CN106585977A - Rotary clamping type quick-release paddle and assembling and disassembling method thereof - Google Patents
Rotary clamping type quick-release paddle and assembling and disassembling method thereof Download PDFInfo
- Publication number
- CN106585977A CN106585977A CN201611228930.8A CN201611228930A CN106585977A CN 106585977 A CN106585977 A CN 106585977A CN 201611228930 A CN201611228930 A CN 201611228930A CN 106585977 A CN106585977 A CN 106585977A
- Authority
- CN
- China
- Prior art keywords
- propeller
- briquetting
- rotation
- deck
- oar
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention discloses a rotary clamping type quick-release paddle and an assembling and dissembling method thereof. The rotary clamping type quick-release paddle comprises a pressing pin, a rotary pressing block, a rotary pin, a propeller, a propeller clamping holder, an elastic block and a spring; the pressing pin which can move up and down in a pressing block boss hole of the rotary pressing block is arranged in the pressing block boss hole of the rotary pressing block in a sleeved mode, the rotary pressing block which can rotate around the rotary pin is locked at the protruding part of one end of the propeller clamping holder through the rotary pin, the propeller is arranged in the propeller clamping holder, the elastic block which can move up and down in a clamping holder boss hole of the peddle clamping holder is arranged in the clamping holder boss hole of the peddle clamping holder in a sleeved mode; the spring is arranged in an internal hole of the elastic block in a sleeved mode.
Description
Technical field
The present invention relates to the oar in unmanned plane field, more particularly, to unmanned plane；Specifically, the present invention relates to a kind of rotation
Turn compression type Quick Release oar and its assembly and disassembly method.
Background technology
Unmanned plane market is more and more burning hoter, is also increasingly received by many people.Travelled outdoors boat using unmanned plane
During bat, Jing is needed often to dismantle propeller to facilitate transport.Existing unmanned plane propeller leans on screw locking substantially with motor, dismounts numerous
It is trivial, and Jing often dismountings are easily caused screw cunning tooth, cause unnecessary risk.
And, existing upper and lower rotary clamping mode has used easy generation diastema long, so as to affect the flight of unmanned plane
Performance.
Therefore, those skilled in the art is devoted to developing a kind of convenient dismounting, will not cause and tear risk by mistake open and avoid
Affect the technical scheme of the flying quality of unmanned plane.
The content of the invention
In view of the drawbacks described above of prior art, the technical problem to be solved be to provide a kind of convenient dismounting,
The flying quality torn risk by mistake open and avoid impact unmanned plane will not be caused rotatably compresses formula Quick Release oar.
For achieving the above object, the invention provides one kind rotatably compresses formula Quick Release oar, including：Pushpin, rotation briquetting,
Rotating dog, propeller, propeller deck, bullet block and spring；Wherein, pushpin according to can rotation briquetting briquetting boss hole
Interior up and down mode is set in the briquetting boss hole of rotation briquetting, and rotation briquetting is according to the side that can be rotated around rotating dog
Formula is locked in the high spot of propeller deck one end by rotating dog, and propeller is disposed in propeller deck, and bullet block is according to energy
Enough up and down modes in deck boss hole are arranged in the deck boss hole with propeller deck；And spring is set in bullet
In the endoporus of block.
For achieving the above object, present invention also offers a kind of described assemble method for rotatably compressing formula Quick Release oar, its
It is characterised by including：Propeller slide fit is put in propeller deck, is put down using the endoporus and propeller deck of propeller deck
Two locating shafts on face are positioned to propeller；The other end for pinning rotation briquetting is rotated to rotating briquetting, makes rotation
Turn the briquetting other end to be stuck in draw-in groove；Make bullet block upspring, be arranged in the groove in rotation briquetting, to limit the fortune of rotation briquetting
It is dynamic, there is pressuring action to limit propeller to prevent propeller from ejecting to propeller using rotation briquetting.
For achieving the above object, present invention also offers a kind of described method for dismounting for rotatably compressing formula Quick Release oar, its
It is characterised by including：Downwards by the pushpin being sheathed on rotation briquetting, promote bullet block to move down, make bullet block depart from rotation pressure
Block, releases bullet block to rotating the restriction effect of briquetting, and the other end for pinning rotation briquetting is rotated, and makes rotation briquetting mark spiral shell
The end region of rotation oar, releases rotation pressuring action of the briquetting to propeller, takes out propeller.
Compared with prior art, the present invention can greatly improve the disassembly efficiency of propeller, facilitate the transport of unmanned plane, and
And the present invention is by compression power restriction propeller, the diastema between limited reduction propeller and deck, the flying quality to unmanned plane
It is no to affect and safe.
The technique effect of the design, concrete structure and generation of the present invention is described further below with reference to accompanying drawing, with
It is fully understood from the purpose of the present invention, feature and effect.
Description of the drawings
With reference to accompanying drawing, and by reference to detailed description below, it will more easily have more complete understanding to the present invention
And its adjoint advantages and features is more easily understood, wherein：
Fig. 1 is the decomposing schematic representation for rotatably compressing formula Quick Release oar according to the preferred embodiment of the invention.
Fig. 2 is the assembling schematic diagram of the part-structure for rotatably compressing formula Quick Release oar according to the preferred embodiment of the invention.
Fig. 3 is that another assembling of the part-structure for rotatably compressing formula Quick Release oar according to the preferred embodiment of the invention is illustrated
Figure.
Fig. 4 is the section of the part-structure of the part-structure for rotatably compressing formula Quick Release oar according to the preferred embodiment of the invention
Figure.
It should be noted that accompanying drawing is used to illustrate the present invention, and the unrestricted present invention.Note, represent that the accompanying drawing of structure can
Can be not necessarily drawn to scale.Also, in accompanying drawing, same or like element indicates same or like label.
Specific embodiment
Fig. 1 is the decomposing schematic representation for rotatably compressing formula Quick Release oar according to the preferred embodiment of the invention, and Fig. 2 is according to this
The assembling schematic diagram of the part-structure for rotatably compressing formula Quick Release oar of bright preferred embodiment, Fig. 3 is preferable to carry out according to the present invention
Another assembling schematic diagram of the part-structure for rotatably compressing formula Quick Release oar of example, Fig. 4 is rotation according to the preferred embodiment of the invention
Turn the sectional view of the part-structure of the part-structure of compression type Quick Release oar.
As shown in Figure 1, Figure 2, Figure 3 and Figure 4, the formula Quick Release oar that rotatably compresses according to the preferred embodiment of the invention includes：Press
Pad 1, rotation briquetting 2, rotating dog 3, propeller 4, propeller deck 5, bullet block 6 and spring 7.
Wherein, pushpin 1 according to can rotation briquetting 2 briquetting boss hole in up and down mode be set in rotation
In the briquetting boss hole of briquetting 2, rotate briquetting 2 and propeller is locked in by rotating dog 3 according to the mode that can be rotated around rotating dog 3
The high spot of 5 one end of deck, propeller 4 are disposed in propeller deck 5, and bullet block 6 is according on can be in the deck boss hole
The mode of lower activity is arranged in the deck boss hole with propeller deck 5；And spring 7 is set in the endoporus of bullet block 6.
For the assembling for rotatably compressing formula Quick Release oar according to the preferred embodiment of the invention, following step can be taken：
4 slide fit of propeller is put in propeller deck 5, using 5 plane of endoporus and propeller deck of propeller deck 5
On two locating shafts propeller 4 is positioned；The other end for pinning rotation briquetting 2 is rotated to rotating briquetting 2, makes rotation
Turn 2 other end of briquetting to be stuck in draw-in groove；Make bullet block 6 upspring, be arranged in the groove in rotation briquetting 2, to limit rotation briquetting 2
Motion, has pressuring action to propeller 4 to limit propeller 4 to prevent propeller 4 from ejecting using rotation briquetting 2.
For the dismounting for rotatably compressing formula Quick Release oar according to the preferred embodiment of the invention, following step can be taken：
Downwards by the pushpin 1 being sheathed on rotation briquetting 2, promote bullet block 6 to move down, make bullet block 6 depart from rotation pressure
Block 2, releases the restriction effect of bullet 6 pairs of rotation briquettings 2 of block, and the other end for installing rotation briquetting 2 is rotated, and makes rotation briquetting 2
The end region of propeller 4 is marked, rotation pressuring action of the briquetting 2 to propeller 4 is released, is taken out propeller 4.
Compared with prior art, the present invention can greatly improve the disassembly efficiency of propeller, facilitate the transport of unmanned plane, and
And the present invention is by compression power restriction propeller, the diastema between limited reduction propeller and deck, the flying quality to unmanned plane
It is no to affect and safe.
Described above illustrates and describes the preferred embodiments of the present invention, as previously mentioned, it should be understood that not office of the invention
Be limited to form disclosed herein, be not to be taken as the exclusion to other embodiment, and can be used for various other combinations, modification and
Environment, and can be changed by the technology or knowledge of above-mentioned teaching or association area in invention contemplated scope described herein
It is dynamic.And change that those skilled in the art are carried out and change be without departing from the spirit and scope of the present invention, then all should be appended by the present invention
In scope of the claims.
Claims (3)
1. one kind rotatably compresses formula Quick Release oar, it is characterised in that include：Pushpin, rotation briquetting, rotating dog, propeller, spiral
Oar deck, bullet block and spring；Wherein, pushpin is according to can be in up and down mode set in the briquetting boss hole of rotation briquetting
It is located in the briquetting boss hole of rotation briquetting, rotation briquetting is locked in spiral shell by rotating dog according to the mode that can be rotated around rotating dog
The high spot of rotation oar deck one end, propeller are disposed in propeller deck, and bullet block is according on can be in the deck boss hole
The mode of lower activity is arranged in the deck boss hole with propeller deck；And spring is set in the endoporus of bullet block.
2. a kind of assemble method for rotatably compressing formula Quick Release oar according to claim 1, it is characterised in that include：By spiral
Oar slide fit is put in propeller deck, using two locating shafts on the endoporus and propeller deck plane of propeller deck to spiral shell
Rotation oar is positioned；The other end for pinning rotation briquetting is rotated to rotating briquetting, makes the rotation briquetting other end be stuck in draw-in groove
It is interior；Make bullet block upspring, be arranged in the groove in rotation briquetting, to limit the motion of rotation briquetting, using rotation briquetting to spiral
Oar has pressuring action to limit propeller to prevent propeller from ejecting.
3. a kind of method for dismounting for rotatably compressing formula Quick Release oar according to claim 1, it is characterised in that include：Press downwards
The pushpin being sheathed on rotation briquetting, promotes bullet block to move down, and makes bullet block depart from rotation briquetting, releases bullet block to rotation pressure
The restriction effect of block, the other end for installing rotation briquetting are rotated, and make rotation briquetting mark the end region of propeller, are released
Rotation pressuring action of the briquetting to propeller, takes out propeller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611228930.8A CN106585977A (en) | 2016-12-27 | 2016-12-27 | Rotary clamping type quick-release paddle and assembling and disassembling method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611228930.8A CN106585977A (en) | 2016-12-27 | 2016-12-27 | Rotary clamping type quick-release paddle and assembling and disassembling method thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106585977A true CN106585977A (en) | 2017-04-26 |
Family
ID=58602676
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611228930.8A Pending CN106585977A (en) | 2016-12-27 | 2016-12-27 | Rotary clamping type quick-release paddle and assembling and disassembling method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106585977A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106672210A (en) * | 2017-02-21 | 2017-05-17 | 上海未来伙伴机器人有限公司 | Quick disassembly propeller and unmanned aerial vehicle adopting same |
| CN109178302A (en) * | 2018-08-16 | 2019-01-11 | 上海歌尔泰克机器人有限公司 | A kind of propeller quick-disassembly structure and aircraft |
| WO2020062509A1 (en) * | 2018-09-30 | 2020-04-02 | 深圳市大疆创新科技有限公司 | Propeller structure, power apparatus, and unmanned aircraft |
| US11014647B2 (en) * | 2016-10-28 | 2021-05-25 | SZ DJI Technology Co., Ltd. | Locking mechanism, propeller, motor, propulsion system assembly, and aircraft |
-
2016
- 2016-12-27 CN CN201611228930.8A patent/CN106585977A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11014647B2 (en) * | 2016-10-28 | 2021-05-25 | SZ DJI Technology Co., Ltd. | Locking mechanism, propeller, motor, propulsion system assembly, and aircraft |
| CN106672210A (en) * | 2017-02-21 | 2017-05-17 | 上海未来伙伴机器人有限公司 | Quick disassembly propeller and unmanned aerial vehicle adopting same |
| CN106672210B (en) * | 2017-02-21 | 2023-09-05 | 上海未来伙伴机器人有限公司 | Quick detach oar and adopt its unmanned aerial vehicle |
| CN109178302A (en) * | 2018-08-16 | 2019-01-11 | 上海歌尔泰克机器人有限公司 | A kind of propeller quick-disassembly structure and aircraft |
| WO2020062509A1 (en) * | 2018-09-30 | 2020-04-02 | 深圳市大疆创新科技有限公司 | Propeller structure, power apparatus, and unmanned aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170426 |