Adhesive bonded composite-to-metal hybrid vanes and method of manufacture

Patent metadata

Field	Value
Publication number	US-11578604-B2
Application number	US-202117185010-A
Country	US
Kind code	B2
Filing date	Feb 25, 2021
Priority date	Mar 17, 2020
Publication date	Feb 14, 2023
Grant date	Feb 14, 2023

Abstract

The present disclosure provides methods and systems for composite-to-metal hybrid bonded structures compromising the laser surface treatment on titanium alloys to promote adhesive bond performance. For example, a computer may be programmed to set a laser path corresponding to a predetermined geometric pattern. A laser may be coupled to the computer and apply a pulsed laser beam to a contact surface of the titanium alloy along the predefined geometric pattern. The laser may generate an open pore oxide layer on the contact surface of the substrate with a thickness of 100 and 500 nm. The open pore oxide layer may have a topography corresponding to the predefined geometric pattern. The topography may contain high degree of open pore structure and promote adhesive bond performance. Adhesive, primer or composite resin matrix may fully infiltrate into the open pore structures. Adhesive and composite laminate may co-cure to form composite-to-titanium hybrid bonded structures.

First claim

What is claimed is:

1. A method of manufacturing a composite-to-metal hybrid vane, the method comprising:
treating a surface of a vane with a pulsed laser, the vane comprising a titanium alloy;
generating a porous oxide layer on a contact surface of the vane;
infiltrating the porous oxide layer with at least one of an adhesive, primer, or composite resin matrix; and
coupling a composite laminate to the vane.

2. The method of claim 1 , wherein coupling the composite laminate to the titanium alloy further comprises co-curing the composite laminate and the adhesive.

3. The method of claim 1 , wherein coupling the composite laminate to the titanium alloy further comprises secondary bonding of the composite laminate with the adhesive.

4. The method of claim 1 , further comprising applying the composite laminate to the adhesive prior to coupling the composite laminate to the vane.

5. The method of claim 4 , wherein applying the composite laminate to the adhesive further comprises applying the composite laminate via liquid molding techniques including resin transfer molding, autoclave processing techniques, or compression molding techniques.

6. The method of claim 1 , wherein infiltrating the porous oxide layer includes only the adhesive.

7. The method of claim 1 , wherein treating the surface of the vane with the pulsed laser further comprises applying a pulsed laser beam to the surface of the vane along a predefined geometric pattern.

8. The method of claim 1 , wherein prior to treating the surface of the vane the method comprises:
determining a predetermined set laser path corresponding to a predefined geometric pattern; and
applying, via a laser, a pulsed laser beam to the contact surface of the vane along the predefined geometric pattern, the pulsed laser beam configured to contact the contact surface at a substantially normal angle relative to the contact surface.

9. The method of claim 8 , further comprising prior to the applying, coupling the laser to a computer numeric control (CNC) tool.

10. The method of claim 8 , wherein the predetermined set laser path is a three-dimensional path corresponding to the predefined geometric pattern of the contact surface, wherein the contact surface has a complex three-dimensional surface.

11. The method of claim 8 , wherein the predefined geometric pattern comprises at least one of a linear array pattern, a perpendicular crosshatch pattern, or a rotating linear array.

12. The method of claim 8 , wherein a topography of the contact surface after applying the pulsed laser beam to the contact surface is more uniform relative to an alkaline etching surface treatment.

13. The method of claim 8 , wherein applying the pulsed laser beam to the contact surface further comprises forming an open pore oxide structure on the contact surface.

14. The method of claim 8 , wherein the laser is configured to travel along a three-dimensional path and treat a complex three-dimensional surface of the contact surface.

Assignees

• Raytheon Tech Corp

Inventors

• Fang Xiaomei
• Riehl John D
• Salisbury George Alan

Classifications

• C09J2400/166

  in the pretreated surface to be joined · CPC title

• C09J2400/163

  in the substrate · CPC title

• B23K2101/001

  Turbines · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title

• F05D2300/603

  Composites; e.g. fibre-reinforced · CPC title