Gas turbine transition duct apparatus
View Patent ↗A gas turbine transition duct is provided comprising a generally tubular main body having first and second ends, the first end being adapted to be positioned adjacent to a combustor unit and the second end being adapted to be positioned adjacent to a turbine and a collar coupled to the main body second end. The collar may have upper, lower and side portions. At least one of the side portions may be provided with a notched section.
1. A gas turbine transition duct comprising:
a generally tubular main body having first and second ends, said first end being adapted to be positioned adjacent to a combustor unit and said second end being adapted to be positioned adjacent to a turbine; and
a collar coupled to said main body second end, said collar having upper, lower and side portions, at least one of said side portions being provided with a notched section.
2. The gas turbine transition duct as set out in claim 1 , wherein said notched section is generally centered along said one side portion.
3. The gas turbine transition duct as set out in claim 2 , wherein said notched section extends between about 30% and about 70% of a length of said one side portion.
4. A gas turbine transition duct apparatus comprising:
a first turbine transition duct comprising a first generally tubular main body having first and second ends, and a first collar coupled to said main body second end, said first collar having a first upper portion, a first lower portion and first side portions, at least one of said first side portions being provided with a first notched section;
a second turbine transition duct comprising a second generally tubular main body having third and fourth ends, and a second collar coupled to said main body fourth end, said second collar having a second upper portion, a second lower portion and second side portions, at least one of said second side portions being provided with a second notched section;
said one first side portion being positioned adjacent to said one second side portion such that said first and second notched sections are located adjacent to one another, said first and second notched sections defining a relief opening between them; and
seal apparatus comprising a plug associated with said relief opening.
5. The gas turbine transition duct apparatus as set out in claim 4 , wherein said seal apparatus comprises a plug plate comprising said plug and support structure integral with said plug, wherein said support structure comprises first and second end portions.
6. The gas turbine transition duct apparatus as set out in claim 5 , wherein said one first side portion further comprises upper and lower first recessed sections and said one second side portion further comprises upper and lower second recessed sections, said support structure first end portion being received in said upper first and second recessed sections and said support structure second end portion being received in said lower first and second recessed sections.
7. The gas turbine transition duct apparatus as set out in claim 6 , wherein said seal apparatus further comprises a side seal device including a support member comprising a main body and first and second locking tabs, said support member being adapted to be positioned adjacent to and engage said plug plate.
8. The gas turbine transition duct apparatus as set out in claim 7 , wherein said one first side portion further comprises first and second slotted sections including respectively first and second slots and said one second side portion further comprises third and fourth slotted sections including respectively third and fourth slots, said first locking tab being received in said first and third slots and said second locking tab being received in said second and fourth slots.
9. The gas turbine transition duct apparatus as set out in claim 8 , wherein said side seal device further comprises spring structure coupled to said support member and engaging first and second landings on said first and second collars and said first and second generally tubular main bodies so as to retain said support member in position against said plug plate.
10. The gas turbine transition duct apparatus as set out in claim 9 , wherein said spring structure comprises first and second spring clips.
11. The gas turbine transition duct apparatus as set out in claim 10 , wherein each of said first and second spring clips comprises slots.
12. Seal apparatus adapted to seal a relief opening defined between opposing first and second transition ducts comprising:
a plug plate comprising a plug and an integral support structure, said plug being adapted to be positioned within the relief opening; and
a side seal device including a support member and spring structure, said support member being adapted to be positioned adjacent to and engage said plug plate and said spring structure being associated with said support member and adapted to engage said first and second transition ducts to maintain said support member in engagement with said plug plate.
13. Seal apparatus as set out in claim 12 , wherein said support member comprises a main body and first and second locking tabs.
14. Seal apparatus as set out in claim 12 , wherein said spring structure comprises first and second spring clips.
15. Seal apparatus as set out in claim 14 , wherein each of said first and second spring clips comprises slots.
16. Seal apparatus as set out in claim 14 , wherein each of said first and second spring clips comprises slots so as to allow said first and second spring clips to conform to the first and second transition ducts as the ducts deform during operation.
17. Seal apparatus as set out in claim 14 , wherein each of said first and second spring clips comprises slots for providing metered cooling for collars of the first and second transition ducts.
18. Seal apparatus as set out in claim 12 , wherein said support member is formed from a superalloy.