Containment engine case with local features and outer surface reinforcement section
A containment case includes an annular body bound by an inner surface and an outer surface and an outer surface feature extending outward from the outer surface. The annular body includes a containment section and an outer reinforcement section extending outwards from the outer surface and subtending a sector of the containment section. The reinforcement section includes a reinforcement thickness that is greater than a casing thickness of the containment section at least partially coinciding with the outer surface feature.
1. A containment case comprising:
an annular body limited by an outer surface and an inner surface, the annular body comprising:
a containment section having a casing thickness defined by a radial distance between the inner surface and the outer surface; and
a reinforcement section subtending a sector of the containment section that defines a reinforcement thickness between the inner surface and the outer surface that is greater than the casing thickness; and
an outer surface feature extending outward from the outer surface that at least partially coincides with the reinforcement section, wherein the outer surface feature coincides with a circumferential end of the reinforcement section.
2. The containment case of claim 1 , wherein the outer surface feature is entirely within the reinforcement section.
3. The containment case of claim 2 , wherein the inner surface of the containment section and the reinforcement section is cylindrical, and wherein the outer surface of reinforcement section is radially outward from the remainder of the outer surface of the containment section.
4. The containment case of claim 1 , wherein an axial extent of the reinforcement section is at least equal to an axial extent of the containment section.
5. The containment case of claim 1 , wherein the reinforcement section includes one or more ribs extending circumferentially along the containment section.
6. The containment case of claim 1 , wherein the reinforcement section defines an annular section.
7. A gas turbine engine comprising:
a bladed rotor operatively associated with a direction of rotation about an axis of the gas turbine engine; and
a containment case comprising:
an annular body limited by an outer surface and an inner surface, the annular body comprising:
a containment section circumscribing the bladed rotor and having a casing thickness defined by a radial distance between the inner surface and the outer surface; and
a reinforcement section subtending a sector of the containment section that defines a reinforcement thickness between the inner surface and the outer surface that is greater than the casing thickness; and
an outer surface feature extending outward from the outer surface that at least partially coincides with the reinforcement section, wherein the outer surface feature coincides with a circumferential end of the reinforcement section.
8. The gas turbine engine of claim 7 , wherein the reinforcement section circumferentially precedes the outer surface feature relative to the direction of rotation.
9. The gas turbine engine of claim 8 , wherein the outer surface feature is entirely within the reinforcement section.
10. The gas turbine engine of claim 9 , wherein the inner surface of the containment section and the reinforcement section is cylindrical, and wherein the outer surface of the reinforcement section is radially outward from the remainder of the outer surface of the containment section.
11. The gas turbine engine of claim 7 , wherein an axial extent of the reinforcement section is at least equal to an axial extent of the containment section.