Seal usable between a transition and a turbine vane assembly in a turbine engine
View Patent ↗A seal usable to seal a transition in a can-annular combustion system of a turbine engine to a turbine vane assembly to direct exhaust gases through the turbine vane assembly. The seal may be formed from an elongated body extending along an outer edge of the transition and having first and second edges. The first edge of the seal may be attached to the transition, and the elongated body may extend away from the transition edge and contact a portion of the turbine vane assembly. The elongated body may flex during use without yielding or otherwise deforming.
1. A seal usable to seal a transition in a can-annular combustion system of a turbine engine to a turbine vane assembly, comprising:
an elongated body extending along an edge of the transition and attached to the transition, wherein the elongated body includes a first edge attached to the transition and a second edge in contact with the turbine vane assembly, and
a secondary clip attached to the turbine vane assembly such that a portion of the elongated body bears against the secondary clip to form a seal between the transition and the turbine vane assembly,
wherein the elongated body extends away from the transition and contacts a portion of the turbine vane assembly enabling a seal to be formed and the elongated body to flex when the turbine engine is operating.
2. The seal of claim 1 , wherein the elongated body is comprised of first and second sheets coupled together.
3. The seal of claim 1 , wherein the elongated body is formed from a transition attachment section adapted to be coupled to the transition, an angled extension section extending between the transition and the turbine vane assembly, and a turbine vane assembly sealing section for contacting the turbine vane assembly.
4. The seal of claim 1 , further comprising a support device coupled to the transition and positioned between the elongated body and the transition for limiting bending of the elongated body toward the transition.
5. The seal of claim 4 , wherein the support device comprises a protrusion extending from the support device that corresponds with the elongated body so that the elongated body is supported by the support device when the elongated body is deflected.
6. The seal of claim 1 , wherein the elongated body is coupled to inner and to outer edges of the transition.
7. The seal of claim 1 , wherein the secondary clip further comprises a fixating device for preventing the secondary clip from separating from a rib on the turbine vane assembly.
8. The seal of claim 1 , wherein the secondary clip further comprises a wear reduction surface at a location where the elongated body contacts the secondary clip.
9. The seal of claim 8 , wherein the wear reduction surface comprises felt metal.
10. The seal of claim 1 , wherein the secondary clip is prevented from circumferential movement using at least one pin.
11. The seal of claim 1 , wherein the elongated body includes an offset lip at a side edge of the elongated body for sealing the elongated body to an adjacent transition seal.
12. A seal usable to seal a transition in a can-annular combustion system of a turbine engine to a turbine vane assembly, comprising:
an elongated body extending along an edge of the transition and attached to the transition, wherein the elongated body includes a first edge attached to the transition and a second edge in contact with the turbine vane assembly, and wherein the elongated body extends away from the transition and contacts a portion of the turbine vane assembly enabling a seal to be formed and the elongated body to flex when the turbine engine is operating;
a support device coupled to the transition and positioned between the elongated body and the transition for limiting bending of the elongated body toward the transition; and
a secondary clip attached to the turbine seal assembly such that a portion of the elongated body bears against the secondary clip to form a seal between the transition and the turbine vane assembly.
13. The seal of claim 12 , wherein the elongated body is comprised of first and second sheets coupled together.
14. The seal of claim 12 , wherein the elongated body is formed from a transition attachment section adapted to be coupled to the transition, an angled extension section extending between the transition and the turbine vane assembly, and a turbine vane assembly sealing section for contacting the turbine vane assembly.
15. The seal of claim 12 , wherein the support device comprises a protrusion extending from the support device that corresponds with the elongated body so that the elongated body is supported by the support device when the elongated body is deflected.
16. The seal of claim 12 , wherein the secondary clip further comprises a fixating device for preventing the secondary clip from separating from a rib on the turbine vane assembly.
17. The seal of claim 12 , wherein the secondary clip further comprises a wear reduction surface at a location where the elongated body contacts the secondary clip.
18. The seal of claim 17 , wherein the wear reduction surface comprises felt metal.
19. The seal of claim 12 , wherein the elongated body includes an offset lip at a side edge of the elongated body for sealing the elongated body to an adjacent transition seal.