Air turbine starter with damping member
An air turbine starter for starting an engine includes a starter housing having an inlet, an outlet, and a flow path extending between the inlet and the outlet. The air turbine starter includes a rotatable turbine member having a central hub defining a platform and a set of blades extending radially from the platform. The air turbine starter also includes a damping member.
1. An air turbine starter for starting an engine, comprising:
a starter housing having an inlet, an outlet, and a flow path extending between the inlet and the outlet;
a rotatable turbine member comprising a central hub defining a platform, and a set of blades circumferentially spaced about the platform and extending radially from the platform into the flow path; and
a damping member defining a body having a wearable portion and an axial stop, the axial stop projecting axially to the wearable portion and defining an axial boundary, and wherein the wearable portion is axially confronting at least one of the platform or the set of blades, wherein the wearable portion is located axially between the axial stop and the at least one of the platform or the set of blades, wherein the wearable portion comprises a first material and the axial stop portion comprises a second material different from the first material, wherein the axial stop of the body has at least one of a greater hardness or a greater strength than the wearable portion of the body and wherein the wearable portion is configured to exert a braking force.
2. An air turbine starter for starting an engine, comprising:
a starter housing defining a housing inlet, a housing outlet, and a flow path extending between the housing inlet and the housing outlet;
a rotatable turbine member comprising a central hub defining a platform, and a set of blades circumferentially spaced about the platform and extending radially from the platform into the flow path; and
a set of damping members, with a damping member in the set of damping members comprising a disk with a rim located within the starter housing and wherein the disk forms an axial stop portion and the rim forms a wearable portion confronting at least one of the platform or the set of blades, the wearable portion located axially between the axial stop portion and the at least one of the platform or the set of blades, wherein the wearable portion comprises a first material and the axial stop portion comprises a second material different from the first material and wherein the axial stop portion has at least one of a greater hardness or a greater strength than the wearable portion and wherein the wearable portion is configured to exert a braking force.
3. The air turbine starter of claim 2 , wherein the wearable portion is radially aligned with the platform.
4. The air turbine starter of claim 2 , wherein the wearable portion comprises at least one of aluminum, composite alloy, or a composite material, and wherein the axial stop portion comprises at least one of steel, nickel, or nickel alloy.
5. The air turbine starter of claim 2 , further comprising a seal and wherein the damping member is mounted between the starter housing and the seal.
6. The air turbine starter of claim 2 , wherein the damping member at least partially defines the flow path.
7. The air turbine starter of claim 2 , wherein the set of damping members further comprises a second damping member positioned radially outward of the rotatable turbine member.
8. The air turbine starter of claim 2 , wherein the wearable portion comprises at least one of aluminum, composite alloy, or a composite material, and wherein the axial stop portion comprises at least one of steel, nickel, or nickel alloy.
9. The air turbine starter of claim 2 , further comprising an operative axial spacing defined between the wearable portion and the rotatable turbine member, wherein the operative axial spacing is between 0.1-3 cm during balanced rotation of the rotatable turbine member during standard operation.
10. The air turbine starter of claim 2 , wherein the set of damping members further comprises a second damping member radially spaced from the set of blades and defining a radial boundary for the rotatable turbine member.
11. The air turbine starter of claim 10 , wherein at least one of the damping member or the second damping member comprises at least one of a metallic material, a composite material, a polymeric material, an abradable material, steel, aluminum, nickel, nickel alloy, ceramic, graphite, or silicon.
12. The air turbine starter of claim 10 , wherein the axial stop portion is spaced from the rotatable turbine member by a distance of 1-15 cm during balanced rotation of the rotatable turbine member during standard operation.
13. The air turbine starter of claim 12 , wherein the radial boundary is spaced from the rotatable turbine member by a distance of 0.1-3 cm during balanced rotation of the rotatable turbine member during standard operation.
14. The air turbine starter of claim 10 , wherein the second damping member comprises a containment ring surrounding the rotatable turbine member and defining the radial boundary.
15. The air turbine starter of claim 2 , wherein the wearable portion includes at least one of a groove, an indent, or dimpling to promote gradual wearing.
16. An air turbine starter for starting an engine, comprising:
a starter housing defining a starter housing inlet, a starter housing outlet, and a flow path extending between the starter housing inlet and the starter housing outlet;
a rotatable turbine member comprising a central hub defining a platform, and a set of blades circumferentially spaced about the platform and extending radially from the platform into the flow path;
a first damping member comprising a disk with a rim located within the starter housing, wherein the disk forms an axial stop portion and the rim forms a wearable portion confronting at least one of the platform or the set of blades, the wearable portion located axially between the axial stop portion and the at least one of the platform or the set of blades, wherein the wearable portion comprises a first material and the axial stop portion comprises a second material different from the first material and wherein the axial stop portion has at least one of a greater hardness or a greater strength than the wearable portion; and
a second damping member, including a containment ring located within the starter housing, the second damping member radially spaced from the set of blades and defining a radial boundary confining the rotatable turbine member.