CN202593850U - Unmanned plane wing installing mechanism capable of being mounted and dismounted quickly - Google Patents
Unmanned plane wing installing mechanism capable of being mounted and dismounted quickly Download PDFInfo
- Publication number
- CN202593850U CN202593850U CN 201120535845 CN201120535845U CN202593850U CN 202593850 U CN202593850 U CN 202593850U CN 201120535845 CN201120535845 CN 201120535845 CN 201120535845 U CN201120535845 U CN 201120535845U CN 202593850 U CN202593850 U CN 202593850U
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- wing
- screw
- plane
- fuselage
- unmanned plane
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Abstract
The utility model discloses an unmanned plane wing installing mechanism capable of being mounted and dismounted quickly. The unmanned plane wing installing mechanism comprises a plane wing clamping groove (1), a plane wing screw (3), a plane body clamping groove (4) and a plane body screw (2), wherein the plane wing clamping groove (1) and the plane wing screw (3) are arranged on a plane wing, and the plane body clamping groove (4) and the plane body screw (2) are arranged on a plane body. When the unmanned plane wing installing mechanism is installed, the plane wing screw (3) is clamped into the plane body clamping groove (4), and the plane body screw (2) is clamped into the plane wing clamping groove (1). The unmanned plane wing installing mechanism can enable installation and connection of the plane wing and the plane body to be convenient and quick and improve installing and operating speed, and has the advantages of being simple, low in price, safe, reliable, convenient to operate and capable of being used repeatedly.
Description
Technical field
The utility model belongs to the unmanned plane field, is specifically related to a kind of unmanned plane wing bindiny mechanism of fast demountable.
Background technology
Unmanned plane is a kind of by unpiloted aerocraft on power driven, the machine.It is made up of body, engine installation, flicon and managerial tools, emission reclaiming scrap etc. usually, can remote control or flight automatically, can disposablely use, and also can reclaim, repeated use.It is one of current new-and high-tech weaponry and equipment, is widely used in battlefield investigation, electronic countermeasure, lesion assessment, many warlike operations such as attack over the ground after the war, is the requisite equipment of IT-based warfare.At civil area, it has been widely used in fields such as air remote sensing, aerial mapping, forest fire protection, coastline patrol.It is a kind of very effective and practical tactical reconnaissance equipment that individual soldier's hand is thrown the scounting aeroplane system, can effectively assist the smooth completion of each item combat duty.This unmanned plane carries different equipment can accomplish different combat duties.It has that cost is low, volume is little, in light weight, simple to operate, characteristics such as adaptive faculty strong, be easy to carry, assemble rapidly, is specially adapted to complicated geographical environment, shortens the reaction time greatly; Improve its combat capabilities; Realize battlefield " zero injures and deaths " simultaneously, greatly reduce cost, raise the efficiency.
Summary of the invention
More loaded down with trivial details in order to solve existing unmanned plane wing Assembly &Disassembly; Wing is safeguarded and is changed inconvenient problem, the utility model discloses a kind of unmanned plane wing installing mechanism of fast demountable, comprises the wing draw-in groove and the wing screw that are arranged on the wing; And be arranged on fuselage draw-in groove and the fuselage screw on the fuselage; During installation, the wing screw snaps in the fuselage draw-in groove, and the fuselage screw snaps in the wing draw-in groove.
Further, wing is provided with the wing screw, and the wing screw is screwed in the wing screw, and fuselage is provided with the fuselage screw, and the fuselage screw is screwed in the fuselage screw.
Further, be reserved with an amount of space between screw and the screw.
The outstanding characteristics of the utility model are:
1, only needs two screws just can the wing and the fuselage of unmanned plane to be coupled together, increased substantially the speed of installation exercise.
2, when aircraft landing receives ground-surface impulsive force, wing avoids fuselage to bear too big overload because inertia can break away from fuselage voluntarily.
3, because the Assembly &Disassembly process is simple,, improved the Operational Effectiveness Rat of aircraft so the unmanned plane wing can be safeguarded and change very easily.
Description of drawings
Fig. 1 is a unmanned plane wing draw-in groove scheme drawing;
Fig. 2 is a unmanned aerial vehicle body draw-in groove scheme drawing;
Fig. 3 is that the wing draw-in groove combines scheme drawing with the fuselage screw;
Fig. 4 is that the wing screw combines scheme drawing with the fuselage draw-in groove.
The specific embodiment
Below in conjunction with accompanying drawing the utility model is specifically described.
Shown in Fig. 1-4; The unmanned plane wing installing mechanism of the utility model comprises the wing draw-in groove 1 and wing screw that is arranged on the wing; And be arranged on the fuselage draw-in groove 4 and fuselage screw on the fuselage; Be screwed with wing screw 3 in the wing screw, be screwed with in the fuselage screw between 2, two screws of fuselage screw and corresponding screw and be reserved with an amount of space.
During installation, wing draw-in groove 1 is aimed at fuselage screw 2, simultaneously wing screw 3 is aimed at fuselage draw-in groove 4, to pusher, make two screws all be stuck in cooresponding draw-in groove bottom after aiming at, wing and fuselage are coupled together.
It is understandable that above embodiment only is the illustrative embodiments that adopts for the principle that the utility model is described, yet utility model is not limited thereto.For the one of ordinary skilled in the art, under the situation of spirit that does not break away from the utility model and essence, can make various modification and improvement, these modification are the protection domain of the utility model with improving also real.
Claims (3)
1. the unmanned plane wing installing mechanism of a fast demountable; It is characterized in that: comprise the wing draw-in groove (1) and the wing screw (3) that are arranged on the wing; And be arranged on fuselage draw-in groove (4) and the fuselage screw (2) on the fuselage; During installation, wing screw (3) snaps in the fuselage draw-in groove (4), and fuselage screw (2) snaps in the wing draw-in groove (1).
2. unmanned plane wing installing mechanism according to claim 1, it is characterized in that: wing is provided with the wing screw, and wing screw (3) is screwed in the wing screw, and fuselage is provided with the fuselage screw, and fuselage screw (2) is screwed in the fuselage screw.
3. unmanned plane wing installing mechanism according to claim 1 and 2 is characterized in that: be reserved with an amount of space between screw and the screw.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120535845 CN202593850U (en) | 2011-12-20 | 2011-12-20 | Unmanned plane wing installing mechanism capable of being mounted and dismounted quickly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120535845 CN202593850U (en) | 2011-12-20 | 2011-12-20 | Unmanned plane wing installing mechanism capable of being mounted and dismounted quickly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202593850U true CN202593850U (en) | 2012-12-12 |
Family
ID=47311415
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201120535845 Expired - Fee Related CN202593850U (en) | 2011-12-20 | 2011-12-20 | Unmanned plane wing installing mechanism capable of being mounted and dismounted quickly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202593850U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105599892A (en) * | 2016-02-04 | 2016-05-25 | 郑州兰旗航空器材制造有限公司 | Small-size unmanned aerial vehicle |
| CN105667790A (en) * | 2016-01-15 | 2016-06-15 | 中国人民解放军国防科学技术大学 | General layout of unmanned aerial vehicle capable of taking off with catapult assisted and being recovered by bumping net |
| CN106005369A (en) * | 2016-07-24 | 2016-10-12 | 尹鸿俊 | Unmanned aerial vehicle |
| CN107344619A (en) * | 2016-05-04 | 2017-11-14 | 上海钛灵盾无人机技术有限公司 | A kind of plant protection unmanned plane |
-
2011
- 2011-12-20 CN CN 201120535845 patent/CN202593850U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105667790A (en) * | 2016-01-15 | 2016-06-15 | 中国人民解放军国防科学技术大学 | General layout of unmanned aerial vehicle capable of taking off with catapult assisted and being recovered by bumping net |
| CN105599892A (en) * | 2016-02-04 | 2016-05-25 | 郑州兰旗航空器材制造有限公司 | Small-size unmanned aerial vehicle |
| CN107344619A (en) * | 2016-05-04 | 2017-11-14 | 上海钛灵盾无人机技术有限公司 | A kind of plant protection unmanned plane |
| CN106005369A (en) * | 2016-07-24 | 2016-10-12 | 尹鸿俊 | Unmanned aerial vehicle |
| CN106005369B (en) * | 2016-07-24 | 2018-07-03 | 尹鸿俊 | A kind of unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121212 Termination date: 20131220 |