CN205770123U - A kind of unmanned plane propeller rapid dismounting apparatus - Google Patents
A kind of unmanned plane propeller rapid dismounting apparatus Download PDFInfo
- Publication number
- CN205770123U CN205770123U CN201620440737.XU CN201620440737U CN205770123U CN 205770123 U CN205770123 U CN 205770123U CN 201620440737 U CN201620440737 U CN 201620440737U CN 205770123 U CN205770123 U CN 205770123U
- Authority
- CN
- China
- Prior art keywords
- hole
- unmanned plane
- base
- buttons
- strip
- 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.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of unmanned plane propeller rapid dismounting apparatus, including: footstock, being provided with bar shaped boss in the middle of footstock bottom surface, be provided with the first through hole inside bar shaped boss along its length, the first through hole is respectively provided on two sides with the strip through-hole communicated with this first through hole；Base, in the middle of base top surface, concave shaped is in strip groove, and base top surface is positioned at the length direction both sides indent respectively of strip groove and forms the recess towards this base center, and each recess has relative two sidewall, and each sidewall is provided with draw-in groove, bar shaped boss is placed in described strip groove；Two buttons, two buttons are respectively equipped with radial direction through hole, and these two buttons are positioned in described first through hole, and an alligator clamp, between two buttons, is provided with straight pin in radial direction through hole, and these straight pin both ends are stretched out and card slot fit from strip through-hole.This utility model makes the installation of unmanned plane propeller and process of pulling down simple, convenient.
Description
Technical field
This utility model relates to the dismounting technical field of unmanned plane propeller, more particularly to a kind of unmanned plane propeller rapid dismounting apparatus.
Background technology
The mode that existing unmanned plane propeller is connected with oar seat is to first pass through key screw oar seat to be locked on motor, the most again propeller is passed through screwed lock on oar seat, so in actual installation is crossed into, the propeller of unmanned plane is installed the most loaded down with trivial details, time-consuming the longest, one propeller needs four screw tightenings, one unmanned plane needs to install eight propellers, eight propellers need to install 32 screws, thus make the installation of unmanned plane propeller and to pull down process the most loaded down with trivial details, need to send out and take the substantial amounts of time.Due to propeller to pull down process the most loaded down with trivial details, so when being transported by unmanned plane, propeller typically will not be pulled down, which results in and need bigger parking space, transport to get up inconvenience, and transport old the highest.
Utility model content
For solving above-mentioned problems of the prior art, this utility model provides a kind of unmanned plane propeller rapid dismounting apparatus so that installation and the process of pulling down of unmanned plane propeller are simple, convenient.
The technical solution of the utility model is: a kind of unmanned plane propeller rapid dismounting apparatus, including:
Footstock, it is fixing with propeller is connected, and is provided with bar shaped boss, is provided with the first through hole inside described bar shaped boss along its length in the middle of described footstock bottom surface, and described first through hole is respectively provided on two sides with the strip through-hole communicated with this first through hole；
Base, it is fixed with motor and is connected, in the middle of described base top surface, concave shaped is in strip groove, described base top surface is positioned at the length direction both sides indent respectively of described strip groove and forms the recess towards this base center, each described recess has relative two sidewall, and each described sidewall is provided with draw-in groove, described bar shaped boss is placed in described strip groove；
Two buttons, it is respectively equipped with radial direction through hole on said two button, one end of two buttons is placed in this first through hole from described first through hole two ends respectively, the other end stretches out this first through hole respectively, one alligator clamp is between said two button, being provided with straight pin in radial direction through hole, these straight pin both ends are stretched out and described card slot fit from described strip through-hole.
The bottom surface of described footstock is positioned at longitudinal both sides of described bar shaped boss and is provided with positive stop lug boss, and the end face of described base is positioned at indent outside described recess and forms the stopper slot coordinated with described positive stop lug boss.
The sidewall of described base is provided with the second through hole connected with draw-in groove.
Described footstock is provided with the screwed hole being connected with propeller, and described base is provided with the counter sink being connected with motor.
Footstock just by pressing button can be connected with base and separate by the unmanned plane propeller rapid dismounting apparatus that this utility model provides so that installation and the process of pulling down of unmanned plane propeller are simple, convenient, the time greatly reduce installation, pulling down.
Accompanying drawing explanation
Fig. 1 is the three-dimensional structure diagram of this utility model unmanned plane propeller rapid dismounting apparatus；
Fig. 2 is the explosive view of this utility model unmanned plane propeller rapid dismounting apparatus.
Detailed description of the invention
As depicted in figs. 1 and 2, the unmanned plane propeller rapid dismounting apparatus that the utility model proposes, including footstock 10, base 30, two straight pins 40 of 20, two buttons and spring 50.
Footstock 10 is provided with bar shaped boss 11 in the middle of bottom surface, bar shaped boss 11 is internal is provided with the first through hole 12 along its length, first through hole 12 is respectively provided on two sides with the strip through-hole 13 communicated with this first through hole 12, in the present embodiment, the first through hole 12 is respectively provided on two sides with two spaced apart strip through-holes 13 communicated with the first through hole 12；Can also be that the first through hole 12 both sides are provided with a strip through-hole 13.
In the middle of base 20 end face, concave shaped is in strip groove 21, and base 20 end face is positioned at the length direction both sides indent respectively of strip groove 21 and forms the recess 22 towards this base 20 center, and each recess 22 has relative two sidewall, and each sidewall is provided with draw-in groove 23.
Two buttons 30, in cylinder, two buttons 30 are respectively equipped with radial direction through hole 31.
One end of two buttons 30 is placed in this first through hole 12 from the first through hole 12 two ends respectively, the other end stretches out this first through hole 12 respectively, spring 50 is clipped between two buttons 30, the middle part of two straight pins 40 is respectively placed in the radial direction through hole 31 of two buttons 30, and two ends of these two straight pins 40 stretch out from strip through-hole 13 respectively, bar shaped boss 11 is placed in strip groove 21, when not pressing two buttons 30, the elastic card of spring 50 is passed through in draw-in groove 23 in two ends of straight pin 40, realize the connection of footstock 10 and base 20, during two buttons 30 of pressing, two ends of two straight pins 40 skid off respectively in draw-in groove 23, realize footstock 10 to separate with base 20.
The bottom surface of footstock 10 is positioned at longitudinal both sides of bar shaped boss 11 and is provided with positive stop lug boss 14, the end face of base 20 is positioned at indent outside recess 22 and forms the stopper slot 24 coordinated with limit convex 14, by arranging coordinating of positive stop lug boss 14 and stopper slot 24, and the coordinating so that not having relative motion between footstock 10 and base 20 of bar shaped boss 11 and strip groove 21.The sidewall of base 20 is provided with the second through hole 25 connected with draw-in groove 23, and this second through hole 25 is used for housing straight pin 40.
Footstock 10 is provided with the screwed hole 15 being connected with propeller, and footstock is connected with propeller by screw through screwed hole, and base 20 is provided with the counter sink being connected with motor, and base is connected with motor by screw through counter sink.
nullFirst the first through hole is put in one end of a button when assembling unmanned plane propeller rapid dismounting apparatus of the present utility model，The other end stretches out，The most again one end of a straight pin is stretched out from the strip through-hole of opposite side after the radial direction through hole button from the strip through-hole of side，The other end stretches out the strip through-hole of side too，Then spring is put into from the other end of the first through hole，The most again the first through hole is put in one end of another button，The other end stretches out，Another straight pin is installed in the same way，Two buttons are because the elastic force of spring can move out，But due to straight pin and strip through-hole position-limiting action，Make two buttons can in the first through hole relative motion，Press two buttons，Two straight pins come closer，Then bar shaped boss is put into strip groove，Positive stop lug boss puts into stopper slot，Unclamp two buttons again，Two buttons move out because of elastic force，Thus drive two ends of straight pin to move in draw-in groove，And be stuck in draw-in groove，Realize the connection of footstock and base，Two buttons of pressing again，Realize footstock to separate with base.
Footstock just by pressing button can be connected with base and separate by unmanned plane propeller rapid dismounting apparatus of the present utility model so that installation and the process of pulling down of unmanned plane propeller are simple, convenient, the time greatly reduce installation, pulling down；Additionally, deposit at needs, when transport, we the most quickly can unload propeller from motor, which reduce parking space, convenient transportation, saves old of transport, when needs use unmanned plane, we have only to pin button and can be contained on unmanned plane by propeller, install very convenient；After making to be finished, we equally pin button and quickly propeller are unloaded from unmanned plane, load in transport case；Also overcome the indiscernible problem of the most positive and negative oar simultaneously.
Above specific embodiment is only in order to illustrate design of the present utility model, and those of ordinary skill in the art can make various deformation and change under design of the present utility model, within these deformation and change are included in protection domain of the present utility model.
Claims (4)
1. a unmanned plane propeller rapid dismounting apparatus, it is characterised in that including:
Footstock (10), it is fixed with propeller and is connected, being provided with bar shaped boss (11) in the middle of described footstock bottom surface, be provided with the first through hole (12) inside described bar shaped boss along its length, described first through hole is respectively provided on two sides with the strip through-hole (13) communicated with this first through hole；
Base (20), it is fixed with motor and is connected, in the middle of described base top surface, concave shaped is in strip groove (21), described base top surface is positioned at the length direction both sides indent respectively of described strip groove and forms the recess (22) towards this base center, each described recess has relative two sidewall, and each described sidewall is provided with draw-in groove (23), described bar shaped boss is placed in described strip groove；Two buttons (30), radial direction through hole (31) it is respectively equipped with on said two button, one end of two buttons is placed in this first through hole from described first through hole two ends respectively, the other end stretches out this first through hole respectively, one spring (50) is clipped between said two button, being provided with straight pin (40) in radial direction through hole, these straight pin both ends are stretched out and described card slot fit from described strip through-hole.
Unmanned plane propeller rapid dismounting apparatus the most according to claim 1, it is characterized in that: the bottom surface of described footstock (10) is positioned at longitudinal both sides of described bar shaped boss (11) and is provided with positive stop lug boss (14), the end face of described base (20) is positioned at described recess (22) outside indent and forms the stopper slot (24) coordinated with described positive stop lug boss.
Unmanned plane propeller rapid dismounting apparatus the most according to claim 1 and 2, it is characterised in that: the sidewall of described base (20) is provided with the second through hole (25) connected with draw-in groove (23).
Unmanned plane propeller rapid dismounting apparatus the most according to claim 1 and 2, it is characterized in that: described footstock (10) is provided with the screwed hole (15) being connected with propeller, described base (20) is provided with the counter sink being connected with motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620440737.XU CN205770123U (en) | 2016-05-16 | 2016-05-16 | A kind of unmanned plane propeller rapid dismounting apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620440737.XU CN205770123U (en) | 2016-05-16 | 2016-05-16 | A kind of unmanned plane propeller rapid dismounting apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205770123U true CN205770123U (en) | 2016-12-07 |
Family
ID=57410134
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620440737.XU Active CN205770123U (en) | 2016-05-16 | 2016-05-16 | A kind of unmanned plane propeller rapid dismounting apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205770123U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018107964A1 (en) * | 2016-12-14 | 2018-06-21 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle and power assembly, propeller and propeller base assembly thereof |
| CN108891579A (en) * | 2018-08-21 | 2018-11-27 | 上海歌尔泰克机器人有限公司 | A kind of fast assembling disassembling structure and the unmanned plane with the structure |
| WO2020253621A1 (en) * | 2019-06-18 | 2020-12-24 | 深圳高度创新技术有限公司 | Support frame fitting structure |
-
2016
- 2016-05-16 CN CN201620440737.XU patent/CN205770123U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018107964A1 (en) * | 2016-12-14 | 2018-06-21 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle and power assembly, propeller and propeller base assembly thereof |
| CN108891579A (en) * | 2018-08-21 | 2018-11-27 | 上海歌尔泰克机器人有限公司 | A kind of fast assembling disassembling structure and the unmanned plane with the structure |
| CN108891579B (en) * | 2018-08-21 | 2021-09-21 | 上海歌尔泰克机器人有限公司 | Quick assembly disassembly structure and have unmanned aerial vehicle of this structure |
| WO2020253621A1 (en) * | 2019-06-18 | 2020-12-24 | 深圳高度创新技术有限公司 | Support frame fitting structure |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205770123U (en) | A kind of unmanned plane propeller rapid dismounting apparatus | |
| US20070234501A1 (en) | Windshield wiper connecter | |
| US20180118330A1 (en) | Detachable propeller holder device | |
| CN106219176A (en) | The conveying arrangement of instrument board | |
| KR100887386B1 (en) | Core unit | |
| CN106585978B (en) | Fixed oar subassembly | |
| CN211869537U (en) | Transportation device mounted on bionic robot and convenient to mount and capable of preventing collision | |
| CN103047233A (en) | Positioning clamp used for fastening support | |
| CN208997111U (en) | A kind of one man operation's Quick connection part and LED display cabinet | |
| WO2016173094A1 (en) | Fixture and apparatus connecting structure | |
| CN207568752U (en) | Motor-vehicle fuel pump mounting structure and motorcycle with electronic fuel injection system | |
| CN105151128A (en) | Automobile panel clamping structure | |
| CN208264095U (en) | Semitrailer container lock pin mechanism | |
| CN208662242U (en) | A kind of mouthful of frame class sheet metal component on-right angle hole flanging special molding mould | |
| CN205943806U (en) | Door window plastics riser switch | |
| CN216421586U (en) | Sensor inner core bush press-fit tool | |
| CN205780079U (en) | A kind of attachment means in quick elimination gap | |
| CN205531194U (en) | Make things convenient for timber apron of dismouting | |
| CN204663164U (en) | A kind of Door lock casing | |
| CN205684580U (en) | The fastener of a kind of curtain wall panel mounting bar and the diel of installing hole | |
| CN215255379U (en) | Mechanical execution structure for logistics lock of Internet of things | |
| CN205469194U (en) | Vehicle for conveying sports goods | |
| CN217597663U (en) | Compact dovetail mechanism for side finishing process | |
| CN108646868A (en) | One kind is towards whole machine cabinet server m.2 device for fixing hard disk and its fixing means | |
| CN214775168U (en) | Aluminum alloy wheel insert structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |