CN205633036U - Many rotor unmanned aerial vehicle's support - Google Patents
Many rotor unmanned aerial vehicle's support Download PDFInfo
- Publication number
- CN205633036U CN205633036U CN201620248602.3U CN201620248602U CN205633036U CN 205633036 U CN205633036 U CN 205633036U CN 201620248602 U CN201620248602 U CN 201620248602U CN 205633036 U CN205633036 U CN 205633036U
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- CN
- China
- Prior art keywords
- unmanned aerial
- support
- horn
- many rotor
- rotor wing
- 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.)
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Abstract
The utility model relates to a many rotor unmanned aerial vehicle's support, including horn, reset spring, card strip and connecting portion, connecting portion include the connecting plate of two relative settings, and the one end of horn is through round pin axle and two connecting plate hinged, the card strip transversely runs through two connecting plates, be equipped with the guide way on the connecting plate, block the strip and can follow guide way horizontal migration, reset spring and guide way parallel arrangement, reset spring one end and calorie strip link to each other, and reset spring's the other end links to each other with connecting portion, is equipped with and blocks the bayonet socket of an adaptation on the horn. Adopt the utility model discloses a support when unmanned aerial vehicle collects, just can draw the horn in through inside promotion card strip, the trouble of having avoided the relapse to dismantle has reduced many rotors unmanned aerial vehicle collection size, has solved the be not convenient for difficult problem of transportation collection of many rotors unmanned aerial vehicle.
Description
Technical field
This utility model relates to field of mechanical technique, particularly relates to propping up of a kind of many rotor wing unmanned aerial vehicles
Frame.
Background technology
Many rotor wing unmanned aerial vehicles control multiple propellers by multiple motors and realize flight, extensively use
In taking photo by plane, monitor, search and rescue, the every field such as resource exploration, agricultural, have that volume is little, weight
Amount is light, expense is low, flexible operation and safety high.Many rotor wing unmanned aerial vehicles have more
Horn, when collecting unmanned plane, need to twist off screw, being disassembled by horn could more preferably
Transport, repeatedly dismantle and install and both wasted time, also accelerate the abrasion of part.
Utility model content
This utility model aims to provide the support of a kind of many rotor wing unmanned aerial vehicles, mounts and dismounts all ten
It is convenient to divide.
For reaching above-mentioned purpose, the technical solution adopted in the utility model is as follows:
A kind of support of many rotor wing unmanned aerial vehicles, including horn, back-moving spring, card article and connecting portion,
Described connecting portion includes two connecting plates being oppositely arranged, one end of described horn by bearing pin with
Two connecting plates are hinged；Card article extends transversely through two connecting plates；Described connecting plate is provided with guiding
Groove, card article can move horizontally along gathering sill, and back-moving spring be arranged in parallel with gathering sill, described multiple
Position spring one end is connected with card article, and the other end of back-moving spring is connected with connecting portion, described horn
It is provided with the bayonet socket adaptive with card article.
Further, the end of described card article is equipped with and pushes away torsion, and described diameter is more than card article
Vertically size.
Further, described card article is positioned at inner side above bearing pin.
Further, also include that motor cabinet, described motor cabinet include top board, base plate and ring junction
The placement ring of structure, described top board is connected with placing top surface of ring, described base plate and placement ring bottom surface
Being connected, described placement ring side is provided with the clamping part of tubulose, and described top board and base plate are provided with
Motor installing hole and axis hole, described clamping part is connected with the other end of horn.
Further, described top board and base plate are connected with placement ring screw.
Further, the front and back of the clamping part of described tubulose is respectively equipped with a groove,
Groove runs through the outer face of clamping part, and the axis of clamping part and two grooves are positioned at same level；
The outer end of described groove is provided with a pair lug, and two lugs are respectively arranged on the upper side and lower side of groove.
Further, also include that propeller and motor, described propeller are arranged on motor, institute
Stating motor to be arranged on motor cabinet by motor installing hole, described motor and propeller have two,
Two motors are separately mounted on top board and base plate.
Further, the blade of described propeller has two.
Further, the front and back of described placement ring is provided with bar hole, described top board and the end
Plate is provided with cable hole.
Further, the material of described top board and base plate is carbon fibre, the material of described placement ring
Matter is aluminium alloy.
Compared with prior art, this utility model has the advantages that
1. the support that this utility model provides, when unmanned plane is collected, by inwardly promoting card article
Just can draw horn in, it is to avoid the trouble repeatedly dismantled, reduce many rotor wing unmanned aerial vehicles collection chi
Very little, solve a difficult problem for the not readily transportable collection of many rotor wing unmanned aerial vehicles；
2. this utility model provide motor cabinet, motor is installed on top board and base plate, top board and
Base plate is arranged on placement ring, mounts and dismounts very convenient.
Accompanying drawing explanation
Fig. 1 is the structural representation of embodiment 1；
Fig. 2 is the structural representation pushing away torsion；
Fig. 3 is the structural representation of horn；
Fig. 4 is the structural representation of embodiment 2；
Fig. 5 is the structural representation of motor cabinet；
In figure: 1-horn, 2-connecting portion, 3-contiguous block, 4-bayonet socket, 5-card article, 6-reset
Spring, 7-spring anchor block, 9-gathering sill, 10-push away torsion, 11-motor cabinet, 12-clamping part,
13-motor installing hole, 14-top board, 15-base plate, 16-place ring, 17-screwed hole B, 18-
Screwed hole A, 19-axis hole, 20-cable hole, 21-groove, 22-lug, 23-bar hole,
24-propeller, 25-motor.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearer, below
In conjunction with accompanying drawing, this utility model is further elaborated.
Embodiment 1
As shown in Figure 1, 2, the support of many rotor wing unmanned aerial vehicles disclosed in the present embodiment, including machine
Arm 1, back-moving spring 6, card article 5 and connecting portion 2, connecting portion 2 includes that two are oppositely arranged
Connecting plate, one end of horn 1 by bearing pin 8 hinged with two connecting plates；Card article 5 is horizontal
Run through two connecting plates；Connecting plate is provided with gathering sill 9, and card article 5 can be along gathering sill 9 level
Mobile, back-moving spring 6 be arranged in parallel with gathering sill 9, back-moving spring 6 one end and card article 5 phase
Even, the other end of back-moving spring 6 is connected with connecting portion 2, and horn 1 is provided with fits with card article 5
The bayonet socket 4 joined.Preferably, two connecting plates are provided with spring anchor block away from one end of horn 1
7, the other end of back-moving spring 6 is fixed on spring anchor block 7.Further, card article 5
Being positioned at inner side above bearing pin 8, the end of card article 5 is equipped with and pushes away torsion 10, pushes away the diameter turning round 10
Vertical size more than card article 5.
As shown in Figure 1,3, the parallel contiguous block being provided with two tabulars in the end of horn 1 one end
3, contiguous block 3 is provided with and the axis hole of bearing pin 8 adaptation.During use, hold and push away torsion 10 edges
Gathering sill 9 inwardly promotes card article 5, and card article 5 exits from bayonet socket 4, and horn 1 is from heavy sensation of the body
Rotating down around bearing pin 8 under power effect, horn 11 heart in unmanned plane draws in.Need support
During start arm 1, same holding pushes away torsion 10 and inwardly promotes along gathering sill 9, manually by machine
Arm 1 is lifted to horizontal level, unclamps and pushes away torsion 10, under the elastic force of back-moving spring 6, and card article 5
It is moved horizontally in bayonet socket 4 along gathering sill 9, under the barrier effect of card article 5, horn 1 nothing
Method rotates.
Embodiment 2
As shown in Figure 4,5, the present embodiment includes with the difference of embodiment 1: also include motor
Seat 11, motor cabinet 11 includes the placement ring 16 of top board 14, base plate 15 and loop configuration, top
Plate 14 is connected with placing ring 16 end face, and base plate 15 is connected with placing ring 16 bottom surface, puts
Put ring 16 side be provided with the clamping part 12 of tubulose, top board 14 and base plate 15 be provided with motor peace
Dress hole 13 and axis hole 19, clamping part 12 is connected with the other end of horn 1.Further,
The front and back of clamping part 12 is respectively equipped with a groove 21, and groove 21 runs through clamping part
The outer face of 12, the axis of clamping part 12 and two grooves 21 are positioned at same level；Logical
The outer end of groove 21 is provided with a pair lug 22, and two lugs 22 are respectively arranged on the upside of groove 21
And downside, lug is provided with screwed hole, is provided with bolt, loosers a bolt during use in screwed hole,
Tight a bolt again after clamping part 2 is enclosed within horn 1, so that it may motor cabinet 11 is arranged on machine
On arm 1, installation and removal are quite convenient to.The front and back placing ring 16 is provided with bar shaped
Hole 23, with heat radiation；Top board 14 and base plate 15 are provided with cable hole 20；Top board 14 and base plate
The material of 15 is carbon fibre, and the material placing ring 16 is aluminium alloy.
Further, also including propeller 24 and motor 25, propeller 24 is arranged on motor
On 25, motor 25 is arranged on motor cabinet 11 by motor installing hole 13, motor 25 He
Propeller 24 has two, and two motors 25 are separately mounted on top board 14 and base plate 15.Electricity
Machine 25 is mounted remotely from the side of clamping part 12.The blade of propeller 24 has two.
Further, top board 14 and base plate 15 are connected with placing ring 16 screw.Preferably,
Machine base body outer face is cylinder, and machine base body inner face is plane, and outer face is than inner face
Horizontal size is big, is respectively equipped with a screwed hole A18 at four angles of top board 14 and base plate 15,
Place ring 16 end face and bottom surface is provided with the screwed hole B17 adaptive with screwed hole A18, during use
Motor 25 is arranged on top board 14 and base plate 15, with screw by top board 14 and base plate 15
Being arranged on placement ring 16, installation and removal are quite convenient to.
Certainly, this utility model also can have other numerous embodiments, new without departing substantially from this practicality
In the case of type spirit and essence thereof, those of ordinary skill in the art can be according to this utility model
Make various corresponding change and deformation, but these change accordingly and deformation all should belong to this reality
By novel appended scope of the claims.
Claims (10)
1. the support of rotor wing unmanned aerial vehicle more than a kind, it is characterized in that: include horn (1), back-moving spring (6), card article (5) and connecting portion (2), described connecting portion (2) includes two connecting plates being oppositely arranged, and one end of described horn (1) is hinged with two connecting plates by bearing pin (8)；Card article (5) extends transversely through two connecting plates；Described connecting plate is provided with gathering sill (9), card article (5) can move horizontally along gathering sill (9), back-moving spring (6) be arranged in parallel with gathering sill (9), described back-moving spring (6) one end is connected with card article (5), the other end of back-moving spring (6) is connected with connecting portion (2), and described horn (1) is provided with the bayonet socket (4) adaptive with card article (5).
The support of many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: the end of described card article (5) is equipped with and pushes away torsion (10), described in push away the diameter of torsion (10) the vertical size more than card article (5).
The support of many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: described card article (5) is positioned at inside bearing pin (8) top.
The support of many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterized in that: also include motor cabinet (11), described motor cabinet (11) includes top board (14), the placement ring (16) of base plate (15) and loop configuration, described top board (14) is connected with placing ring (16) end face, described base plate (15) is connected with placing ring (16) bottom surface, described placement ring (16) side is provided with the clamping part (12) of tubulose, described top board (14) and base plate (15) are provided with motor installing hole (13) and axis hole (19), described clamping part (12) is connected with the other end of horn (1).
The support of many rotor wing unmanned aerial vehicles the most according to claim 4, it is characterised in that: described top board (14) and base plate (15) are connected with placing ring (16) screw.
The support of many rotor wing unmanned aerial vehicles the most according to claim 4, it is characterized in that: the front and back of the clamping part (12) of described tubulose is respectively equipped with a groove (21), groove (21) runs through the outer face of clamping part (12), and axis and two grooves (21) of clamping part (12) are positioned at same level；The outer end of described groove (21) is provided with a pair lug (22), and two lugs (22) are respectively arranged on the upper side and lower side of groove (21).
The support of many rotor wing unmanned aerial vehicles the most according to claim 4, it is characterized in that: also include propeller (24) and motor (25), described propeller (24) is arranged on motor (25), described motor (25) is arranged on motor cabinet (11) by motor installing hole (13), described motor (25) and propeller (24) have two, and two motors (25) are separately mounted on top board (14) and base plate (15).
The support of many rotor wing unmanned aerial vehicles the most according to claim 7, it is characterised in that: the blade of described propeller (24) has two.
The support of many rotor wing unmanned aerial vehicles the most according to claim 4, it is characterized in that: the front and back of described placement ring (16) is provided with bar hole (23), described top board (14) and base plate (15) and is provided with cable hole (20).
The support of many rotor wing unmanned aerial vehicles the most according to claim 4, it is characterised in that: the material of described top board (14) and base plate (15) is carbon fibre, and the material of described placement ring (16) is aluminium alloy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620248602.3U CN205633036U (en) | 2016-03-25 | 2016-03-25 | Many rotor unmanned aerial vehicle's support |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620248602.3U CN205633036U (en) | 2016-03-25 | 2016-03-25 | Many rotor unmanned aerial vehicle's support |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205633036U true CN205633036U (en) | 2016-10-12 |
Family
ID=57075440
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620248602.3U Expired - Fee Related CN205633036U (en) | 2016-03-25 | 2016-03-25 | Many rotor unmanned aerial vehicle's support |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205633036U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113002768A (en) * | 2021-02-26 | 2021-06-22 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle horn rapid disassembly structure reaches unmanned aerial vehicle including it |
-
2016
- 2016-03-25 CN CN201620248602.3U patent/CN205633036U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113002768A (en) * | 2021-02-26 | 2021-06-22 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle horn rapid disassembly structure reaches unmanned aerial vehicle including it |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161012 Termination date: 20170325 |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| DD01 | Delivery of document by public notice |
Addressee: Sichuan Kris Aeronautical Technology Co., Ltd. Finance Document name: Notification of Approving Refund |
|
| DD01 | Delivery of document by public notice |