초록 ▼

A fan blade for a gas turbine engine having an airfoil with a leading edge; a trailing edge; a concave side; and a convex side. The blade has an integral platform with: a convex fillet merging with the airfoil; a forward edge; an aft edge; and a thickness defined between a top surface and an undersi

A fan blade for a gas turbine engine having an airfoil with a leading edge; a trailing edge; a concave side; and a convex side. The blade has an integral platform with: a convex fillet merging with the airfoil; a forward edge; an aft edge; and a thickness defined between a top surface and an underside surface. The platform includes a stiffener on the underside surface adjacent the convex side of the blade, such that the stiffener defines a blade-off event platform fracture path on a second side of the platform adjacent the following blade and adjacent the convex side of the airfoil.

대표청구항 ▼

I claim: 1. A method of reducing failure of a following fan blade of a gas turbine engine during impact with a dislodged fan blade during a blade-off event, each fan blade comprising: an airfoil having: a leading edge; a trailing edge; a concave side; and a convex side; and an integral platform for

I claim: 1. A method of reducing failure of a following fan blade of a gas turbine engine during impact with a dislodged fan blade during a blade-off event, each fan blade comprising: an airfoil having: a leading edge; a trailing edge; a concave side; and a convex side; and an integral platform formed with the airfoil as a single piece and having: a convex fillet merging with the airfoil; a forward edge; an aft edge; and a thickness defined between a top surface and an underside surface; the method comprising: defining a platform fracture path on a side of platform adjacent the convex side of the airfoil, wherein the path includes a single stiffening member on the underside surface adjacent the convex side of each blade extending transversely from the convex side of the airfoil. 2. A method according to claim 1 wherein the stiffener reduces an absolute value of a curvature of the platform fracture path. 3. A method according to claim 2 wherein the stiffener reduces convex curvature of the platform fracture path. 4. A method according to claim 2 wherein the stiffener reduces a rate of change of curvature of the platform fracture path. 5. A method according to claim 4 wherein the stiffener reduces an inversion of curvature of the platform fracture path. 6. A method according to claim 1 wherein the stiffener comprises an increase in the platform thickness progressing in a downstream direction from the forward edge to the aft edge.