CN209064346U - A kind of unmanned plane modularization wing - Google Patents
A kind of unmanned plane modularization wing Download PDFInfo
- Publication number
- CN209064346U CN209064346U CN201821783870.0U CN201821783870U CN209064346U CN 209064346 U CN209064346 U CN 209064346U CN 201821783870 U CN201821783870 U CN 201821783870U CN 209064346 U CN209064346 U CN 209064346U
- Authority
- CN
- China
- Prior art keywords
- wing
- submodule
- unmanned plane
- interface
- modularization
- 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
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A kind of unmanned plane modularization wing belongs to unmanned plane technical field of structures, it is therefore intended that can only form specific type after solving the problems, such as wing and fuselage adaptation of the existing technology.A kind of unmanned plane modularization wing of the utility model is formed by connecting by multiple wing submodules, is detachably connected between two neighboring wing submodule by multiple groups module interface.A kind of unmanned plane modularization wing of the utility model uses modularized design, and wing-body is connected and fixed by multiple wing submodules by module interface, and fast to insert connection, structure is simple, is that a kind of suitability is high, versatile unmanned plane modularization wing.
Description
Technical field
The utility model belongs to unmanned plane technical field of structures, and in particular to a kind of unmanned plane modularization wing.
Background technique
When traditional unmanned aerial vehicle design, wing is only capable of forming specific type after being adapted to fuselage, and different type of machines needs are set
Different fuselages, wing, empennage and rotor are counted, more design times are not only needed, it is also necessary to be designed for each type different
Mold needs more costs.
Utility model content
The purpose of this utility model is that propose a kind of unmanned plane modularization wing, solve wing of the existing technology and
The problem of specific type can only be formed after fuselage adaptation.
To achieve the above object, a kind of unmanned plane modularization wing of the utility model connected by multiple wing submodules and
At being detachably connected with, be arranged on each wing submodule organic by multiple groups module interface between two neighboring wing submodule
Body interface and rotor interface.
The rib that each wing submodule (1), which includes two beams disposed in parallel, to be vertically fixedly connected with the beam with
And the wing plate on the outside of the skeleton of beam and rib composition is set.
Module interface described in every group includes:
Two sub- Module sleeves of coaxial arrangement, two submodule casings are separately positioned on two adjacent wing
The opposite end of module；
The both ends connecting sleeve with two submodule casing connections respectively；
And be separately positioned on two neighboring wing submodule and respectively with the submodule quill in two submodules
Two vertical spring catch of line, spring catch radially penetrate or pop up submodule casing and connecting sleeve.
Module interface at least two groups between two neighboring wing submodule.
Corresponding position is provided with fuselage connecting interface, rotor connecting interface and empennage and connects on the wing submodule
Mouthful.
The utility model has the following beneficial effects: a kind of unmanned plane modularization wing of the utility model is set using modularization
Meter, wing-body are connected and fixed by multiple wing submodules by module interface, and fast to insert connection, structure is simple, is a kind of adaptation
Property high, versatile unmanned plane modularization wing.It is versatile, suitability is high is: for different magnitude of aircraft, such as
45kg and 90kg aircraft, corresponding fuselage, wing, empennage and rotor are inevitable different.So I now devised wing
Module arranges fuselage interface, wing interface, empennage and rotor interface thereon, then synthesizing one using 2 wing submodules
The wing of 45kg aircraft synthesizes the wing of a 90kg aircraft using 4 wing submodules.Therefore each wing design is saved
Cost, different wings are processed to use different molds, therefore save die cost, connected by interface bolt, therefore save
Aircraft assembly time is saved.
Detailed description of the invention
Fig. 1 is a kind of unmanned plane modularization wing overall structure diagram of the utility model；
Fig. 2 is a kind of unmanned plane modularization wing structure explosive view of the utility model；
Fig. 3 is a kind of each wing sub-modular structure schematic diagram of unmanned plane modularization wing of the utility model；
Fig. 4 is the middle portion the E schematic enlarged-scale view of Fig. 3；
Fig. 5 is the portion D schematic enlarged-scale view in Fig. 3；
Wherein: 1, wing submodule, 101, beam, 102, rib, 2, submodule casing, 3, connecting sleeve, 4, spring catch, 5, three
Hornblock.
Specific embodiment
The embodiments of the present invention is described further with reference to the accompanying drawing.
Referring to attached drawing 1- attached drawing 5, a kind of unmanned plane modularization wing of the utility model is connected by multiple wing submodules 1
It forms, is detachably connected between two neighboring wing submodule 1 by multiple groups module interface.It is arranged on each wing submodule 1
There are fuselage interface and rotor interface.
Each wing submodule 1 includes what two beams 101 disposed in parallel were vertically fixedly connected with the beam 101
Rib 102 and the wing plate being arranged on the outside of the skeleton that beam 101 and rib 102 form.
Rotor interface includes corner block 5, and the corner block 5 realization Nian Jie with beam 101 and rib 102 is fixed, pre- in corner block 5
Cylindrical steel sleeve is buried, steel bushing is Nian Jie with corner block 5, and bolt, which passes through steel bushing and is screwed on rotor hickey, realizes rotor and wing
It is fixed.
Fuselage interface is using a kind of entitled unmanned wing body locking dress of wing body separate type of Patent No. 2018111452405
It sets and the locking device of locking method is realized, stay hook and rib are fixed by screw assembly, and stay hook is in wing body locking device
The fixation of wing and fuselage is realized in movable hook locking in one part, stay hook and wing body locking device.
Module interface described in every group includes:
Two sub- Module sleeves 2 of coaxial arrangement, two submodule casings 2 are separately positioned on two adjacent wings
The opposite end of submodule 1；Submodule casing 2 in wing submodule 1 beam or rib it is affixed；
The connecting sleeve 3 that both ends are connected with two submodule casings 2 respectively；
And be separately positioned on two neighboring wing submodule 1 and respectively with the submodule casing 2 in two submodules
Two vertical spring catch 4 of axis, spring catch 4 is radial to penetrate or pops up submodule casing 2 and connecting sleeve 3.
Connecting sleeve 3 is inserted into the submodule casing 2 in two wing submodules 1, in connecting sleeve 3 and wing submodule 1
Submodule casing 2 be respectively provided with hole location, spring catch 4 is inserted into the hole location of connecting sleeve 3 and submodule casing 2, realizes wing submodule
Interconnection between block 1.
Module interface at least two groups between the 1 of two neighboring wing submodule.
Corresponding position is provided with fuselage connecting interface, rotor connecting interface and empennage connection on the wing submodule 1
Interface.
Connecting sleeve 3 is inserted into five freedom degrees of limitation in submodule casing 2, limits remaining next freedom by spring catch 4
Degree effectively transmits lift and moment of flexure.
Modularization wing is made of three wing submodules 1, and the utility model is not limited only to three wing submodules 1.
Two interfaces are arranged in 1 end face of wing submodule, and 1 end face of the utility model wing submodule is not limited only to two and connects
Mouthful.
Claims (5)
1. a kind of unmanned plane modularization wing, which is characterized in that it is formed by connecting by multiple wing submodules (1), two neighboring machine
Wing submodule is detachably connected between (1) by multiple groups module interface, be provided on each wing submodule (1) fuselage interface and
Rotor interface.
2. a kind of unmanned plane modularization wing according to claim 1, which is characterized in that each wing submodule
(1) rib (102) and be arranged in beam that include two beams (101) disposed in parallel be vertically fixedly connected with the beam (101)
(101) and rib (102) composition skeleton on the outside of wing plate.
3. a kind of unmanned plane modularization wing according to claim 1, which is characterized in that module interface packet described in every group
It includes:
Two sub- Module sleeves (2) of coaxial arrangement, two submodule casings (2) are separately positioned on two adjacent wings
The opposite end of submodule (1)；
The connecting sleeve (3) that both ends are connected with two submodule casings (2) respectively；
And be separately positioned on two neighboring wing submodule (1) and respectively with the submodule casing (2) in two submodules
Two vertical spring catch (4) of axis, spring catch (4) radially penetrate or pop up submodule casing (2) and connecting sleeve (3).
4. a kind of unmanned plane modularization wing according to claim 1 or 2 or 3, which is characterized in that two neighboring wing
Module interface at least two groups between module (1).
5. a kind of unmanned plane modularization wing according to claim 1, which is characterized in that on the wing submodule (1)
Corresponding position is provided with fuselage connecting interface, rotor connecting interface and empennage connecting interface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821783870.0U CN209064346U (en) | 2018-10-31 | 2018-10-31 | A kind of unmanned plane modularization wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821783870.0U CN209064346U (en) | 2018-10-31 | 2018-10-31 | A kind of unmanned plane modularization wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209064346U true CN209064346U (en) | 2019-07-05 |
Family
ID=67096976
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821783870.0U Active CN209064346U (en) | 2018-10-31 | 2018-10-31 | A kind of unmanned plane modularization wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209064346U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109178293A (en) * | 2018-10-31 | 2019-01-11 | 长光卫星技术有限公司 | A kind of unmanned plane modularization wing |
| CN115783235A (en) * | 2022-11-04 | 2023-03-14 | 厦门腾希航空科技有限公司 | Modularized wing aircraft |
| CN115783257A (en) * | 2022-11-04 | 2023-03-14 | 厦门腾希航空科技有限公司 | Composite wing module |
-
2018
- 2018-10-31 CN CN201821783870.0U patent/CN209064346U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109178293A (en) * | 2018-10-31 | 2019-01-11 | 长光卫星技术有限公司 | A kind of unmanned plane modularization wing |
| CN115783235A (en) * | 2022-11-04 | 2023-03-14 | 厦门腾希航空科技有限公司 | Modularized wing aircraft |
| CN115783257A (en) * | 2022-11-04 | 2023-03-14 | 厦门腾希航空科技有限公司 | Composite wing module |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209064346U (en) | A kind of unmanned plane modularization wing | |
| CN204173154U (en) | A kind of modularized combination type unmanned plane | |
| CN103921116B (en) | A kind of aircraft target ship flexible assembly system | |
| CA2893338C (en) | Fuselage structure of an unmanned helicopter | |
| CN103101632B (en) | Unmanned aerial vehicle body modularization folding tool platform and usage of the same | |
| CN109178293A (en) | A kind of unmanned plane modularization wing | |
| CN108791800B (en) | Connecting fastener for unmanned aerial vehicle | |
| DE102008023194A1 (en) | Airplane e.g. sail or motor driven flying module, has carrying surface and control unit connected with airplane- or flying module body via permanent magnets, whose plan surfaces are displaced in direction of module body | |
| CN203245761U (en) | Push-pull-type positioning device | |
| CN104338825A (en) | Auxiliary device for punching equipment clamp | |
| CN206042616U (en) | Integrated quick -witted case of avionic device | |
| CN102765472B (en) | Modular connection device for airplane body | |
| CN204368408U (en) | For being fixedly connected with the mounting structure of model plane fuselage and wing | |
| CN105372121A (en) | Flexibility inspection clamp of aircraft wing shot blasting wallplate skin | |
| CN201394360Y (en) | Model airplane no-aileron headstock assembly | |
| CN205010465U (en) | Unmanned aerial vehicle | |
| CN202506125U (en) | Quick-dismounting structure for wings | |
| CN206202704U (en) | The modular removable formula nacelle of unmanned plane | |
| CN204197267U (en) | A kind of fixed-wing unmanned plane body two sectional type rapid dismounting apparatus | |
| CN204688414U (en) | Horn assembly, frame and unmanned plane | |
| CN205168870U (en) | Aircraft wing body connection structure | |
| CN206704558U (en) | A kind of small-sized fixed-wing unmanned plane load cabin modular unit | |
| CN107970621B (en) | Modular model airplane | |
| CN103759622B (en) | A kind of aircraft wing long purlin flexible testing frock | |
| CN206364420U (en) | A kind of special assembly tooling of portable solid insulation switch cabinet |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: No. 1299, Mingxi Road, Beihu science and Technology Development Zone, Changchun City, Jilin Province Patentee after: Changguang Satellite Technology Co.,Ltd. Address before: No.1759 Mingxi Road, Gaoxin North District, Changchun City, Jilin Province Patentee before: CHANG GUANG SATELLITE TECHNOLOGY Co.,Ltd. |