Textured structure and method of making the textured structure
The present application is directed to textured surfaces and methods for forming textured surfaces. The textured surfaces of the present application comprise a conformable film, which conforms to a texture pattern. In certain embodiments, the texture pattern comprises inks having a desired thickness. The methods of the present application may be used to form textured surfaces for a variety of applications, including, for example, aircraft having at least one interior panel with a textured surface.
1. A method of forming a laminate having a textured surface, wherein the laminate consists of: a first film having a first major surface; a texture pattern deposited on the first major surface of the first film, the texture pattern comprising an ink having a first thickness and deposited by a digital printing process; and a conformable film applied over the texture pattern and deformed around the texture pattern to form the textured surface comprising raised surface portions and lower surface portions of a major surface of the conformable film, the method comprising:
providing the first film having the first major surface;
depositing the texture pattern comprising the ink having the first thickness on the first major surface of the first film using the digital printing process;
applying the conformable film over the texture pattern;
subjecting the conformable film to a temperature and pressure sufficient to cause the conformable film to deform around the texture pattern to form the textured surface comprising the raised surface portions and the lower surface portions of the major surface of the conformable film; and
bonding the laminate to an aircraft panel by deforming the conformable film around the texture pattern a second time to form the textured surface.
2. The method of claim 1 further comprising the ink forming a colored texture pattern which shows through the conformable film so as to be at least partially visible to a naked eye.
3. The method of claim 1 wherein the first thickness of the ink is at least 0.03 mm (1 mil).
4. The method of claim 1 wherein the temperature is in a range from 93° C. (200° F.) to 204° C. (400° F.), and the pressure is in a range from 0.345 MPa (50 psi) to 1.034 MPa (150 psi).
5. The method of claim 1 wherein the bonding the laminate to the aircraft panel comprises subjecting the laminate to a bonding temperature while employing a vacuum to cause the laminate to bond to the aircraft panel.
6. A method of forming a laminate having a textured surface, wherein the laminate consists of: a first film having a first surface; a colored texture pattern deposited on the first surface of the first film, the colored texture pattern comprising an ink having a first thickness deposited by a digital printing process; and a conformable film applied over the texture pattern and deformed around the texture pattern forming the textured surface comprising raised surface portions and lower surface portions of a surface of the conformable film, the method comprising:
providing the first film having the first surface;
depositing the colored texture pattern comprising the ink having the first thickness on the first surface of the first film using the digital printing process;
applying the conformable film over the colored texture pattern so that the colored texture pattern shows through the conformable film so as to be at least partially visible to a naked eye;
subjecting the conformable film to a temperature and pressure sufficient to cause the conformable film to deform around the colored texture pattern to form the textured surface comprising the raised surface portions and the lower surface portions of the surface of the conformable film; and
bonding the laminate to an aircraft panel by subjecting the laminate to a bonding temperature while employing a vacuum and deforming the conformable film around the colored texture pattern a second time to form the textured surface.
7. The method of claim 6 wherein the temperature is in a range from 93° C. (200° F.) to 204° C. (400° F.), and the pressure is in a range from 0.345 MPa (50 psi) to 1.034 MPa (150 psi).
8. The method of claim 7 wherein the first thickness of the ink is at least 0.03 mm (1 mil).