CN205010467U - Wing and fuselage connecting device - Google Patents
Wing and fuselage connecting device Download PDFInfo
- Publication number
- CN205010467U CN205010467U CN201520650668.0U CN201520650668U CN205010467U CN 205010467 U CN205010467 U CN 205010467U CN 201520650668 U CN201520650668 U CN 201520650668U CN 205010467 U CN205010467 U CN 205010467U
- Authority
- CN
- China
- Prior art keywords
- wing
- fuselage
- side plate
- transverse slat
- connecting panel
- 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
Abstract
The utility model discloses a wing and fuselage connecting device, include: diaphragm, its characterized in that are connected with the fuselage to wing connecting plate, connecting hole, first curb plate, first fixed orifices, wing screens cutting, wing connection diaphragm, second curb plate, positional punch, second fixed orifices, nut, screw, third curb plate, fuselage connecting plate, fuselage screens cutting, fourth curb plate: be provided with the connecting hole on the wing connecting plate, wing connecting plate bottom is provided with the wing and connects the diaphragm, and the wing is connected and is provided with the wing screens on the diaphragm and transplants a cutting, and the mutual fixed connection of diaphragm is connected to wing screens cutting and wing, and wing connecting plate one side is provided with first curb plate, first curb plate and the mutual fixed connection of diaphragm is connected to the wing, is provided with first fixed orifices on the first curb plate, and wing connecting plate opposite side is provided with the second curb plate. The utility model has the advantages of flexibility height, simple structure, reduce cost.
Description
Technical field
The utility model relates to aircraft components field, particularly relates to a kind of wing and fuselage connection.
Background technology
At present, the large parts of existing aircraft, as between fuselage, wing, are interconnected joint and mostly are bolt and are connected with auricle joint.This traditional link form structure is complicated, and weight is large, and when assembling or dismounting, work capacity is large, is inconvenient to use.Especially for the wing of monocoque, covering is main bearing member, and jointing should be multiple spot distributing joint.Periphery is divided into connect dispersion power transmission and concentrated power transmission, because its performance different separately may be used for the aircraft of different purposes according to its power transmission form.Wherein, the bolt quantity that periphery connects dispersion power transmission is more, and advantage is the power transmission efficiency giving full play to wing root covering, does not need special complicated jointing, is conducive to alleviating structure design weight; Shortcoming is the increase in be linked and packed between wing and fuselage with heavy work load, must add the tolerance on fit in king bolt and hole, make Transfer of Shear and strength at repeated alternation bring adverse effect.Concentrate power transmission exactly wing and the several point of fuselage to be coupled together, can transmit larger force and moment, the man-hour that is linked and packed of wing and fuselage reduces.Existing wing and fuselage connection are generally wing and fuselage jointing are made of one, and such beam is the transom of wing and wing body is also the plug-in and inner load resting point loaded of wing; Its shortcoming mainly wing can not be separated with fuselage connector, and alerting ability is poor and waste of material is many.
Utility model content
Technical problem to be solved in the utility model is for above-mentioned the deficiencies in the prior art, provides a kind of wing and fuselage connection, and the utility model has the advantage that alerting ability is high, structure simple, reduce costs.
The technical solution of the utility model is: a kind of wing and fuselage connection, comprise: wing connecting panel, connecting bore, first side plate, first fixed orifice, wing screens cutting, wing connects transverse slat, second side plate, positional punch, second fixed orifice, nut, screw, 3rd side plate, fuselage connecting panel, fuselage screens cutting, 4th side plate is connected transverse slat with fuselage, it is characterized in that: described wing connecting panel is provided with connecting bore, be provided with wing bottom described wing connecting panel and connect transverse slat, described wing connection transverse slat is provided with wing screens cutting, described wing screens cutting is connected transverse slat with described wing and is mutually permanently connected, described wing connecting panel side is provided with the first side plate, described first side plate is connected transverse slat with described wing and is mutually permanently connected, described first side plate is provided with the first fixed orifice, described wing connecting panel opposite side is provided with the second side plate, described second side plate is connected transverse slat with described wing and is mutually permanently connected, described second side plate is provided with the second fixed orifice, described second fixed orifice side is provided with positional punch, described wing connecting panel one end is provided with fuselage connecting panel, be provided with fuselage bottom described fuselage connecting panel and connect transverse slat, described fuselage connecting panel side is provided with the 3rd side plate, described 3rd side plate is connected transverse slat with described fuselage and is mutually permanently connected, described fuselage connecting panel opposite side is provided with the 4th side plate, described 4th side plate is connected transverse slat with described fuselage and is mutually permanently connected, described 3rd side plate and the 4th side plate are provided with screw, described screw is provided with nut, described screw and nut are mutually permanently connected, described fuselage connection transverse slat is provided with fuselage screens cutting, described fuselage screens cutting is connected transverse slat with described fuselage and is mutually permanently connected.
Further, described wing screens cutting is provided with two.
Further, described fuselage screens cutting is provided with two.
Further, described screw is provided with nine.
The beneficial effects of the utility model are:
1. the utility model is by being arranged on the wing screens cutting on wing connecting panel, can be interconnected with wing, can be mutually permanently connected with aircraft wing by the first fixed orifice, the second fixed orifice and the positional punch that arrange on the first side plate and the second side plate, there is the advantage that alerting ability is high, structure simple, reduce costs.
2. the screw number of the utility model periphery connection dispersion power transmission is more, and advantage is the power transmission efficiency having fully played wing root covering.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Wherein: 1, wing connecting panel 2, connecting bore 3, first side plate
4, the first fixed orifice 5, wing screens cutting 6, wing connect transverse slat
7, the second side plate 8, positional punch 9, second fixed orifice
10, nut 11, screw 12, the 3rd side plate
13, fuselage connects transverse slat 14, fuselage screens cutting the 15, the 4th side plate
16, fuselage connecting panel
Detailed description of the invention
Below in conjunction with accompanying drawing, brief description is made to detailed description of the invention of the present utility model.
As shown in Figure 1, a kind of wing and fuselage connection, comprise: wing connecting panel 1, connecting bore 2, first side plate 3, first fixed orifice 4, wing screens cutting 5, wing connects transverse slat 6, second side plate 7, positional punch 8, second fixed orifice 9, nut 10, screw 11, 3rd side plate 12, fuselage connecting panel 13, fuselage screens cutting 14, 4th side plate 15 is connected transverse slat 16 with fuselage, it is characterized in that: described wing connecting panel 1 is provided with connecting bore 2, be provided with wing bottom described wing connecting panel 1 and connect transverse slat 6, described wing connection transverse slat 6 is provided with wing screens cutting 5, described wing screens cutting 5 is connected transverse slat 6 with described wing and is mutually permanently connected, described wing connecting panel 1 side is provided with the first side plate 3, described first side plate 3 is connected transverse slat 6 with described wing and is mutually permanently connected, described first side plate 3 is provided with the first fixed orifice 4, described wing connecting panel 1 opposite side is provided with the second side plate 7, described second side plate 7 is connected transverse slat 6 with described wing and is mutually permanently connected, described second side plate 7 is provided with the second fixed orifice 9, described second fixed orifice 9 side is provided with positional punch 8, described wing connecting panel 1 one end is provided with fuselage connecting panel 16, be provided with fuselage bottom described fuselage connecting panel 16 and connect transverse slat 13, described fuselage connecting panel 16 side is provided with the 3rd side plate 12, described 3rd side plate 12 is connected transverse slat 13 with described fuselage and is mutually permanently connected, described fuselage connecting panel 16 opposite side is provided with the 4th side plate 15, described 4th side plate 15 is connected transverse slat 13 with described fuselage and is mutually permanently connected, described 3rd side plate 12 and the 4th side plate 15 are provided with screw 11, described screw 11 is provided with nut 10, described screw 11 is mutually permanently connected with nut 10, described fuselage connection transverse slat 13 is provided with fuselage screens cutting 14, described fuselage screens cutting 14 is connected transverse slat 13 with described fuselage and is mutually permanently connected.
Mode of operation: the utility model is by being arranged on the wing screens cutting on wing connecting panel, can be interconnected with wing, can be mutually permanently connected with aircraft wing by the first fixed orifice, the second fixed orifice and the positional punch arranged on the first side plate and the second side plate.By being arranged on the fuselage screens cutting on fuselage connecting panel, can be interconnected with fuselage, by being arranged on the screw on the 3rd side plate and the 4th side plate, can be mutually permanently connected with fuselage, wing connecting panel is provided with connecting bore, and connecting bore can insert screw and fuselage connecting panel is interconnected.The utility model has the advantage that alerting ability is high, structure simple, reduce costs.
Above embodiment, only in order to the technical solution of the utility model to be described, can not limit scope of the present utility model with this; To the amendment that the technical scheme described in foregoing embodiments is carried out, or to the equivalent replacement that wherein portion of techniques feature is carried out, do not make the essence of appropriate technical solution depart from the spirit and scope of each embodiment technical scheme of the utility model, all should still belong in scope that the utility model patent contains.
Claims (4)
1. a wing and fuselage connection, comprise: wing connecting panel, connecting bore, first side plate, first fixed orifice, wing screens cutting, wing connects transverse slat, second side plate, positional punch, second fixed orifice, nut, screw, 3rd side plate, fuselage connecting panel, fuselage screens cutting, 4th side plate is connected transverse slat with fuselage, it is characterized in that: described wing connecting panel is provided with connecting bore, be provided with wing bottom described wing connecting panel and connect transverse slat, described wing connection transverse slat is provided with wing screens cutting, described wing screens cutting is connected transverse slat with described wing and is mutually permanently connected, described wing connecting panel side is provided with the first side plate, described first side plate is connected transverse slat with described wing and is mutually permanently connected, described first side plate is provided with the first fixed orifice, described wing connecting panel opposite side is provided with the second side plate, described second side plate is connected transverse slat with described wing and is mutually permanently connected, described second side plate is provided with the second fixed orifice, described second fixed orifice side is provided with positional punch, described wing connecting panel one end is provided with fuselage connecting panel, be provided with fuselage bottom described fuselage connecting panel and connect transverse slat, described fuselage connecting panel side is provided with the 3rd side plate, described 3rd side plate is connected transverse slat with described fuselage and is mutually permanently connected, described fuselage connecting panel opposite side is provided with the 4th side plate, described 4th side plate is connected transverse slat with described fuselage and is mutually permanently connected, described 3rd side plate and the 4th side plate are provided with screw, described screw is provided with nut, described screw and nut are mutually permanently connected, described fuselage connection transverse slat is provided with fuselage screens cutting, described fuselage screens cutting is connected transverse slat with described fuselage and is mutually permanently connected.
2. according to a kind of wing described in claim 1 and fuselage connection, it is characterized in that: described wing screens cutting is provided with two.
3. according to a kind of wing described in claim 1 and fuselage connection, it is characterized in that: described fuselage screens cutting is provided with two.
4. according to a kind of wing described in claim 1 and fuselage connection, it is characterized in that: described screw is provided with nine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520650668.0U CN205010467U (en) | 2015-08-26 | 2015-08-26 | Wing and fuselage connecting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520650668.0U CN205010467U (en) | 2015-08-26 | 2015-08-26 | Wing and fuselage connecting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205010467U true CN205010467U (en) | 2016-02-03 |
Family
ID=55209081
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520650668.0U Expired - Fee Related CN205010467U (en) | 2015-08-26 | 2015-08-26 | Wing and fuselage connecting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205010467U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112572759A (en) * | 2020-12-29 | 2021-03-30 | 北京北航天宇长鹰无人机科技有限公司 | Wing body combines to connect and unmanned aerial vehicle |
-
2015
- 2015-08-26 CN CN201520650668.0U patent/CN205010467U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112572759A (en) * | 2020-12-29 | 2021-03-30 | 北京北航天宇长鹰无人机科技有限公司 | Wing body combines to connect and unmanned aerial vehicle |
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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: 20160203 Termination date: 20210826 |