Laser surface treatment on stainless steel and nickel alloys for adhesive bonding
Methods and systems for the laser surface treatment on stainless steel alloys and nickel alloys may include 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 substrate along the predefined geometric pattern. The pulsed laser beam may have a laser power between 0.1 W and 100 W, single pulse fluence 1 mJ/mm 2 and 1025 mJ/mm 2 and a laser speed between 25.4 cm/s and 127 cm/s. The laser may generate an open pore oxide layer on the contact surface of the substrate with a thickness of 0.1-1 μm, an open pore distance of 0.05-1 μm. The open pore oxide layer may have a topography corresponding to the predefined geometric pattern. The topography may contain open pore structures and promote adhesive bond performance.
1. A method for manufacturing an airfoil, the method comprising:
disposing an airfoil under a system comprising a computer numerical control (CNC) tool coupled to a laser;
programming one or more processors with a predetermined set laser path corresponding to a predefined geometric pattern for the laser along the airfoil to form a program;
commanding, by the one or more processors and in response to execution of the program, a laser to apply a pulsed laser beam to a contact surface of the airfoil along the predefined geometric pattern, the pulsed laser beam having a single pulse fluence between 1 mJ/mm 2 and 1025 mJ/mm 2 , wherein the airfoil comprises at least one of nickel or steel;
in response to the commanding the laser along the predefined geometric pattern, forming a topography on the contact surface having a height between 0.1 μm and 1 μm, an open pore structure with a pore distance between 0.05 and 1 μm, and an oxide layer between 0.01 and 0.3 μm, wherein:
the contact surface is at least one of a pressure side and a suction side of the airfoil,
maintaining the pulsed laser beam substantially normal to the contact surface during operation, and
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, and
disposing an adhesive on the contact surface; and
bonding a second substrate to the contact surface of the airfoil.
2. The method of claim 1 , further comprising prior to the commanding, by the processor, coupling the laser to a computer numeric control (CNC) tool.
3. The method of claim 1 , wherein the single pulse fluence is between 10 mJ/mm2 and 205 mJ/mm2.
4. The method of claim 1 , wherein the predefined geometric pattern comprises at least one of a perpendicular crosshatch pattern or a rotating linear array.
5. The method of claim 1 , wherein the pulsed laser beam comprises a wavelength of about 355 nm or about 1,064 nm.
6. The method of claim 1 , wherein the second substrate has a dissimilar material relative to the airfoil.