CN204846356U - Unmanned aerial vehicle wing connecting device - Google Patents
Unmanned aerial vehicle wing connecting device Download PDFInfo
- Publication number
- CN204846356U CN204846356U CN201520332851.6U CN201520332851U CN204846356U CN 204846356 U CN204846356 U CN 204846356U CN 201520332851 U CN201520332851 U CN 201520332851U CN 204846356 U CN204846356 U CN 204846356U
- Authority
- CN
- China
- Prior art keywords
- strut bar
- wing
- slot
- bolts
- connecting device
- 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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- Mutual Connection Of Rods And Tubes (AREA)
Abstract
The utility model relates to an unmanned aerial vehicle wing connecting device, including wing bracing piece, mounting disc, be equipped with the slot of two bendings on the wing bracing piece, be equipped with two bolts that correspond with the slot of two bendings in the mounting disc, be equipped with the locating plate in one side of two bolts, the wing bracing piece passes through the slot of two bendings inserts two bolts, and the wing bracing piece gets into two bolts along the route of the bending of the slot of two bendings, and formation is connected to through locating plate side direction contact, make to form the cartridge that to dismantle fast between wing bracing piece and the mounting disc and be connected. The utility model discloses simple structure, installation easy maintenance, processing is also convenient.
Description
Technical field
The utility model belongs to a kind of unmanned plane, is specifically related to a kind of unmanned plane wing connecting device.
Background technology
Unmanned plane wing connecting device in the past has folding connection, have direct coupled, although subpanel and wing strut bar can be made to link together, but go back Shortcomings: between first subpanel with wing strut bar, adopt screw to be fixedly connected with, dismounting is more time-consuming, take a lot of work, and is not easy to install and maintenance; It two is adopt screw to be fixedly connected with between subpanel with wing strut bar, easily loosens, causes flight failure.It three is adopt screw to be fixedly connected with between subpanel with wing strut bar, because the joint be fixedly connected with will be installed additional, so, processing trouble.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane wing connecting device, and its structure is simple, and installation and maintenance are convenient, and processing also facilitates.
In order to achieve the above object, the utility model has following technical scheme:
A kind of unmanned plane wing connecting device of the present utility model, comprise wing strut bar, subpanel, described wing strut bar is provided with two bending slots, subpanel is provided with two bolts that the slot bending with two is corresponding, locating plate is provided with in the side of two bolts, described wing strut bar inserts two bolts by described two bending slots, wing strut bar enters two bolts along the bending path of two bending slots, formed and connect, and contacted by locating plate side direction, make wing strut bar and formed between subpanel and can the plug-in mounting of quick-detachment be connected.
Wherein, described two bending slots comprise the slot of strut bar end and the slot of strut bar side.
Wherein, the slot of described strut bar end comprises longitudinal socket, oblique slot one, described longitudinal socket is communicated with oblique slot one, and described longitudinal socket path is parallel with the axial direction of wing strut bar, and the axial direction of described oblique slot one path and wing strut bar is acute angle; The slot of described strut bar side comprises lateral insert and oblique slot two, described lateral insert is communicated with oblique slot two, described lateral insert path is vertical with the axial direction of wing strut bar, and the described path of oblique slot two and the axial direction of wing strut bar are acute angle.
Owing to taking above technical scheme, the utility model has the advantage of:
1 the utility model structure is simple;
2 subpanels and wing strut bar install or remove easily, and can save time, saving of labor;
3 is easy to maintenance, and processing also facilitates.
Accompanying drawing explanation
Fig. 1 is the utility model subpanel schematic diagram;
Fig. 2 is the schematic diagram of the birds-eye view of Fig. 1;
Fig. 3 is the schematic diagram of the utility model wing strut bar.
In figure, 1, subpanel; 2, wing strut bar; 3, bolt; 4, locating plate; 5, longitudinal socket; 6, lateral insert; 7, oblique slot one; 8, oblique slot two.
Detailed description of the invention
Following examples for illustration of the utility model, but are not used for limiting scope of the present utility model.
See Fig. 1-3:
A kind of unmanned plane wing connecting device of the present utility model, comprise wing strut bar, subpanel, described wing strut bar is provided with two bending slots, subpanel is provided with two bolts that the slot bending with two is corresponding, locating plate is provided with in the side of two bolts, described wing strut bar inserts two bolts by described two bending slots, wing strut bar enters two bolts along the bending path of two bending slots, formed and connect, and contacted by locating plate side direction, make wing strut bar and formed between subpanel and can the plug-in mounting of quick-detachment be connected.
Wherein, described two bending slots comprise the slot of strut bar end and the slot of strut bar side.
Wherein, the slot of described strut bar end comprises longitudinal socket, oblique slot one, described longitudinal socket is communicated with oblique slot one, and described longitudinal socket path is parallel with the axial direction of wing strut bar, and the axial direction of described oblique slot one path and wing strut bar is acute angle; The slot of described strut bar side comprises lateral insert and oblique slot two, described lateral insert is communicated with oblique slot two, described lateral insert path is vertical with the axial direction of wing strut bar, and the described path of oblique slot two and the axial direction of wing strut bar are acute angle.
Described subpanel is provided with six connecting devices be connected with wing strut bar, and described wing strut bar is provided with several holes, and one is for fixing screw propeller; Two is for expendable weight.Described wing strut bar is cross-sectional plane is square tubular rod segments.
Above-described is only preferred implementation of the present utility model; it should be pointed out that for the person of ordinary skill of the art, under the prerequisite not departing from the utility model creation design; can also make some distortion and improvement, these all belong to protection domain of the present utility model.
Claims (3)
1. a unmanned plane wing connecting device, comprise wing strut bar, subpanel, it is characterized in that: described wing strut bar is provided with two bending slots, subpanel is provided with two bolts that the slot bending with two is corresponding, locating plate is provided with in the side of two bolts, described wing strut bar inserts two bolts by described two bending slots, wing strut bar enters two bolts along the bending path of two bending slots, formed and connect, and contacted by locating plate side direction, make wing strut bar and formed between subpanel and can the plug-in mounting of quick-detachment be connected.
2. a kind of unmanned plane wing connecting device as claimed in claim 1, is characterized in that: described two bending slots comprise the slot of strut bar end and the slot of strut bar side.
3. a kind of unmanned plane wing connecting device as claimed in claim 2, it is characterized in that: the slot of described strut bar end comprises longitudinal socket, oblique slot one, described longitudinal socket is communicated with oblique slot one, described longitudinal socket path is parallel with the axial direction of wing strut bar, and the axial direction of described oblique slot one path and wing strut bar is acute angle; The slot of described strut bar side comprises lateral insert and oblique slot two, described lateral insert is communicated with oblique slot two, described lateral insert path is vertical with the axial direction of wing strut bar, and the described path of oblique slot two and the axial direction of wing strut bar are acute angle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520332851.6U CN204846356U (en) | 2015-05-21 | 2015-05-21 | Unmanned aerial vehicle wing connecting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520332851.6U CN204846356U (en) | 2015-05-21 | 2015-05-21 | Unmanned aerial vehicle wing connecting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204846356U true CN204846356U (en) | 2015-12-09 |
Family
ID=54736931
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520332851.6U Expired - Fee Related CN204846356U (en) | 2015-05-21 | 2015-05-21 | Unmanned aerial vehicle wing connecting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204846356U (en) |
-
2015
- 2015-05-21 CN CN201520332851.6U patent/CN204846356U/en not_active Expired - Fee Related
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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: 20151209 Termination date: 20190521 |