CN205707294U - Folding piece in a kind of horn on Multi-axis aircraft - Google Patents
Folding piece in a kind of horn on Multi-axis aircraft Download PDFInfo
- Publication number
- CN205707294U CN205707294U CN201620675927.XU CN201620675927U CN205707294U CN 205707294 U CN205707294 U CN 205707294U CN 201620675927 U CN201620675927 U CN 201620675927U CN 205707294 U CN205707294 U CN 205707294U
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- China
- Prior art keywords
- horn
- axis aircraft
- folding piece
- connector
- snap fit
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- 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
Links
- 238000005452 bending Methods 0.000 claims description 3
- 238000010276 construction Methods 0.000 abstract description 2
- TVEXGJYMHHTVKP-UHFFFAOYSA-N 6-oxabicyclo[3.2.1]oct-3-en-7-one Chemical compound C1C2C(=O)OC1C=CC2 TVEXGJYMHHTVKP-UHFFFAOYSA-N 0.000 description 1
- 230000004308 accommodation Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002372 labelling Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
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- Clamps And Clips (AREA)
Abstract
This utility model belongs to Multi-axis aircraft technical field, it is specifically related to folding piece in a kind of horn on Multi-axis aircraft, including horn connector A, horn connector B, horn connector A lower surface is provided with engaging lug A, it is mutually hinged with engaging lug B that horn connector B lower surface is provided with engaging lug B, engaging lug A；Horn connector A upper surface is provided with connection seat, connects seat and is provided with rotating shaft, and rotating shaft is provided with stage clip and snap fit, and the lower surface of stage clip one end props up snap fit upper surface, and horn connector B upper surface is provided with draw-in groove, and snap fit hooks in draw-in groove.This utility model sound construction, easy and simple to handle, longer horn can be made directly to fold, convenient for collecting, the space of storage can be reduced, make long-armed Multi-axis aircraft carry more convenient.
Description
Technical field
This utility model belongs to Multi-axis aircraft technical field, is specifically related in a kind of horn on Multi-axis aircraft
Folding piece.
Background technology
Multi-axis aircraft, the most rotor wing unmanned aerial vehicles, it is provided with multiple propeller, controls multiple propellers by multiple motors and come
Realize flight, be widely used in take photo by plane, monitor, search and rescue, the every field such as resource exploration, agricultural, have that volume is little, lightweight, expense
With low, flexible operation and safety high.When Multi-axis aircraft is for different field, it is sometimes desirable to by the length of horn
Lengthen, when horn length is longer, Multi-axis aircraft will be made to compare and take up space, all can be the most square when making storage and move
Just.In order to solve this problem, some Multi-axis aircrafts are provided with folded piece in the junction of mainframe Yu horn, the most permissible
Horn is disposed vertically, but when the length value of horn is bigger than the height value of mainframe, even if being provided with folding in horn the inner
Overlapping piece, it is also difficult to by preferable for horn folding storage.
Summary of the invention
This utility model in prior art when the horn of Multi-axis aircraft is long the drawback of the more difficult storage of horn, carry
For folding piece in a kind of horn on Multi-axis aircraft, long horn can be divided into two sections, and in two sections of horns, folding piece is even
Connect, use folding piece in this two sections of intact linking together of horn can not to be affected the serviceability of horn, and user
Just.
Goal of the invention of the present utility model is achieved through the following technical solutions: a kind of machine on Multi-axis aircraft
Folding piece in arm, including the horn connector A and the horn connector B of tubular-shaped structures of tubular-shaped structures, horn connector A lower surface sets
Having engaging lug A, it is mutually hinged with engaging lug B that horn connector B lower surface is provided with engaging lug B, engaging lug A；On horn connector A
Surface is provided with connection seat, connects seat and is provided with rotating shaft, and rotating shaft is provided with stage clip and snap fit, and the lower surface of stage clip one end props up
Snap fit upper surface, horn connector B upper surface is provided with draw-in groove, and snap fit hooks in draw-in groove.
As preferably, horn connector A side is provided with fluting A, and fluting A both sides are respectively provided with a clamping plate A, two clamping plates A
It is provided with screw A in correspondence with each other.
As preferably, horn connector B side is provided with fluting B, and fluting B both sides are respectively provided with a clamping plate B, two clamping plates B
It is provided with screw B in correspondence with each other.
As preferably, described stage clip is made up of tail end, the collar, head end, and tail end is connected with collar left end, collar right-hand member with
Head end connects, and tail end props up horn connector A upper surface, and the collar is enclosed within rotating shaft, and the lower surface of head end props up snap fit upper surface.
As preferably, the tail end of stage clip is U-shaped structure.
As preferably, the head end of stage clip is that two mutually symmetrical with L-shaped structure parts are constituted.
As preferably, stage clip is that elastic wire bending is made.
As preferably, snap fit both sides are respectively provided with a C-shaped snap ring, and C-shaped snap ring is arranged in rotating shaft.
Compared with prior art, this utility model has the advantages that horn connector A, horn connector B are respectively
Connect two sections of horns, bolt is set in screw A and screw B and clamps two sections of horns respectively, be connected firmly.Launch at horn
Time, the snap fit being arranged on horn connector A hooks in horn connector B draw-in groove, simultaneously horn connector A and horn connector
B lower surface is hinged, and now two sections of horns are point-blank, and the lower surface of stage clip one end props up snap fit upper surface, pressure
Spring can prevent snap fit to be rotated up, and makes horn can keep deployed condition, when needs storage horn, only need to upwards be turned by snap fit
Dynamic, horn connector B just can depart from the locking state of snap fit, so that the horn being connected with horn connector B can rotate, real
Existing folding effect, operates the most simple and convenient, it is adaptable to need the horn of frequent folding and expanding, makes to be provided with longer horn
Multi-axis aircraft is easily received, and saves accommodation space.
In sum, this utility model sound construction, easy and simple to handle, longer horn can be made directly to fold, convenient
Storage, can reduce the space of storage, make long-armed Multi-axis aircraft carry more convenient.
Accompanying drawing explanation
Fig. 1 is this utility model axonometric chart；
Fig. 2 is this utility model front view；
Fig. 3 is that this utility model uses state diagram；
Fig. 4 is stage clip structural representation；
Labelling in figure: 1, horn connector A, 2, horn connector B, 3, engaging lug A, 4, engaging lug B, 5, connect seat, 6,
Rotating shaft, 7, stage clip, 8, snap fit, 9, draw-in groove, 10, fluting A, 11, clamping plate A, 12, screw A, 13, fluting B, 14, clamping plate B, 15, spiral shell
Hole B, 16, tail end, 17, the collar, 18, head end, 19, C-shaped snap ring.
Detailed description of the invention
This utility model is further described by the embodiment represented by 1 below in conjunction with the accompanying drawings:
Embodiment 1
As Figure 1-4, folding piece in a kind of horn on Multi-axis aircraft, including the horn connector of tubular-shaped structures
The horn connector B2 of A1 and tubular-shaped structures, horn connector A1 lower surface is provided with engaging lug A3, horn connector B2 lower surface
It is provided with engaging lug B4, engaging lug A3 mutually hinged with engaging lug B4；Horn connector A1 upper surface is provided with connection seat 5, connects seat 5
Being provided with rotating shaft 6, rotating shaft 6 is provided with stage clip 7 and snap fit 8, and the lower surface of stage clip 7 one end props up snap fit 8 upper surface, horn
Connector B2 upper surface is provided with draw-in groove 9, and snap fit hooks in draw-in groove 9.Snap fit 8 both sides are respectively provided with a C-shaped snap ring 19, C-shaped snap ring
19 are arranged in rotating shaft 6.
As it is shown in figure 1, horn connector A1 side is provided with fluting A10, fluting A10 both sides are respectively provided with a clamping plate A11, two
Block clamping plate A11 is provided with screw A12 in correspondence with each other.Horn connector B2 side is provided with fluting B13, and fluting B13 both sides respectively set
A clamping plate B14, two clamping plates B14 is had to be provided with screw B15 in correspondence with each other.
As Figure 1 and Figure 4, described stage clip 7 is made up of tail end 16, the collar 17, head end 18, and the tail end of stage clip 7 is U-shaped
Structure, the head end of stage clip 7 is that two mutually symmetrical with L-shaped structure parts are constituted.Tail end 16 is connected with the collar 17 left end, the collar 17
Right-hand member is connected with head end 18, and tail end 16 props up horn connector A1 upper surface, and the collar 17 is enclosed within rotating shaft 6, the following table of head end 18
Face props up snap fit 8 upper surface.Stage clip 7 is made for elastic wire bending.
Specific embodiment described in literary composition is only to this utility model spirit explanation for example.Belonging to this utility model
Described specific embodiment can be made various amendment or supplements or use similar by those skilled in the art
Mode substitutes, but without departing from spirit of the present utility model or surmount scope defined in appended claims.
Claims (8)
1. a folding piece in the horn on Multi-axis aircraft, including the horn connector A(1 of tubular-shaped structures) and tubular-shaped structures
Horn connector B(2), it is characterised in that horn connector A lower surface is provided with engaging lug A(3), horn connector B lower surface
It is provided with engaging lug B(4), engaging lug A is mutually hinged with engaging lug B；Horn connector A upper surface is provided with connection seat (5), connects seat
Being provided with rotating shaft (6), rotating shaft is provided with stage clip (7) and snap fit (8), and the lower surface of stage clip one end props up snap fit upper surface,
Horn connector B upper surface is provided with draw-in groove (9), and snap fit hooks in draw-in groove.
Folding piece in a kind of horn on Multi-axis aircraft the most according to claim 1, it is characterised in that horn connects
Part A side is provided with fluting A(10), fluting A both sides are respectively provided with a clamping plate A(11), two clamping plates A is provided with spiral shell in correspondence with each other
Hole A(12).
Folding piece in a kind of horn on Multi-axis aircraft the most according to claim 1, it is characterised in that horn connects
Part B side is provided with fluting B(13), fluting B both sides are respectively provided with a clamping plate B(14), two clamping plates B is provided with spiral shell in correspondence with each other
Hole B(15).
Folding piece in a kind of horn on Multi-axis aircraft the most according to claim 1, it is characterised in that described pressure
Spring is made up of tail end (16), the collar (17), head end (18), and tail end is connected with collar left end, and collar right-hand member is connected with head end, tail end
Propping up horn connector A upper surface, the collar is enclosed within rotating shaft, and the lower surface of head end props up snap fit upper surface.
Folding piece in a kind of horn on Multi-axis aircraft the most according to claim 4, it is characterised in that the tail of stage clip
End is U-shaped structure.
Folding piece in a kind of horn on Multi-axis aircraft the most according to claim 4, it is characterised in that the head of stage clip
End is that two mutually symmetrical with L-shaped structure parts are constituted.
7., according to folding piece in a kind of horn on Multi-axis aircraft described in claim 1 or 4 or 5 or 6, its feature exists
In, stage clip is that elastic wire bending is made.
Folding piece in a kind of horn on Multi-axis aircraft the most according to claim 1, it is characterised in that snap fit both sides
Being respectively provided with a C-shaped snap ring (19), C-shaped snap ring is arranged in rotating shaft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620675927.XU CN205707294U (en) | 2016-06-27 | 2016-06-27 | Folding piece in a kind of horn on Multi-axis aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620675927.XU CN205707294U (en) | 2016-06-27 | 2016-06-27 | Folding piece in a kind of horn on Multi-axis aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205707294U true CN205707294U (en) | 2016-11-23 |
Family
ID=57318349
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620675927.XU Expired - Fee Related CN205707294U (en) | 2016-06-27 | 2016-06-27 | Folding piece in a kind of horn on Multi-axis aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205707294U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741824A (en) * | 2017-01-24 | 2017-05-31 | 厦门南羽科技有限公司 | Unmanned plane power arm and unmanned plane |
| CN107031816A (en) * | 2017-03-07 | 2017-08-11 | 广西云瑞科技有限公司 | A kind of foldable horn of the agricultural unmanned plane of many rotors of multipurpose |
| CN107323661A (en) * | 2017-07-03 | 2017-11-07 | 湖北龙翼机器人有限公司 | A kind of axle aircraft of multifunctional portable six |
| CN108860564A (en) * | 2018-06-21 | 2018-11-23 | 上海歌尔泰克机器人有限公司 | A kind of unmanned plane and its horn foldable structure |
-
2016
- 2016-06-27 CN CN201620675927.XU patent/CN205707294U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741824A (en) * | 2017-01-24 | 2017-05-31 | 厦门南羽科技有限公司 | Unmanned plane power arm and unmanned plane |
| CN107031816A (en) * | 2017-03-07 | 2017-08-11 | 广西云瑞科技有限公司 | A kind of foldable horn of the agricultural unmanned plane of many rotors of multipurpose |
| CN107031816B (en) * | 2017-03-07 | 2019-08-16 | 广西云瑞科技有限公司 | A kind of foldable horn of the agricultural unmanned plane of more rotors of multipurpose |
| CN107323661A (en) * | 2017-07-03 | 2017-11-07 | 湖北龙翼机器人有限公司 | A kind of axle aircraft of multifunctional portable six |
| CN108860564A (en) * | 2018-06-21 | 2018-11-23 | 上海歌尔泰克机器人有限公司 | A kind of unmanned plane and its horn foldable structure |
| CN108860564B (en) * | 2018-06-21 | 2021-08-20 | 上海歌尔泰克机器人有限公司 | Unmanned aerial vehicle and horn beta structure thereof |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161123 Termination date: 20210627 |