Composite component having angled braze joint, coupon brazing method and related storage medium
Various aspects include a composite component (also known as a Shear Enabled Regionally Engineered Facet (SEREF)) and methods of forming such a component. In some cases, a method includes: forming a slot in a main body of a metal alloy component, the slot extending at least partially through a wall of the metal alloy component, the forming of the slot including forming an angled main body interface in the wall of the metal alloy component; forming a coupon for coupling with the slot in the metal alloy component, the coupon having an angled coupon interface complementing the angled main body interface; and brazing the coupon to the main body at the slot to form a composite component.
1. A composite component comprising:
a metal alloy component including a main body, the main body having:
a wall having an inner surface and an outer surface; and
a slot extending at least partially through the wall, the slot including an angled main body interface in the wall;
a coupon coupled with the slot, the coupon having an angled coupon interface complementing the angled main body interface, wherein the coupon has a larger diameter (LD) spanning the slot across the outer surface of the main body; and a smaller diameter (SD) spanning the slot across an inner surface of the main body, wherein the LD is defined by:
LD=((2 *Z )/tan α)+SD
wherein Z=a thickness of the wall and α=an angle of the angled main body interface and the angled coupon interface, as measured from a plane coincident with the outer surface of the main body; and
a braze joint coupling the coupon to the main body at the slot.
2. The composite component of claim 1 , wherein the metal alloy component includes a high-gamma prime alloy or a brittle alloy including: René 125, René 80, René N5, René N4, René 108, GTD-111, GTD-444, Inconel (IN) 738, IN792, MAR-M200, MAR-M247, CMSX-3, CMSX-4, PWA1480, PWA1483, or PWA1484.
3. The composite component of claim 1 , wherein the angle α is between approximately 10 degrees and approximately 45 degrees, as measured from the plane coincident with the outer surface of the main body.
4. The composite component of claim 1 , wherein the angle α is between approximately 10 degrees and approximately 25 degrees, as measured from the plane coincident with the outer surface of the main body.
5. The composite component of claim 1 , wherein the angled main body interface and the angled coupon interface are configured to bear a predominately shear stress in response to application of tension on the composite component.
6. The composite component of claim 1 , wherein the composite component includes a turbomachine component.
7. The composite component of claim 1 , wherein the coupon includes the metal alloy or a distinct metal alloy from the metal alloy of the metal alloy component.