CN207194245U - Encorbelment glass all-wing aircraft corner structure - Google Patents
Encorbelment glass all-wing aircraft corner structure Download PDFInfo
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- CN207194245U CN207194245U CN201720771906.2U CN201720771906U CN207194245U CN 207194245 U CN207194245 U CN 207194245U CN 201720771906 U CN201720771906 U CN 201720771906U CN 207194245 U CN207194245 U CN 207194245U
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- glass
- wing aircraft
- fin
- glass panel
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Abstract
To be encorbelmented glass all-wing aircraft corner structure the utility model discloses one kind, it includes two all-wing aircraft plates for being mutually angle, wherein：All-wing aircraft plate includes some glass panels, and the glass fin perpendicular to glass panel is provided with the vertical lattice of adjacent glass panel；Two all-wing aircraft plates are mutually between angle forms the two neighboring glass panel of corner to be connected by docking component；Be fixed at the top of glass panel and glass fin in agent structure and bottom is hanging, or the bottom of glass panel and glass fin is fixed in agent structure and top is hanging.The utility model improves the permeability of angle position, and appearance is good, install convenient, is easy to later stage cleaning and safeguards, suitable for promoting.
Description
Technical field
A kind of corner structure for glass all-wing aircraft of encorbelmenting is the utility model is related to, belongs to glass curtain wall field.
Background technology
The current existing way for encorbelmenting glass curtain wall corner mainly has two ways：One kind is to set one in angle position
Glass fin, but used by this way for the glass fin space limited to angle position, installation is inconvenient, curtain wall
Top braces difficult design, while can give later stage cleaning tape come greatly inconvenience.Another kind be angle position set a steel or
The side of aluminium material is logical as supporting construction, but this way has the problem of above-mentioned first way is same, and influences outward appearance
Visual effect.
Utility model content
The purpose of this utility model is to provide one kind and encorbelmented glass all-wing aircraft corner structure, which improves the logical of angle position
Permeability, appearance is good, install convenient, is easy to later stage cleaning and safeguards, suitable for promoting.
To achieve these goals, the utility model employs following technical scheme：
One kind is encorbelmented glass all-wing aircraft corner structure, it is characterised in that：It includes two all-wing aircraft plates for being mutually angle, its
In：All-wing aircraft plate includes some glass panels, and the glass perpendicular to glass panel is provided with the vertical lattice of adjacent glass panel
Glass floor；Two all-wing aircraft plates are mutually between angle forms the two neighboring glass panel of corner to be connected by docking component；Glass
It is fixed at the top of glass panel and glass fin in agent structure and bottom is hanging, or the bottom of glass panel and glass fin
It is fixed in agent structure and top is hanging.
The docking component connects the top of the two neighboring glass panel, one end of the docking component and adjacent two
A glass panel in the individual glass panel is be hinged and the other end with it is another in the two neighboring glass panel
The individual glass panel concrete mutually, wherein：The docking component includes Connecting claw, overlapping joint.
Be fixed at the top of the glass panel and the glass fin in the agent structure and bottom it is hanging when：
The bottom of the glass fin is connected by the first bearing pin with the first adaptor, and mountain font section bar passes through screw and
One adaptor connects, and is provided with auxiliary frame at the vertical lattice between the adjacent glass panel, auxiliary frame passes through installed in mountain font
Cap bolt component on section bar is articulated on the font section bar of mountain；
The top of the glass fin is connected by bolt assembly with the second adaptor, and the adjacent glass panel is by refuting
Joint is fixed on the second adaptor；
The top of the glass fin is connected by the second bearing pin with the 3rd adaptor, and the 3rd adaptor stretches out the glass
The part of floor is connected by the 4th adaptor, the 5th adaptor with the agent structure.
The utility model has the advantages that：
The utility model optimizes the way of existing corner, and glass fin, the just support such as logical are not provided with angle position
Structure, corner structure being enormously simplify, the rigidity of structure can meet engine request with intensity, improve the permeability of angle position,
Appearance is good, install convenient, and curtain wall top supported design difficulty reduces, while is easy to later stage cleaning and safeguards.
Brief description of the drawings
Fig. 1 is that the utility model is encorbelmented the cross-sectional node schematic diagram of glass all-wing aircraft corner structure bottom.
Fig. 2 is that the utility model is encorbelmented the cross-sectional node schematic diagram on glass all-wing aircraft corner structure top.
Fig. 3 is that the utility model is encorbelmented the schematic diagram being connected with agent structure at the top of glass all-wing aircraft corner structure.
Embodiment
Such as Fig. 1 to Fig. 3, the utility model glass all-wing aircraft corner structure of encorbelmenting includes two all-wing aircraft plates for being mutually angle α,
Wherein：All-wing aircraft plate includes some glass panels 10, is provided with the vertical lattice of adjacent glass panel 10 perpendicular to glass surface
The glass fin 30 of plate 10；Two all-wing aircraft plates, which are mutually between angle forms the two neighboring glass panel 10 of corner, passes through docking
Component is connected；The top of glass panel 10 and glass fin 30 is fixed in agent structure 70 and bottom is hanging, or glass surface
The bottom of plate 10 and glass fin 30 is fixed in agent structure and top is hanging.
In actual design, it is preferred that the top of the two neighboring glass panel 10 of docking component connection, the one of docking component
End and a glass panel 10 in two neighboring glass panel 10 are be hinged, bear shearing, pulling force, and the other end of docking component
Another concrete mutually of glass panel 10 with two neighboring glass panel 10, bears moment of flexure, shearing, pulling force, wherein：Docking structure
Part includes Connecting claw 21, overlapping joint 22, installs overlapping joint 22 in Connecting claw 21, overlapping joint 22 is fixed with the phase of glass panel 10.For
Solves the uniformity that power is transmitted between Connecting claw 21 and glass panel 10, in gap between overlapping joint 22 and glass panel 10
Epoxide-resin glue can be clogged.
In actual design, it is preferred that adjacent two glass panels 10 of angle position are SGP doubling glass panels, and
The glass panel 10 of other positions can be PVB doubling glass panel or SGP doubling glass panels, come depending on actual installation position true
Fixed, even if can so ensure that glass panel damages, it will not also fall.
When the top of glass panel 10 and glass fin 30 is fixed in agent structure 70 and bottom is hanging, such as Fig. 1 extremely
Shown in Fig. 3：
Such as Fig. 1, the bottom of glass fin 30 is connected by the first bearing pin 46 with the first adaptor 41, and mountain font section bar 44 is logical
Cross screw 43 to be connected with the first adaptor 41, auxiliary frame 42, auxiliary frame 42 are installed at the vertical lattice between adjacent glass panel 10
It is articulated in by the cap bolt component 45 on mountain font section bar 44 on mountain font section bar 44；
Such as Fig. 2, the top of glass fin 30 is connected by bolt assembly 53 with the second adaptor 51, adjacent glass panel 10
It is fixed to by overlapping joint 52 on the second adaptor 51；
Such as Fig. 3, the top of glass fin 30 is connected by the second bearing pin 54 with the 3rd adaptor 62, and the 3rd adaptor 62 is stretched
The part for going out glass fin 30 is connected by the 4th adaptor 61, the 5th adaptor 63 with agent structure 70.
Such as Fig. 2, further, it is arranged on after the second 54 sets of bearing pin upper bush 55 on glass fin 30, and sleeve 55 and glass
Epoxide-resin glue 56 is packed with gap between glass floor 30.
Such as Fig. 2, in actual design, it is preferred that the second adaptor 51 is connected with the 3rd adaptor 62.And actually setting
In meter, the hole on the second adaptor 51 for installation bolt component 53 is horizontal slotted hole (such as Fig. 3), to adjust the second switching
Part 51 enters the wind load for deviating and discharging perpendicular to glass panel 10.
When the bottom of glass panel 10 and glass fin 30 is fixed in agent structure and top is hanging, Fig. 1 can refer to
Understand to the structure shown in Fig. 3, will not be repeated here.
In the utility model, it is preferred that glass fin 30 is the SGP doubling glass ribs that divided glass rib overlaps
Plate.
In the utility model, the support knot such as glass fin is not provided between two glass panels 10 of angle position
Structure, but an entirety is directly connected as by docking component, docking component is used for the deadweight for bearing the two glass panels 10
Load, wind load is not subject to, two glass panels 10 of angle position support each other, bear the wind load outside glass panel 10.
Wind load is delivered on glass fin 30 by auxiliary frame 42 suffered by glass panel 10, then by the 3rd adaptor 62, the 4th turn
Fitting 61, the 5th adaptor 63 are delivered on the embedded part of agent structure 70, and the deadweight of same glass fin 30 passes through the second bearing pin
54th, the 3rd adaptor 62, the 4th adaptor 61 are delivered on the embedded part of agent structure 70, and lateral wind load is by the 4th adaptor
61st, the 5th adaptor 63 is born.To the load parallel to glass panel 10, adjacent other non-corners are delivered to by docking component
On the glass panel 10 and glass fin 30 of position, to solve the problems, such as stress.
The utility model has the advantages that：
The utility model optimizes the way of existing corner, and glass fin, the just support such as logical are not provided with angle position
Structure, corner structure being enormously simplify, the rigidity of structure can meet engine request with intensity, improve the permeability of angle position,
Appearance is good, install convenient, and curtain wall top supported design difficulty reduces, while is easy to later stage cleaning and safeguards.
The technical principle described above for being the utility model preferred embodiment and its being used, for those skilled in the art
It is any based on technical solutions of the utility model basis in the case of without departing substantially from spirit and scope of the present utility model for member
On equivalent transformation, it is simple replace etc. it is obvious change, belong within scope of protection of the utility model.
Claims (7)
- The glass all-wing aircraft corner structure 1. one kind is encorbelmented, it is characterised in that：It includes two all-wing aircraft plates for being mutually angle, wherein： All-wing aircraft plate includes some glass panels, and the Glass Rib perpendicular to glass panel is provided with the vertical lattice of adjacent glass panel Plate；Two all-wing aircraft plates are mutually between angle forms the two neighboring glass panel of corner to be connected by docking component；Glass surface It is fixed at the top of plate and glass fin in agent structure and bottom is hanging, or the bottom of glass panel and glass fin is fixed In in agent structure and top is hanging.
- 2. glass all-wing aircraft corner structure as claimed in claim 1 of encorbelmenting, it is characterised in that：The docking component connects the top of the two neighboring glass panel, one end of the docking component and two neighboring institute The glass panel stated in glass panel is hinged and the other end and another institute in the two neighboring glass panel State glass panel concrete mutually.
- 3. glass all-wing aircraft corner structure as claimed in claim 2 of encorbelmenting, it is characterised in that：The adjacent described two glass panels of angle position are SGP doubling glass panels, and the glass panel of other positions is PVB doubling glass panel or SGP doubling glass panels.
- 4. glass all-wing aircraft corner structure as claimed in claim 1 of encorbelmenting, it is characterised in that：Be fixed at the top of the glass panel and the glass fin in the agent structure and bottom it is hanging when：The bottom of the glass fin is connected by the first bearing pin with the first adaptor, and mountain font section bar passes through screw and first turn Fitting connects, and is provided with auxiliary frame at the vertical lattice between the adjacent glass panel, auxiliary frame passes through installed in mountain font section bar On cap bolt component be articulated on the font section bar of mountain；The top of the glass fin is connected by bolt assembly with the second adaptor, and the adjacent glass panel passes through overlapping joint Fixed on the second adaptor；The top of the glass fin is connected by the second bearing pin with the 3rd adaptor, and the 3rd adaptor stretches out the glass fin Part be connected by the 4th adaptor, the 5th adaptor with the agent structure.
- 5. glass all-wing aircraft corner structure as claimed in claim 4 of encorbelmenting, it is characterised in that：It is arranged on after the second pin sleeve upper bush on the glass fin, and the gap between sleeve and the glass fin In be packed with epoxide-resin glue.
- 6. glass all-wing aircraft corner structure as claimed in claim 4 of encorbelmenting, it is characterised in that：Second adaptor is connected with the 3rd adaptor.
- 7. the glass all-wing aircraft corner structure of encorbelmenting as any one of claim 1 to 6, it is characterised in that：The glass fin is the SGP doubling glass floors that divided glass rib overlaps.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720771906.2U CN207194245U (en) | 2017-06-29 | 2017-06-29 | Encorbelment glass all-wing aircraft corner structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720771906.2U CN207194245U (en) | 2017-06-29 | 2017-06-29 | Encorbelment glass all-wing aircraft corner structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207194245U true CN207194245U (en) | 2018-04-06 |
Family
ID=61785224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720771906.2U Active CN207194245U (en) | 2017-06-29 | 2017-06-29 | Encorbelment glass all-wing aircraft corner structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207194245U (en) |
-
2017
- 2017-06-29 CN CN201720771906.2U patent/CN207194245U/en active Active
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