carrying process very well
Protection blade and foot rest etc..
Accompanying drawing explanation
Fig. 1 is schematic diagram when being expanded to state of flight of the present utility model；
Fig. 2 is schematic diagram when being contracted to receiving state of the present utility model；
Fig. 3 is the stretching structure exploded view of utility model of the present invention；
Fig. 4 is telescopic arms schematic diagram of the present utility model；
Fig. 5 is foot rest structure schematic diagram of the present utility model；
Fig. 6 is that schematic diagram received by foot rest of the present utility model；
Fig. 7 is that The Cloud Terrace of the present utility model dismounts schematic diagram；
Fig. 8 is enlarged diagram at the A of Fig. 5；
Fig. 9 is enlarged diagram at the B of Fig. 5.
Detailed description of the invention
Below in conjunction with the accompanying drawings and embodiment further illustrates this utility model.
Embodiment: this utility model includes body 01, rotor 02, telescopic arm 03, foot rest 04, The Cloud Terrace 05, power supply and phase
Close control circuit；Each telescopic arm 03 one end is provided with slide block 11, and is arranged in the chute 15 of internal body by slide block 11,
Each telescopic arm 03 other end is provided with one group of rotor 02, and rotor 02 is made up of one group of oar folder 06, blade 07 and motor 08；Blade
07 afterbody is provided with pin hole 31, is connected the collapsible blade of formation by pivot pin 18 with oar folder 06；In use telescopic arm
03 is deployable to flight size such as Fig. 1, and when not using, telescopic arm 03 may contract to receive size such as Fig. 2.
As shown in Fig. 1～2, body 01 is provided with the blade fixing hole 09 of some fixed blades；In use, oar
Leaf 07 is deployable to state of flight；When not using, blade 07 is collapsible, and inserts in the blade fixing hole 09 on body.
As it is shown on figure 3, telescopic arm 03 is made up of rod member 10, slide block 11 and motor cabinet 12, commonly use as this utility model
A kind of form, slide block 11 and motor cabinet 12 are respectively placed in rod member 10 two ends, and use tightening to connect；Slide block 11 cross section is polygon
Shape, slide block 11 is provided with latch recess 14；As another kind of form of the present utility model, slide block 11 and motor cabinet 12 also can be with
Rod member 10 uses one-body molded；As other forms of the present utility model, slide block 11 uses tightening to be connected with rod member 10 one end, with
Time motor cabinet 12 use one-body molded or other connected modes with rod member 10 other end；Or slide block 11 uses with rod member 10 one end
One-body molded, motor cabinet 12 uses tightening to be connected or other connected modes with rod member 10 other end simultaneously.
As shown in figs. 34, body 01 is internally provided with 4 chutes 15, and chute 15 cross section is corresponding with slide block 11 many
Limit shape, can limit the rotation of rod member；Being provided with a plurality of convex tendon 16 on chute 15, chute 15 two ends are respectively arranged with locking spring plate
17；Convex tendon 16 gradual change from inside to outside is increased, and when telescopic arm 03 outwards launches, is clamped by telescopic arm 03 by convex tendon 16；Stretching
When contracting arm 03 is expanded to flight size, the latch recess 14 that the locking spring plate 17 that chute 15 outer end is arranged will buckle on slide block 11,
Limit moving axially of expansion link 03；When telescopic arm 03 is retracted to receive size, the shell fragment 32 that chute the inner is arranged will buckle into
Latch recess 14 on slide block 11, limits moving axially of expansion link.
As shown in Fig. 5～6, foot rest 04 is two groups of U-shaped foot rests varied in size, and two combined supports can embedded be placed；Often organize foot
It is provided with rotating shaft 19 on frame, is installed on the foot rest shaft hole 20 of body both sides by rotating shaft；Damping abrasion resistant it is provided with in rotating shaft
Cushion rubber 21, can make the increase foot rest 04 resistance during rotary folding, landing, air crash to unmanned plane to a certain extent enter
Row buffering, protection body 01 and The Cloud Terrace 05；Buckle 22 it is provided with on foot rest 04；In use foot rest 04 is deployable to flight
Size, and locked by buckle 22；May contract to when not using receive size.
As it is shown in fig. 7, be provided with first buckle the 23, first draw-in groove 24, locating dowel 25 and line joint 26 on The Cloud Terrace 05；
Corresponding, organism bottom is provided with second draw-in groove the 27, second buckle 28, hole 29, location and plinth 30；The Cloud Terrace 05 exists
Installed to body 01 by above-mentioned buckle notch during use, and realized the circuit of body 01 and The Cloud Terrace 05 by joint
Connect.
Above-described embodiment is this utility model preferably embodiment, but embodiment of the present utility model is not by above-mentioned
The restriction of embodiment, the change made under other any spirit without departing from the present invention and principle, modify, substitute, group
Close, simplify, all should be the substitute mode of equivalence, within being included in protection domain of the present utility model, other unaccounted portion
Divide and be prior art.
Claims (10)
1. an extension type unmanned plane, is provided with the body (01) of chute (15) and for rotation including rotor (02), inside
The wing (02) carries out the telescopic arm (03) launching and shrinking, it is characterised in that rod member (10) one end of described telescopic arm (03) is provided with cunning
Block (11), described slide block (11) is located in chute (15), and described rotor (02) includes oar folder (06), blade (07) and motor
(08), described rod member (10) other end is provided with motor cabinet (12), and described motor (08) is arranged on motor cabinet (12), described blade
(07) it is arranged on motor (08) by oar folder (06).
Extension type unmanned plane the most according to claim 1, it is characterised in that described chute (15) inwall is provided with a plurality of
Convex tendon (16), described chute (15) is respectively arranged at two ends with the first locking spring plate (17) and the second locking spring plate (32), described slide block
(11) latch recess (14) coordinated with the first locking spring plate (17) and the second locking spring plate (32) it is provided with on.
Extension type unmanned plane the most according to claim 2, it is characterised in that also include foot rest (04), described foot rest (04)
Two legs on be provided with rotating shaft (19), described body (01) both sides are provided with foot rest shaft hole (20), and described rotating shaft (19) is pacified
It is contained in foot rest shaft hole (20)；It is provided with buckle (22) in the rotating shaft (19) of one leg, the rotating shaft (19) of another leg sets
It is equipped with the damping abrasion resistant cushion rubber (21) for increasing foot rest (04) resistance during rotary folding.
Extension type unmanned plane the most according to claim 3, it is characterised in that also include being arranged on body (01) bottom
The Cloud Terrace (05), described The Cloud Terrace (05) is provided with the first buckle (23), the first draw-in groove (24), locating dowel (25) and line joint
(26), described body (01) bottom is provided with the second draw-in groove (27), the second buckle (28), hole, location (29) and plinth
(30), described first buckle (23) is arranged in the second draw-in groove (27), and described second buckle (28) is arranged on the first draw-in groove (24)
In, described locating dowel (25) is arranged in hole, location (29), and described line joint (26) is connected with plinth (30).
Extension type unmanned plane the most according to claim 4, it is characterised in that cutting of described slide block (11) and chute (15)
Face is polygon.
Extension type unmanned plane the most according to claim 5, it is characterised in that described convex tendon (16) is along chute (15) longitudinally
Gradual change is increased from inside to outside.
Extension type unmanned plane the most according to claim 6, it is characterised in that described slide block (11) and motor cabinet (12) its
In at least one is formed in one with rod member (10).
Extension type unmanned plane the most according to claim 7, it is characterised in that described body is provided with multiple oar on (01)
Leaf fixing hole (09).
Extension type unmanned plane the most according to claim 8, it is characterised in that described blade (07) afterbody is provided with pivot pin
Hole (31), is provided with pivot pin (18) in described pin hole (31), described blade (07) is by pin hole (31) and pivot pin (18) and oar
Folder (06) connects the collapsible blade of formation.
Extension type unmanned plane the most according to claim 6, it is characterised in that described slide block (11) and motor cabinet (12) its
In at least one is that tightening is connected with rod member (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620852792.XU CN205872439U (en) | 2016-08-08 | 2016-08-08 | Retractable unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620852792.XU CN205872439U (en) | 2016-08-08 | 2016-08-08 | Retractable unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205872439U true CN205872439U (en) | 2017-01-11 |
Family
ID=57701170
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620852792.XU Expired - Fee Related CN205872439U (en) | 2016-08-08 | 2016-08-08 | Retractable unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205872439U (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107054623A (en) * | 2017-03-13 | 2017-08-18 | 普宙飞行器科技（深圳）有限公司 | Unmanned plane slidingtype horn device and unmanned plane |
| CN107084643A (en) * | 2017-03-28 | 2017-08-22 | 东南大学 | A kind of head transmitter and its automatic identification and sighting system |
| CN107097967A (en) * | 2017-05-03 | 2017-08-29 | 李秀荣 | A kind of unmanned plane |
| CN107323659A (en) * | 2017-06-22 | 2017-11-07 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for being easy to store based on Internet of Things |
| CN107792361A (en) * | 2017-09-22 | 2018-03-13 | 蓝振宁 | A kind of multi-functional unmanned plane |
| CN107826244A (en) * | 2017-11-15 | 2018-03-23 | 安徽工程大学 | A kind of six shaft rotating devices of aircraft |
| CN108725747A (en) * | 2018-07-19 | 2018-11-02 | 广州鼎飞航空科技有限公司 | One kind is from release device |
| WO2018201416A1 (en) * | 2017-05-05 | 2018-11-08 | SZ DJI Technology Co., Ltd. | Systems and methods related to transformable unmanned aerial vehicles |
| CN112693590A (en) * | 2021-01-08 | 2021-04-23 | 徐艳 | Protection folded cascade unmanned aerial vehicle truck structure |
| CN113277075A (en) * | 2021-07-02 | 2021-08-20 | 宁波阿瑞斯自动化技术有限公司 | Collapsible many rotor unmanned aerial vehicle |
-
2016
- 2016-08-08 CN CN201620852792.XU patent/CN205872439U/en not_active Expired - Fee Related
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107054623A (en) * | 2017-03-13 | 2017-08-18 | 普宙飞行器科技（深圳）有限公司 | Unmanned plane slidingtype horn device and unmanned plane |
| CN107054623B (en) * | 2017-03-13 | 2023-09-05 | 普宙科技有限公司 | Unmanned aerial vehicle slidingtype horn device and unmanned aerial vehicle |
| WO2018166436A1 (en) * | 2017-03-13 | 2018-09-20 | 普宙飞行器科技（深圳）有限公司 | Unmanned aerial vehicle sliding-type mechanical arm device and unmanned aerial vehicle |
| CN107084643A (en) * | 2017-03-28 | 2017-08-22 | 东南大学 | A kind of head transmitter and its automatic identification and sighting system |
| CN107084643B (en) * | 2017-03-28 | 2019-03-29 | 东南大学 | A kind of holder transmitter and its automatic identification and sighting system |
| CN107097967A (en) * | 2017-05-03 | 2017-08-29 | 李秀荣 | A kind of unmanned plane |
| WO2018201416A1 (en) * | 2017-05-05 | 2018-11-08 | SZ DJI Technology Co., Ltd. | Systems and methods related to transformable unmanned aerial vehicles |
| CN107323659A (en) * | 2017-06-22 | 2017-11-07 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for being easy to store based on Internet of Things |
| CN107792361A (en) * | 2017-09-22 | 2018-03-13 | 蓝振宁 | A kind of multi-functional unmanned plane |
| CN107826244B (en) * | 2017-11-15 | 2021-03-09 | 安徽工程大学 | Six rotary device of aircraft |
| CN107826244A (en) * | 2017-11-15 | 2018-03-23 | 安徽工程大学 | A kind of six shaft rotating devices of aircraft |
| CN108725747A (en) * | 2018-07-19 | 2018-11-02 | 广州鼎飞航空科技有限公司 | One kind is from release device |
| CN108725747B (en) * | 2018-07-19 | 2024-02-06 | 广州鼎飞航空科技有限公司 | Self-releasing device |
| CN112693590A (en) * | 2021-01-08 | 2021-04-23 | 徐艳 | Protection folded cascade unmanned aerial vehicle truck structure |
| CN112693590B (en) * | 2021-01-08 | 2022-12-23 | 国网甘肃省电力公司白银供电公司 | Protection folded cascade unmanned aerial vehicle truck structure |
| CN113277075A (en) * | 2021-07-02 | 2021-08-20 | 宁波阿瑞斯自动化技术有限公司 | Collapsible many rotor unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170329 Address after: 100020 Beijing city Chaoyang District Ritan Road No. 7 Building 1 floor 1 No. 118 Patentee after: Beijing Yong Chuang Technology Co., Ltd. Address before: 430000 Optics Valley Road, East Lake New Technology Development Zone, Hubei, China, No. 58, No. Patentee before: Wuhan science and Technology Co., Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170111 Termination date: 20190808 |