Leaf seal for transition duct in turbine system
A turbine system is disclosed. In one embodiment, the turbine system includes a transition duct. The transition duct includes an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The transition duct further includes an interface member for interfacing with a turbine section. The turbine system further includes a leaf seal contacting the interface member to provide a seal between the interface member and the turbine section.
1. A turbine system, comprising:
a transition duct comprising an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis, the outlet of the transition duct offset from the inlet along the longitudinal axis, the radial axis and the tangential axis, the transition duct further comprising an interface member for interfacing with a turbine section; and
a leaf seal contacting the interface member to provide a seal between the interface member and the turbine section, the leaf seal comprising a leaf element and a pin, the pin mounting the leaf seal to the interface member, the leaf seal capable of sealing the transition duct to the turbine section during movement of the transition duct along the longitudinal axis, the radial axis and the tangential axis.
2. The turbine system of claim 1 , wherein the leaf element is movable along the pin in a generally axial direction.
3. The turbine system of claim 2 , wherein the interface member comprises a flange configured to restrict axial movement of the leaf element.
4. The turbine system of claim 1 , wherein the leaf seal further comprises a spring element applying a biasing force to the leaf element.
5. The turbine system of claim 1 , further comprising a plurality of leaf seals.
6. The turbine system of claim 1 , further comprising a plurality of interface members.
7. The turbine system of claim 1 , further comprising a plurality of transition ducts, each of the plurality of transition ducts disposed annularly about the longitudinal axis and connected to the turbine section.
8. The turbine system of claim 1 , wherein the interface member is a first interface member, further comprising the turbine section, the turbine section comprising a second interface member for interfacing with the first interface member, the leaf seal contacting the second interface member to provide a seal between the first and second interface members.
9. The turbine system of claim 8 , wherein the turbine section comprises a first stage bucket assembly, and wherein no nozzles are disposed upstream of the first stage bucket assembly.
10. A turbine system, comprising:
a transition duct comprising an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis, the outlet of the transition duct offset from the inlet along the longitudinal axis, the radial axis and the tangential axis, the transition duct further comprising a first interface member;
a turbine section comprising a second interface member; and
a leaf seal contacting and providing a seal between the first interface member and the second interface member, the leaf seal comprising a leaf element and a pin, the pin mounting the leaf seal to the first interface member, the leaf seal capable of sealing the transition duct to the turbine section during movement of the transition duct along the longitudinal axis, the radial axis and the tangential axis.
11. The turbine system of claim 10 , wherein the leaf element is movable along the pin in a generally axial direction.
12. The turbine system of claim 11 , wherein the first interface member comprises a flange configured to restrict axial movement of the leaf element.
13. The turbine system of claim 10 , wherein the leaf seal further comprises a spring element applying a biasing force to the leaf element.
14. The turbine system of claim 10 , further comprising a plurality of leaf seals.
15. The turbine system of claim 10 , further comprising a plurality of first interface members and a plurality of second interface members.
16. The turbine system of claim 10 , further comprising a plurality of transition ducts, each of the plurality of transition ducts disposed annularly about the longitudinal axis and connected to the turbine section.