CN208641751U - A kind of model plane wing Quick Release connection structure - Google Patents
A kind of model plane wing Quick Release connection structure Download PDFInfo
- Publication number
- CN208641751U CN208641751U CN201821131171.8U CN201821131171U CN208641751U CN 208641751 U CN208641751 U CN 208641751U CN 201821131171 U CN201821131171 U CN 201821131171U CN 208641751 U CN208641751 U CN 208641751U
- Authority
- CN
- China
- Prior art keywords
- wing
- quick release
- fuselage
- slot
- connection
- 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
Links
- 230000000712 assembly Effects 0.000 claims abstract description 10
- 238000000429 assembly Methods 0.000 claims abstract description 10
- 230000003014 reinforcing effect Effects 0.000 claims description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 8
- 230000006378 damage Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000005194 fractionation Methods 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Landscapes
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The utility model relates to a kind of model plane wing Quick Release connection structures; it includes fuselage connector and wing connection; fuselage connector and wing connection side relative to each other, which can be overlapped, is adjacent to combination and faying face is equipped with clip assembly, positioning component, jack assemblies and Quick Release slot; fuselage connector and wing connection side away from one another are recessed the groove that side is connected for wrapping up fuselage connecting side face with wing respectively; clip assembly includes buckle and card slot; positioning component includes locating piece and locating slot, and Quick Release slot is arranged along the vertical direction.Beneficial effect is: fuselage connector and wing connection quickly can be positioned and are clamped by clip assembly and positioning component, assembling fixation is very convenient when being adjacent to combination, it further include simultaneously Quick Release slot, bottle opener or flat rigid posts are inserted into Quick Release slot, can very easily be dismantled the fuselage connector and wing connection that are adjacent to engagement；Jack assemblies guarantee that not needing external cord can be realized being electrically connected for electric appliance between fuselage and wing.
Description
Technical field
The utility model belongs to aircraft and aviation model field, and in particular to a kind of model plane wing Quick Release connection structure.
Background technique
Currently, model airplane be it is a kind of overweight air, have size limit, with or without engine and cannot
Manned aircraft, general aircraft model is as manned aircraft, mainly by wing, empennage, fuselage, undercarriage, engine
It is formed with control system.The model plane of Today, most are mostly that assembling finishes, because of non-removable model plane, it is inconvenient to there is storage
And the problem of can not being convenient for changing after damage of components.Wing falls tumble injury when being model plane flight or collsion damage is easiest to damage
Part, while it is also a very crucial component, is that model plane generate lift in flight and keep the not all right horizontal side of model plane
Stable mechanism realizes the Quick Release of itself and fuselage and is stably connected with very crucial.
Utility model content
The utility model provides a kind of model plane wing Quick Release connection structure, it is intended to overcome model plane fuselage and machine in the prior art
The deficiency that connection between the wing can not easily realize Quick Release and be stably connected with.
The technical solution that the utility model solves above-mentioned technical problem is as follows: a kind of model plane wing Quick Release connection structure,
Including the identical fuselage connector of shapes and sizes and wing connection, the fuselage connector and wing connection are relative to each other
Side can be overlapped and be adjacent to combination and faying face and be equipped with clip assembly, positioning component, jack assemblies and Quick Release slot, the fuselage
Connector and wing connection side away from one another are recessed respectively for wrapping up fuselage connecting side face and wing connecting side
The groove in face, the clip assembly include be respectively arranged on the fuselage connector and wing connection two relative side and that
This corresponding buckle and card slot, the positioning component include being respectively arranged at the fuselage connector and wing connection two relatively
On side and the locating piece and locating slot that correspond to each other, the jack assemblies include being set on fuselage connector side
Female plug and the male plug being set in the wing connection respective side, the Quick Release slot are arranged along the vertical direction.
Compared with prior art, the utility model has the beneficial effects that fuselage connector and wing connection pass through clamping
Component and positioning component quickly can be positioned and are clamped, and assembling fixation is very convenient when being adjacent to combination, while further including Quick Release slot, will
Bottle opener or flat rigid posts are inserted into the Quick Release slot, can very easily connect the fuselage connector for being adjacent to engagement with wing
Part is dismantled；Jack assemblies can easily realize being electrically connected for electric appliance between fuselage and wing, not need to connect wires in outside, and insert
Holder assembly also has certain support connection function in vertical direction other than as electrical connection bridge.
Based on the above technical solution, the utility model can also do following improvement.
Further, the clip assembly, positioning component and Quick Release slot are respectively arranged with multiple.
Beneficial effect using above-mentioned further scheme be make to position, be clamped and split equal enhanced convenience it is efficient.
Further, it is described buckle be cylinder, the barrel of the cylinder circumferentially uniform intervals be equipped with it is multiple run through slot,
The axial direction through slot along the barrel stretches.
Beneficial effect using above-mentioned further scheme is that cylinder is made to be divided into multiple arc plates, makes it by radial pressure
To shrinkable at axle center when power, to more easily be caught in card slot.
Further, the cylinder encloses arc clasp convex block, the button towards setting one on one end outer wall of the card slot
Hold convex block the cylinder radially with a thickness of 0.3-0.8mm.
Beneficial effect using above-mentioned further scheme is that clasp convex block may be stuck in one end of card slot, not easily to fall off, even
It connects more firm.
Further, the Quick Release slot includes being respectively arranged on the fuselage connector and wing connection two relative side
And the through slot that the first groove body and the second groove body to correspond to each other, first groove body and the second groove body are open for upper and lower ends.
Beneficial effect using above-mentioned further scheme is that first and second groove body is the groove body that upper and lower ends are open,
It is also then both ends open (being similar to through-hole) close to the rear Quick Release slot formed by the two, then can protrudes into bottle opener or hard from both ends
Bar, it is more convenient when fractionation.
Further, several reinforcing ribs are equipped in the groove of the fuselage connector and wing connection.
Beneficial effect using above-mentioned further scheme is that setting reinforcing rib makes fuselage connector and wing connection more
Add durable, when collision is hardly damaged.
It further, further include several spliced eyes passed through for the inserting column being fixedly installed on the fuselage or the wing,
The spliced eye includes respectively along through the fuselage connector and wing connection and corresponding to each other perpendicular to side surface direction
First through hole and the second through-hole.
Beneficial effect using above-mentioned further scheme is the setting of spliced eye, is facilitated holding between fuselage and wing
Reconnection fitting (inserting column) passes through, to make to connect between fuselage and wing more firm.
Detailed description of the invention
Fig. 1 is that a kind of model plane wing Quick Release connection structure provided by the utility model is overlapped the structural schematic diagram before being adjacent to；
Fig. 2 is that a kind of model plane wing Quick Release connection structure provided by the utility model is overlapped the structural representation being adjacent to after combining
Figure；
Fig. 3 is knot when a kind of model plane wing Quick Release connection structure provided by the utility model is used to connect fuselage and wing
Structure schematic diagram;
Fig. 4 is the amplified schematic diagram of buckle that virtual coil is lived in Fig. 1.
In attached drawing, parts list represented by the reference numerals are as follows:
1. fuselage connector；2. wing connection；3. buckle；4. card slot；5. groove；6. spliced eye；7. male plug；8. female
It inserts；9. locating piece；10. locating slot；11. Quick Release slot；12. fuselage；13. wing；
30. running through slot；31. clasp convex block.
Specific embodiment
The principles of the present invention and feature are described below in conjunction with attached drawing, example is served only for explaining that this is practical
It is novel, it is not intended to limit the scope of the utility model.
As shown in Figures 1 to 4, the utility model provides a kind of model plane wing Quick Release connection structure comprising shapes and sizes
Identical fuselage connector 1 and wing connection 2, the fuselage connector 1 and the side relative to each other of wing connection 2 can weigh
Conjunction is adjacent to combination and faying face is equipped with clip assembly, positioning component, jack assemblies and Quick Release slot 11, the fuselage connector 1
Side away from one another is recessed respectively with wing connection 2 connects side and the connection of wing 13 side for wrapping up fuselage 12
Groove 5, the clip assembly include be respectively arranged on 2 two relative side of the fuselage connector 1 and wing connection and
The buckle 3 and card slot 4 to correspond to each other, the positioning component include being respectively arranged at the fuselage connector 1 and wing connection 2
On two relative side and the locating piece 9 and locating slot 10 that correspond to each other, the jack assemblies include being set to the fuselage connection
Female plug 8 on 1 side of part and the male plug 7 being set in 2 respective side of wing connection, the Quick Release slot 11 is along vertical side
To setting.
Further, the clip assembly, positioning component and Quick Release slot 11 are respectively arranged with multiple.
In one embodiment of the utility model, as shown in Figure 1, clip assembly, positioning component and Quick Release slot are set respectively
There are two, and a front end in fuselage, wing connection opposite flank, another is in the rear end of fuselage, wing connection.Separately
Outside, the quantity of jack assemblies is one, is located at the middle part of fuselage, wing connection, electronic component, power supply in female plug and fuselage
Deng electrical connection, male plug is electrically connected with the electronic component on wing.
Further, it is described buckle 3 be cylinder, the barrel of the cylinder circumferentially uniform intervals be equipped with it is multiple run through slot
30, the axial direction through slot 30 along the barrel stretches.
Further, the cylinder is described towards one circle arc clasp convex block 31 of setting on one end outer wall of the card slot 4
Clasp convex block 31 the cylinder radially with a thickness of 0.3-0.8mm.
Further it will be understood that can also be the buckle of other shapes, such as just more in addition to the buckle of cylinder shape
Prism (cylinder) shape etc..
Further, the Quick Release slot 11 includes being respectively arranged at 2 two opposite sides of the fuselage connector 1 and wing connection
On face and the first groove body and the second groove body that correspond to each other, it is logical that first groove body and the second groove body are that upper and lower ends are open
Slot.
It is understood that Quick Release slot may be unilateral slot, i.e., one is selected on fuselage connector or wing connection
Quick Release slot is set.
Further, several reinforcing ribs are equipped in the groove 5 of the fuselage connector 1 and wing connection 2.
It further, further include several grafting passed through for the inserting column being fixedly installed on the fuselage 12 or the wing 13
Hole 6, the spliced eye 6 include respectively along perpendicular to side surface direction through the fuselage connector 1 and wing connection 2 and each other
Corresponding first through hole and the second through-hole.
Model plane wing Quick Release connection structure structure provided by the utility model is simple, connect and dismantle it is very convenient, specifically
It is as follows: when connection, by fuselage connector be first installed on fuselage connection side (groove wrap fuselage connection side, can be clamped or
Fixed bonding), at the same also by wing connection be installed on wing connection side (groove wrap wing connection side, can be clamped
Or fixed bonding), then fuselage connector is close to each other with wing connection and is overlapped and is adjacent to, positioning component use when coincidence is adjacent to
In positioning, clip assembly fixes fuselage connector with wing connection for clamping, and male plug is inserted into female plug, realizes fuselage and machine
The electrical connection of electronic component between the wing, while the inserting column vertically fixed on fuselage connection side passes through the first, second through-hole
It protrudes into wing in preset slot；When fractionation, Quick Release slot is protruded into one end of bottle opener, slightly swings power to two sides, is then clamped
Component unclamps, and fuselage connector and wing connection are quickly dismantled.
The above is only the preferred embodiment of the present invention, is not intended to limit the utility model, all practical at this
Within novel spirit and principle, any modification, equivalent replacement, improvement and so on should be included in the guarantor of the utility model
Within the scope of shield.
Claims (7)
1. a kind of model plane wing Quick Release connection structure, which is characterized in that including the identical fuselage connector (1) of shapes and sizes and
Wing connection (2), the fuselage connector (1) and wing connection (2) side relative to each other can be overlapped be adjacent to combination and
Faying face is equipped with clip assembly, positioning component, jack assemblies and Quick Release slot (11), and the fuselage connector (1) and wing connect
Fitting (2) side away from one another is recessed respectively connects side for wrapping up fuselage (12) connection side and wing (13)
Groove (5), the clip assembly include being respectively arranged at the fuselage connector (1) and wing connection (2) two relative side
Buckle (3) and card slot (4) upper and correspond to each other, the positioning component including be respectively arranged at the fuselage connector (1) and
On wing connection (2) two relative side and the locating piece (9) and locating slot (10) that correspond to each other, the jack assemblies include setting
The female plug (8) being placed on fuselage connector (1) side and the male plug being set in the wing connection (2) respective side
(7), the Quick Release slot (11) is arranged along the vertical direction.
2. a kind of model plane wing Quick Release connection structure according to claim 1, which is characterized in that the clip assembly is determined
Hyte part and Quick Release slot (11) are respectively arranged with multiple.
3. a kind of model plane wing Quick Release connection structure according to claim 1, which is characterized in that the buckle (3) is circle
Cylinder, circumferentially uniform intervals are equipped with multiple through slot (30) for the barrel of the cylinder, and run through slot (30) are along the cylinder
The axial direction of wall stretches.
4. a kind of model plane wing Quick Release connection structure according to claim 3, which is characterized in that the cylinder is towards institute
One circle arc clasp convex block (31) of setting on one end outer wall of card slot (4) is stated, the clasp convex block (31) is in the cylinder diameter
It is upward with a thickness of 0.3-0.8mm.
5. a kind of model plane wing Quick Release connection structure according to any one of claims 1 to 4, which is characterized in that described fast
Tearing slot (11) open includes being respectively arranged on the fuselage connector (1) and wing connection (2) two relative side and corresponding to each other
The first groove body and the second groove body, first groove body and the second groove body are the through slot that upper and lower ends are open.
6. a kind of model plane wing Quick Release connection structure according to any one of claims 1 to 4, which is characterized in that the machine
Several reinforcing ribs are equipped in the groove (5) of body connector (1) and wing connection (2).
7. a kind of model plane wing Quick Release connection structure according to any one of claims 1 to 4, which is characterized in that further include
Several spliced eyes (6) passed through for the inserting column being fixedly installed on the fuselage (12) or the wing (13), the spliced eye
(6) include respectively along perpendicular to side surface direction through the fuselage connector (1) and wing connection (2) and correspond to each other the
One through-hole and the second through-hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821131171.8U CN208641751U (en) | 2018-07-17 | 2018-07-17 | A kind of model plane wing Quick Release connection structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821131171.8U CN208641751U (en) | 2018-07-17 | 2018-07-17 | A kind of model plane wing Quick Release connection structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208641751U true CN208641751U (en) | 2019-03-26 |
Family
ID=65785358
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821131171.8U Expired - Fee Related CN208641751U (en) | 2018-07-17 | 2018-07-17 | A kind of model plane wing Quick Release connection structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208641751U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109927878A (en) * | 2019-04-25 | 2019-06-25 | 西安航空学院 | Diamond wing mounting structure and aircraft with the mounting structure |
| CN110745232A (en) * | 2019-11-18 | 2020-02-04 | 西安爱生技术集团公司 | Modularization unmanned aerial vehicle fuselage butt-joint structural |
-
2018
- 2018-07-17 CN CN201821131171.8U patent/CN208641751U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109927878A (en) * | 2019-04-25 | 2019-06-25 | 西安航空学院 | Diamond wing mounting structure and aircraft with the mounting structure |
| CN109927878B (en) * | 2019-04-25 | 2024-02-02 | 西安航空学院 | Diamond wing mounting structure and aircraft with same |
| CN110745232A (en) * | 2019-11-18 | 2020-02-04 | 西安爱生技术集团公司 | Modularization unmanned aerial vehicle fuselage butt-joint structural |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208641751U (en) | A kind of model plane wing Quick Release connection structure | |
| CN109436288A (en) | Rack and aircraft for aircraft | |
| CN105691605A (en) | Unmanned aerial vehicle with detachable vehicle arms | |
| CN105098474B (en) | Electric connector combination | |
| CN209441609U (en) | Rack and aircraft for aircraft | |
| CN205203369U (en) | Airborne elevator connection structure and have its aircraft | |
| US20180080603A1 (en) | Hook device and hook assembly including the hook device | |
| CN208618936U (en) | A kind of easily dress handle | |
| CN107579193A (en) | Connect up clamp structure, battery component and electric car | |
| CN210310912U (en) | Support frame assembly structure | |
| CN209441608U (en) | Horn clamping device and aircraft for aircraft | |
| CN209567071U (en) | Horn clamping device and aircraft for aircraft | |
| CN205891214U (en) | Wing grafting structure | |
| CN207381465U (en) | Connect up clamp structure, battery component and electric car | |
| CN105691599A (en) | Undercarriage disassembly and assembly structure of aircraft | |
| CN206592808U (en) | A kind of LED safety lamp holders | |
| CN105667769A (en) | Undercarriage for unmanned aerial vehicle | |
| CN209667353U (en) | Unmanned plane | |
| CN211253027U (en) | Unmanned plane | |
| CN109436289A (en) | Horn clamping device and aircraft for aircraft | |
| CN210592406U (en) | Connecting mechanism and wing connected with tail boom | |
| CN206125920U (en) | Unmanned aerial vehicle rotor quick assembly disassembly structure | |
| CN210251205U (en) | Portable paper plane capable of being quickly disassembled and assembled | |
| CN208487449U (en) | Conveniently-connected point light source | |
| CN111180963B (en) | Charging port support, charging seat and smoke rescue illumination indicating device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20190326 |