Flying wing structure and flying wing mounting structure

Abstract

The utility model discloses a flying wing structure and a flying wing installation structure, the flying wing structure comprises a front plate assembly and a back plate assembly which are connected with each other, the front plate assembly and the back plate assembly are combined to form a cavity, the cavity is filled with honeycomb core materials, and a plurality of bolts are fixedly arranged on the back plate assembly. The front plate assembly and the back plate assembly are adopted to form the appearance of the flying wing, the cavity formed in the flying wing is filled with the honeycomb core material, and the honeycomb core material filling can effectively improve the strength of the flying wing so as to avoid the problems of distortion and breakage.

Description

Technical Field

[0001] The utility model relates to a flying wing structure and a flying wing installation structure. Background Art

[0002] The flying wing is a component of the building curtain wall. The existing flying wing structure has the problem that the flying wing formed by bending a single metal plate has low strength and poor stability. Further improvement is needed. Utility Model Content

[0003] The utility model aims to solve at least one of the technical problems existing in the prior art. To this end, the utility model proposes a flying wing structure and a flying wing mounting structure.

[0004] A flying wing structure designed for this purpose includes a front plate assembly and a back plate assembly connected to each other, wherein the front plate assembly and the back plate assembly are combined to form a cavity filled with a honeycomb core material, and a plurality of bolts are fixed on the back plate assembly.

[0005] Preferably, the front panel assembly comprises a front panel, and outwardly bent panels are provided on upper and lower sides of the front panel, and the bent panels are fixedly connected to the back panel assembly.

[0006] Preferably, the backplane assembly at least includes a backplane, and the backplane is connected to the frontplane assembly.

[0007] Preferably, the back panel assembly further comprises two upper and lower cross beams, and the cross beams are respectively fixedly connected to the back panel and the bending plate.

[0008] Preferably, the backplane assembly further comprises a plurality of columns arranged along the extending direction of the wing, and the upper and lower sides of the columns are respectively fixedly connected to the upper and lower beams.

[0009] Preferably, the bending plate is provided with fastening screws which are threadedly connected to the cross beam and the column.

[0010] Preferably, a bending groove is provided on the bending plate, the fastening screw is provided in the bending groove, and a decorative fastener is installed in the bending groove.

[0011] Preferably, the crossbeam is in an L-shaped structure, and the crossbeam fits with the corners of the column and the corners of the back plate respectively.

[0012] A flying wing installation structure comprises a curtain wall system and a flying wing structure. The curtain wall system is provided with an adapter, the back panel assembly is fitted with the adapter, and the bolts are connected with the adapter.

[0013] Compared with the prior art, the utility model comprises a front plate assembly and a back plate assembly connected to each other, wherein the front plate assembly and the back plate assembly are combined to form a cavity, wherein the cavity is filled with a honeycomb core material, and a plurality of bolts are fixedly arranged on the back plate assembly. The front plate assembly and the back plate assembly are used to form the shape of the flying wing, and the cavity formed therein is filled with a honeycomb core material, which can effectively improve the strength of the flying wing itself to avoid the problem of distortion and fracture. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 is a schematic diagram of the cross-sectional structure of the flying wing;

[0015] Figure 2 This is a schematic diagram of the installation structure of the flying wing. DETAILED DESCRIPTION

[0016] The utility model is further described below in conjunction with the accompanying drawings and embodiments.

[0017] See also Figure 1 and Figure 2 A flying wing structure includes a front plate assembly 10 and a back plate assembly 20 connected to each other, wherein the front plate assembly 10 and the back plate assembly 20 are combined to form a cavity 100, wherein the cavity 100 is filled with a honeycomb core material 40, and a plurality of bolts 30 are fixedly arranged on the back plate assembly 20. The front plate assembly and the back plate assembly are used to form the shape of the flying wing, and the cavity formed therein is filled with the honeycomb core material, which can effectively improve the strength of the flying wing itself to avoid the problem of distortion and fracture.

[0018] At the same time, in the above embodiment, the bolts 30 provided on the back panel assembly 20 are plugged into the adapter 70 installed on the curtain wall system 80 during the later assembly with the curtain wall system 80, and then the nut is locked into the bolt 30 to complete the assembly.

[0019] Furthermore, the honeycomb core material is a metal honeycomb core material.

[0020] See also Figure 1 The front plate assembly 10 includes a front plate 110 , and the upper and lower sides of the front plate 110 are provided with outwardly bent plates 120 , and the bent plates 120 are fixedly connected to the back plate assembly 20 .

[0021] See also Figure 1 The backplane assembly 20 at least includes a backplane 210 , and the backplane 210 is connected to the frontplane assembly 10 .

[0022] See also Figure 1The back plate assembly 20 further includes two upper and lower cross beams 220, and the cross beams 220 are respectively fixedly connected to the back plate 210 and the bending plate 120. The cross beams 220 can effectively strengthen the strength of the flying wing to avoid deformation problems such as twisting of the flying wing.

[0023] See also Figure 1 The backplane assembly 20 further includes a plurality of columns 230 arranged along the extending direction of the wing, and the upper and lower sides of the columns 230 are respectively fixedly connected to the upper and lower beams 220. The function of the columns 230 is to further enhance the strength of the entire wing to ensure stability.

[0024] See also Figure 1 The back plate 210 , the cross beam 220 and the column 230 are respectively provided with mounting holes, the bolts 30 are passed through the mounting holes, and the bolt heads of the bolts 30 are fixedly connected to the column 230 .

[0025] See also Figure 1 The bending plate 120 is provided with a fastening screw 50 which is threadedly connected with the cross beam 220 and the column 230 .

[0026] See also Figure 1 The bending plate 120 is provided with a bending groove 121, the fastening screw 50 is arranged in the bending groove 121, and the decorative fastener 60 is installed in the bending groove 121. The bending groove 121 is used to hide the screw head of the fastening screw 50, so that the surface of the wing is flat and beautiful.

[0027] See also Figure 1 The crossbeam 220 is in an L-shaped structure, and the crossbeam 220 is respectively fitted with the corners of the column 230 and the corners of the back plate 210.

[0028] See also Figure 2 A flying wing installation structure includes a curtain wall system 80, an adapter 70 is arranged on the curtain wall system 80, the back panel assembly 20 is fitted with the adapter 70, and the bolt 30 is connected with the adapter 70. During assembly, the bolt 30 is plugged into the adapter 70 installed on the curtain wall system 80 until the back panel assembly 20 is fitted with the adapter 70, and then a nut is locked into the bolt 30 to complete the assembly.

[0029] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise" and the like indicating the orientation or position relationship are based on the orientation or position relationship shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present invention. The terms "first" and "second" are only used for descriptive purposes and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features.

[0030] The above shows and describes the basic principle and main features of the utility model and the advantages of the utility model. The technicians in this industry should understand that the utility model is not limited by the above embodiments. The above embodiments and the description are only to illustrate the principle of the utility model. Without departing from the spirit and scope of the utility model, the utility model will have various changes and improvements, and these changes and improvements fall within the scope of the utility model to be protected. The scope of protection claimed by the utility model is determined by the attached claims and their equivalents.

[0031] Material world.

Claims

1. A flying wing structure, characterized in that: The invention comprises a front plate assembly (10) and a back plate assembly (20) which are connected to each other. The front plate assembly (10) and the back plate assembly (20) are combined to form a cavity (100). The cavity (100) is filled with a honeycomb core material (40).

2. A flying wing structure according to claim 1, characterized in that: The front panel assembly (10) comprises a front panel (110), and outwardly bent plates (120) are provided on the upper and lower sides of the front panel (110), and the bent plates (120) are fixedly connected to the back panel assembly (20).

3. A flying wing structure according to claim 2, characterized in that: The back panel assembly (20) at least comprises a back panel (210), and the back panel (210) is connected to the front panel assembly (10).

4. A flying wing structure according to claim 3, characterized in that: The back plate assembly (20) further comprises two upper and lower cross beams (220), wherein the cross beams (220) are fixedly connected to the back plate (210) and the bending plate (120) respectively.

5. A flying wing structure according to claim 4, characterized in that: The backboard assembly (20) further comprises a plurality of columns (230) arranged along the extending direction of the wing, and the upper and lower sides of the columns (230) are respectively fixedly connected to the upper and lower cross beams (220).

6. A flying wing structure according to claim 5, characterized in that: The bending plate (120) is provided with a fastening screw (50) which is threadedly connected to the crossbeam (220) and the column (230).

7. A flying wing structure according to claim 6, characterized in that: The bending plate (120) is provided with a bending groove (121), the fastening screw (50) is arranged in the bending groove (121), and a decorative fastener (60) is installed in the bending groove (121).

8. A flying wing structure according to claim 5, characterized in that: The crossbeam (220) is in an L-shaped structure, and the crossbeam (220) is respectively fitted with the corners of the upright column (230) and the corners of the back plate (210).

9. A flying wing structure according to claim 1, characterized in that: A plurality of bolts (30) are fixedly arranged on the back plate assembly (20).

10. A flying wing installation structure, comprising a curtain wall system (80), characterized in that: It also includes the flying wing structure of claim 9, wherein an adapter (70) is provided on the curtain wall system (80), the back panel assembly (20) is fitted with the adapter (70), and the bolt (30) is connected to the adapter (70).

Images