CN206031756U - Unmanned aerial vehicle wing - Google Patents
Unmanned aerial vehicle wing Download PDFInfo
- Publication number
- CN206031756U CN206031756U CN201620991335.9U CN201620991335U CN206031756U CN 206031756 U CN206031756 U CN 206031756U CN 201620991335 U CN201620991335 U CN 201620991335U CN 206031756 U CN206031756 U CN 206031756U
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- CN
- China
- Prior art keywords
- wing
- rib
- beam type
- type bolt
- fuselage
- 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.)
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Abstract
The utility model provides an unmanned aerial vehicle wing, includes wing body, wing body has coated the wing covering, the wing covering is honeycomb formula combined material shell structure, wing covering middle part is provided with rib no. 1, rib no. 1 is connected with the horizontal big beam type bolt that sets up in wing middle part, big beam type bolt is connected with the rib no. 2 of wing inner edge setting, the wing is connected with the fuselage through big beam type bolt, before the wing, sell through the prelocalization respectively the rear end, rear positioning pins is connected with the fuselage, through big beam type bolt, prelocalization round pin and rear positioning pins are connected wing and fuselage fixed, the aircraft can normal flight, the wing covering can increase the power of shocking resistance of wing, increase the wing rigidity simultaneously, make its non -deformable, big beam type bolt can will be done all can through rib no. 1 and rib no. 2, and balancedly dispersion to whole wing is surperficial, it is even to make the wing atress, and is simple in structure, the flue is high in intensity, convenient maintenance, no environmental pollution and low cost.
Description
Technical field
This utility model is related to aircraft wing technical field, more particularly to a kind of unmanned plane wing.
Background technology
Existing aircraft wing structure is complicated, has that rough wing cover, wing and body connection structure be loaded down with trivial details, wing
The shortcomings of low intensity, inconvenient maintenance, it is impossible to meet the demand of practical application well.
The content of the invention
In order to overcome the above-mentioned deficiencies of the prior art, the purpose of this utility model is to propose a kind of unmanned plane wing, its
Easy to maintenance, low cost, with simple structure, intensity is high the characteristics of.
To achieve these goals, the technical solution adopted in the utility model is：
A kind of unmanned plane wing, including wing-body, wing-body overlying has wing cover l, and the wing cover 1 is honeybee
Socket composite shell structure, is provided with rib 1 in the middle part of wing cover 1, in the middle part of rib 1 and wing, horizontally set is big
Beam type latch 2 is connected, and the rib 25 that fall crossbeam type latch 2 is arranged with wing inner edge is connected, and wing passes through fall crossbeam type latch 2
It is connected with fuselage, wing front and back ends are connected with fuselage by prelocalization pin 3, rear alignment pin 4 respectively.
The rib 1 is vertical with fall crossbeam type latch 2 to be connected.
The rib 25 is vertical with fall crossbeam type latch 2 to be connected.
This utility model employs the wing cover of honeycomb fashion composite shell structure, by increasing capacitance it is possible to increase wing intensity, and
The interior external carbuncle of whole wing is distributed in by shell structure transmission, wing rigidity is increased while anti-impact force is strengthened,
It is unlikely to deform which, so make wing intensity big；Fall crossbeam type latch can pass through rib one and power is balancedly disperseed by rib two
To whole aerofoil surface, wing uniform force is made；This utility model wing is simple with body connection structure, reduces manufacturing cost
And work forming efficiency is improve, while being easy to maintenance.
Description of the drawings
Fig. 1 is top view of the present utility model.
Fig. 2 is side view of the present utility model.
Specific embodiment
Below in conjunction with the accompanying drawings this utility model is described in further detail.
Referring to Fig. 1, Fig. 2, a kind of unmanned plane wing, including wing-body, wing-body overlying has wing cover l, described
Wing cover 1 is honeycomb fashion composite shell structure, is provided with rib 1, in rib 1 and wing in the middle part of wing cover 1
The fall crossbeam type latch 2 of portion's horizontally set is vertical to be connected, and the rib 25 that fall crossbeam type latch 2 is arranged with wing inner edge is vertical to be connected, machine
The wing is connected with fuselage by fall crossbeam type latch 2, and wing front and back ends are connected with fuselage by prelocalization pin 3, rear alignment pin 4 respectively.
Operation principle of the present utility model is：
Wing and fuselage are connected by fall crossbeam type latch 2, prelocalization pin 3 and rear alignment pin 4, aircraft can be normal
Flight.During work, wing cover 1 can increase the anti-impact force of wing, while increasing wing rigidity so as to be unlikely to deform.Greatly
Beam type latch 2 can pass through rib 1 and power is balancedly dispersed to rib 25 whole aerofoil surface, makes wing uniform force.
Claims (3)
1. a kind of unmanned plane wing, including wing-body, it is characterised in that wing-body overlying has wing cover (1), the machine
Wing eyelid covering (1) is honeycomb fashion composite shell structure, is provided with rib one (6) in the middle part of wing cover (1), rib one (6) with
In the middle part of wing, the fall crossbeam type latch (2) of horizontally set is connected, the rib two (5) that fall crossbeam type latch (2) is arranged with wing inner edge
It is connected, wing is connected with fuselage by fall crossbeam type latch (2), wing front and back ends are respectively by prelocalization pin (3), rear positioning
Pin (4) is connected with fuselage.
2. a kind of unmanned plane wing according to claim 1, it is characterised in that the rib one (6) and fall crossbeam type latch
(2) it is vertical to connect.
3. a kind of unmanned plane wing according to claim 1, it is characterised in that the rib two (5) and fall crossbeam type latch
(2) it is vertical to connect.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620991335.9U CN206031756U (en) | 2016-08-30 | 2016-08-30 | Unmanned aerial vehicle wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620991335.9U CN206031756U (en) | 2016-08-30 | 2016-08-30 | Unmanned aerial vehicle wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206031756U true CN206031756U (en) | 2017-03-22 |
Family
ID=58302324
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620991335.9U Active CN206031756U (en) | 2016-08-30 | 2016-08-30 | Unmanned aerial vehicle wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206031756U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109470089A (en) * | 2018-11-23 | 2019-03-15 | 江西洪都航空工业集团有限责任公司 | A kind of short beam sandwich mini-bomb wing structure |
| CN110294100A (en) * | 2018-03-23 | 2019-10-01 | 北京京东尚科信息技术有限公司 | Fixed Wing AirVehicle and its wing |
-
2016
- 2016-08-30 CN CN201620991335.9U patent/CN206031756U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110294100A (en) * | 2018-03-23 | 2019-10-01 | 北京京东尚科信息技术有限公司 | Fixed Wing AirVehicle and its wing |
| CN109470089A (en) * | 2018-11-23 | 2019-03-15 | 江西洪都航空工业集团有限责任公司 | A kind of short beam sandwich mini-bomb wing structure |
| CN109470089B (en) * | 2018-11-23 | 2021-08-20 | 江西洪都航空工业集团有限责任公司 | Small-size bullet wing structure of short beam core |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |