Stepless regulation shading device for airplane dazzle window and assembly method thereof

By designing a stepless adjustment and shading device for aircraft glare windows containing slide rail components and plexiglass, the problems of poor lighting and insufficient visual observation methods in the aircraft cabin are solved, and the stepless adjustment and shading function is improved.

CN119408693APending Publication Date: 2025-02-11SHAANXI AIRCRAFT CORPORATION
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Patent Information

Application Number
CN202411490938.6
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-10-24
Publication Date
2025-02-11

AI Technical Summary

Technical Problem

In the prior art, the light performance in the aircraft cabin is poor and it is impossible to provide an effective visual observation method.

Method used

A stepless adjustment and shading device for aircraft glare windows is designed, including decorative panels, window frames, shading panels, brackets, slide rail components and plexiglass, and the stepless adjustment function of the light shield is realized through the slide rail components.

Benefits of technology

It realizes the stepless adjustment and shading function of the aircraft glare window, improves the lighting in the cabin, and provides flexible visual observation methods.

✦ Generated by Eureka AI based on patent content.

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Abstract

The invention provides a stepless adjustment shading device for an aircraft glare window and an assembly method thereof, and belongs to the technical field of aviation technology living facility system design, and the stepless adjustment shading device for the aircraft glare window comprises a decorative plate, a window frame, a shading plate, a support, two sliding rail assemblies and organic glass; the support is arranged on the window frame, the window frame is fixed on the decorative plate, one parts of the two sliding rail assemblies are fixedly installed on the decorative plate, and the other parts of the two sliding rail assemblies penetrate through the decorative plate and are connected to the support on the window frame; the organic glass is fixedly installed on the two sliding rail assemblies, and the shading plate is located between the two sliding rail assemblies and can move up and down along the two sliding rail assemblies. The dazzle window can be decorated by an airplane, and meanwhile the technical requirement that the dazzle window is provided with the light shielding plate is met; the operation shading plate can freely slide in a guide rail of the sliding rail assembly and can be stopped at any position, and the stepless adjusting function of the dazzle window shading plate is achieved; the overall weight is light.
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Description

Technical Field

[0001] The invention belongs to the technical field of aviation technology and living facility system design, and in particular relates to a stepless adjustment shading device for an aircraft glare window and an assembly method thereof. Background Art

[0002] According to the characteristics of the aircraft, interior decoration is required in the cabin to provide a comfortable living and working environment for the crew members on board; shading devices are required at the glare windows to improve the lighting in the cabin and provide a visual observation path.

[0003] Therefore, it is necessary to design a stepless adjustable shading device for aircraft glare windows according to the aircraft interior and glare window structure to meet the living and working needs of the crew on board. Summary of the invention

[0004] In order to solve the technical problem of poor lighting in the cabin and inability to provide a visual observation path in the prior art, the present invention provides an aircraft glare window stepless adjustment shading device according to the aircraft glare window structure and interior decoration installation characteristics. This aircraft glare window stepless adjustment shading device is easy to use and operate, can be adjusted to any position of the glare window, and has a light overall weight. The technical solution is as follows:

[0005] In a first aspect, a stepless adjustable shading device for an aircraft glare window is provided, comprising: a decorative panel, a window frame, a shading panel, a bracket, two slide rail assemblies, and organic glass;

[0006] The bracket is set on the window frame, the window frame is fixed on the decorative panel, one part of the two slide rail assemblies is installed and fixed on the decorative panel, and the other part passes through the decorative panel and is connected to the bracket on the window frame; the organic glass is fixed on the two slide rail assemblies, the shading plate is located between the two slide rail assemblies, and can move up and down along the two slide rail assemblies.

[0007] Optionally, the bracket consists of a first support plate nut, a plate bending part, and a base plate; the first support plate nut is fixed in the recessed area of ​​the plate bending part, and the plate bending part and the base plate are butt-jointed and fixed; the base plate is adhered to the window frame; the plate bending part is fixedly connected to the slide rail assembly and the decorative panel.

[0008] Optionally, the plate bending member is fixedly connected to the slide rail assembly and the decorative panel by a second screw.

[0009] Optionally, the first support plate nut is fixed to the recessed area of ​​the plate bending part by a first rivet.

[0010] Optionally, the plate bending piece and the base plate are butt-jointed and fixed by a second rivet.

[0011] Optionally, each slide rail assembly is composed of a bracket bar and a guide rail;

[0012] The support bar is a Z-shaped structure, the guide rail is fixed on the support bar, and the plate bending part is fixedly connected to the support bar by a second screw; the support bar is also fixedly connected to the decorative plate.

[0013] Optionally,

[0014] The bracket strip is fixedly connected to the decorative plate by a third screw.

[0015] The window frame is fixed on the decorative plate by means of a first screw.

[0016] Optionally, the base plate is adhered to the window frame by adhesive.

[0017] Furthermore, a pad strip is provided on the support strip to reduce shock to the organic glass.

[0018] In a second aspect, a method for assembling the aircraft glare window steplessly adjustable shading device according to any one of the first aspects is provided, the method comprising:

[0019] First assemble the bracket, then stick the bracket to the window frame and connect it to the decorative panel;

[0020] Assemble the slide rail assembly, install the organic glass on the two slide rail assemblies, and then install the shading plate on the slide rail assembly to form a semi-assembled assembly of the glare window stepless adjustment shading device;

[0021] The semi-assembled component of the glare window stepless adjustment shading device is installed and fixed on the decorative plate, and connected to the bracket on the window frame through the decorative plate.

[0022] The beneficial effects of the present invention are at least:

[0023] The present invention provides a stepless adjustable shading device for aircraft glare windows, comprising: a decorative panel, a window frame, a shading plate, a bracket, two slide rail assemblies, and organic glass; the bracket is arranged on the window frame, the window frame is fixed on the decorative panel, a part of the two slide rail assemblies is installed and fixed on the decorative panel, and the other part passes through the decorative panel and is connected to the bracket on the window frame; the organic glass is fixed on the two slide rail assemblies, the shading plate is located between the two slide rail assemblies, and can move up and down along the two slide rail assemblies. The present invention can realize the decoration of the glare windows of aircraft, and also meet the technical requirements of setting shading plates for glare windows. The shading plate can be operated to slide freely in the guide rail of the slide rail assembly, and can be stopped at any position, so as to realize the stepless adjustment function of the glare window shading plate. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 This is the actual assembly application diagram;

[0025] Figure 2 This is a structural diagram of a stepless adjustable shading device for aircraft glare windows;

[0026] Figure 3It is a cross-sectional view of a stepless adjustable shading device for aircraft glare windows;

[0027] Figure 4 Assembly drawing for the bracket;

[0028] Figure 5 Assembly drawing for the slide rail assembly;

[0029] Among them: 1-decorative panel, 2-window frame, 3-shading plate, 4-bracket, 5-first screw, 6-second screw, 7-third screw, 8-slide rail assembly, 9 organic glass, 10-screw, 11-support plate nut, 12-gasket, 4a-first support plate nut, 4b-first rivet, 4c-plate bending piece, 4d-second rivet, 4e-bottom plate, 8a-bracket bar, 8b-guide rail. DETAILED DESCRIPTION

[0030] The present invention is further described in detail below through specific implementation modes and drawings.

[0031] An embodiment of the present invention provides a stepless shading device for aircraft glare windows, such as Figure 1 , Figure 2 and Figure 3 As shown, the device includes: a decorative panel 1, a window frame 2, a sunshade 3, a bracket 4, two slide rail assemblies 8, and organic glass 9.

[0032] The bracket 4 is adhered to the window frame 2 by adhesive, and the window frame 2 is fixed to the decorative panel 1 .

[0033] One part of the two slide rail assemblies 8 is mounted and fixed on the decorative panel 1 , and the other part passes through the decorative panel 1 and is connected to the bracket 4 on the window frame 2 .

[0034] The organic glass 9 is fixedly mounted on the two slide rail assemblies 8.

[0035] The shading plate 3 is located between the two slide rail assemblies 8 and can move up and down along the two slide rail assemblies 8 .

[0036] When in use, the shading plate 3 can be pushed and pulled up and down according to actual needs, so that the shading plate 3 can stay at any position to achieve the purpose of shading, thereby realizing the stepless adjustment function of the glare window shading plate.

[0037] An embodiment of the present invention provides a stepless shading device for aircraft glare windows, such as Figure 1 , Figure 2 and Figure 3 As shown, the device may include: a decorative panel 1, a window frame 2, a sunshade 3, a bracket 4, two slide rail assemblies 8, organic glass 9, and a gasket 12.

[0038] The bracket 4 is adhered to the window frame 2 by adhesive, and the window frame 2 is fixed to the decorative panel 1 .

[0039] One part of the two slide rail assemblies 8 is mounted and fixed on the decorative panel 1 , and the other part passes through the decorative panel 1 and is connected to the bracket 4 on the window frame 2 .

[0040] The organic glass 9 is fixedly mounted on the two slide rail assemblies 8.

[0041] The shading plate 3 is located between the two slide rail assemblies 8 and can move up and down along the two slide rail assemblies 8 .

[0042] See also Figure 4 , the bracket 4 is composed of a first support plate nut 4a, a rivet 4b, a plate bending piece 4c, a rivet 4d, and a bottom plate 4e;

[0043] The first support plate nut 4a is fixed to the recessed area of ​​the plate bending part 4c by a rivet 4b;

[0044] The plate bending part 4c and the bottom plate 4e are fixed by rivets 4d;

[0045] The bottom plate 4e is adhered to the window frame 2 by adhesive;

[0046] The plate bending member 4 c is fixedly connected to the slide rail assembly 8 and the decorative panel 1 by means of the second screw 6 .

[0047] The window frame 2 is fixed to the decorative panel 1 by means of first screws 5 .

[0048] See also Figure 5 , each slide rail assembly 8 is composed of a bracket bar 8a and a guide rail 8b;

[0049] The support bar 8a is a Z-shaped structure, the guide rail 8b is fixed on the support bar 8a, and the plate bending piece 4c is fixedly connected to the support bar 8a by the second screw 6. The support bar 8a is fixedly connected to the decorative plate 1 by the third screw 7.

[0050] The cushion strip 12 is arranged on the support strip, and the cushion strip 12 is used to play a shock absorbing role on the organic glass 9.

[0051] The assembly method of the aircraft glare window stepless adjustment shading device provided by the embodiment of the present invention comprises the following steps:

[0052] Press the support plate nut 4a, rivet 4b, plate bending piece 4c, rivet 4d, bottom plate 4e Figure 4 Assemble the bracket 4, stick the bracket 4 on the window frame 2 with an adhesive, and then connect it to the decorative plate 1 with a first screw 5;

[0053] The support strip 8a and the guide rail 8b are pressed with adhesive. Figure 5 Assemble the slide rail assembly 8, and install the organic glass 9 on the bracket bars 8a of the two slide rail assemblies 8 through the fourth screw 10, the second support plate nut 11, and the pad 12;

[0054] Press the sunshade 3 Figure 2As shown, it is installed on the bracket bar 8a of the slide rail assembly 8 to form a semi-assembled assembly of the glare window stepless adjustment shading device;

[0055] The semi-assembled component of the glare window stepless adjustment shading device is fixed on the decorative panel 1 by the third screw 7, and connected to the bracket 4 on the window frame 2 by the second screw 6 through the decorative panel 1, thereby completing the assembly of the aircraft glare window stepless adjustment shading device.

[0056] The above only expresses the implementation mode of the present invention, and its description is relatively specific and detailed, but it cannot be understood as limiting the scope of the patent. It should be pointed out that for ordinary technicians in this field, several modifications and improvements can be made without departing from the concept of the present invention, which all belong to the protection scope of the present invention. In addition, the parts not detailed in the present invention are all conventional technologies.

Claims

1. A stepless shading device for aircraft glare windows, characterized in that: include: Decorative panels, window frames, sunshades, brackets, two slide rail assemblies, plexiglass; The bracket is set on the window frame, the window frame is fixed on the decorative panel, one part of the two slide rail assemblies is installed and fixed on the decorative panel, and the other part passes through the decorative panel and is connected to the bracket on the window frame; the plexiglass is fixed on the two slide rail assemblies, the shading plate is located between the two slide rail assemblies, and can move up and down along the two slide rail assemblies.

2. The device according to claim 1, characterized in that The bracket is composed of a first support plate nut, a plate bending part, and a bottom plate; the first support plate nut is fixed in the recessed area of ​​the plate bending part, and the plate bending part and the bottom plate are butt-jointed and fixed; the bottom plate is adhered to the window frame; the plate bending part is fixedly connected to the slide rail assembly and the decorative plate.

3. The device according to claim 2, characterized in that The plate bending part is fixedly connected with the slide rail assembly and the decorative plate through the second screw.

4. The device according to claim 2, characterized in that The first supporting plate nut is fixed to the recessed area of ​​the plate bending part through a first rivet.

5. The device according to claim 2, characterized in that The plate bending part and the bottom plate are butt-jointed and fixed by a second rivet.

6. The device according to claim 2, characterized in that Each slide rail assembly consists of a bracket bar and a guide rail; The support bar is a Z-shaped structure, the guide rail is fixed on the support bar, and the plate bending part is fixedly connected to the support bar by a second screw; the support bar is also fixedly connected to the decorative plate.

7. The device according to claim 6, characterized in that The bracket strip is fixedly connected to the decorative plate by a third screw; The window frame is fixed on the decorative plate by means of a first screw.

8. The device according to claim 2, characterized in that The base plate is attached to the window frame by adhesive.

9. The device according to claim 6, characterized in that The support bar is provided with a cushion bar which has a shock-absorbing effect on the organic glass.

10. An assembly method for the aircraft glare window stepless adjustment shading device according to any one of claims 1 to 9, characterized in that: The method comprises: First assemble the bracket, then stick the bracket to the window frame and connect it to the decorative panel; Assemble the slide rail assembly, install the organic glass on the two slide rail assemblies, and then install the shading plate on the slide rail assembly to form a semi-assembled assembly of the glare window stepless adjustment shading device; The semi-assembled component of the glare window stepless adjustment shading device is installed and fixed on the decorative plate, and connected to the bracket on the window frame through the decorative plate.

Citation Information

Patent Citations

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