초록 ▼

A combustor for a gas turbine is provided having a nozzle assembly located at one end and a combustion chamber defining a second end of the combustor. A venturi is positioned within the combustor, between the nozzle and the combustion chamber. The venturi defines a passageway therein having a first

A combustor for a gas turbine is provided having a nozzle assembly located at one end and a combustion chamber defining a second end of the combustor. A venturi is positioned within the combustor, between the nozzle and the combustion chamber. The venturi defines a passageway therein having a first side facing the nozzle and a second side facing the combustion chamber. Compressed air is directed into an inlet in fluid communication with the first and second sides of the venturi passageway. The venturi passageway directs the compressed air from the inlet in opposite directions within the first and second sides of the passageway for cooling the venturi.

대표청구항 ▼

What is claimed is: 1. A combustor for a gas turbine comprising: a nozzle assembly located at a first end of the combustor; a combustion chamber defined within the combustor, downstream of the nozzle; a venturi positioned within the combustor and defining a transition between the first end and the

What is claimed is: 1. A combustor for a gas turbine comprising: a nozzle assembly located at a first end of the combustor; a combustion chamber defined within the combustor, downstream of the nozzle; a venturi positioned within the combustor and defining a transition between the first end and the combustion chamber, the venturi having a venturi wall and a radially outer wall adjacent to and running along an interior of the combustor and an internal passageway therebetween, the internal passageway having first and second passageway portions and a radial plenum extending radially inward towards the wall of the venturi and defined by sidewalls that extend in a generally radial direction, with the radial plenum being in direct fluid communication with the first and second passageway portions, wherein the first passageway portion extends along the venturi wall towards the first end of the combustor and the second passageways portion extends along the venturi wall towards the second end of the combustor, and wherein the radial plenum engages the first and second passageway portions adjacent the wall of the venturi; and a compressed air source directing cooling air into the first and second passageway portions via the radial plenum, the first and second passageway portions directing the compressed air from the source in opposite directions within the venturi. 2. The combustor of claim 1 further comprising a secondary passageway communicating with a downstream end of the second side of the venturi passageway, wherein the air flow moving through the second passageway portion into the secondary passageway is reversed in direction and directed towards the first side of the of the venturi. 3. The combustor of claim 2 further comprising a cooling air exit positioned at an end of the first passageway portion directing the cooling air into the first end of the combustor. 4. The combustor of claim 3 wherein the secondary passageway and the first passageway portion are each in fluid communication with the cooling air exit. 5. The combustor of claim 4 wherein the cooling air exit directs the air flow from the secondary passageway and the first passageway portion into the first end of the combustor, upstream of the venturi. 6. The combustor of claim 1, wherein the radial plenum communicates with the first passageway portion at a position behind the upstream side of the venturi within the combustor. 7. A combustor for a gas turbine comprising: a nozzle assembly located at a first end of the combustor; a combustion chamber defined within the combustor, downstream of the nozzle; a venturi positioned within the combustor and defining a transition between the first end and the combustion chamber, the venturi having a venturi wall and a radially outer wall adjacent to and running along an interior of the combustor and an internal passageway therebetween, the internal passageway having a first side and a second side located on and extending along opposite sides of an apex of the venturi and a redial plenum extending radially inward towards the venturi wall and defined by sidewalls that extend on a generally redial direction, the radial plenum being in direct fluid communication with the first and second sides, wherein the radial plenum engages the first and second sides adjacent the wall of the venturi; and a compressed air flow source in fluid communication with the first and second sides of the internal passageway, via the radial plenum, and wherein the compressed air from the compressed air flow source is directed through the venturi passageway in opposite directions within the first and second sides for cooling the venturi. 8. The combustor of claim 7, wherein the radial plenum communicates with either the first or second side of the interval passageway at a position offset from the apex of the venturi within the combustor. 9. The combustor of claim 7 further comprising a secondary passageway communicating with a downstream end of the second side of the internal passageway, wherein the air flow moving through the second side of the internal passageway into the secondary passageway is reversed in direction and directed towards the first side of the of the venturi. 10. The combustor of claim 9 further comprising a cooling air exit positioned at an end of the first side of the internal passageway for directing the cooling air into the first end of the combustor. 11. The combustor of claim 10 wherein the secondary passageway and the first side of the internal passageway are each in fluid communication with the cooling air exit. 12. The combustor of claim 11 wherein the cooling air exit directs the air flow from the secondary passageway and the first side of the internal passageway into the first end of the combustor, upstream of the venturi. 13. A venturi within a gas turbine combustor comprising: a venturi wall and a radially outer venturi wall extending along an interior surface of the combustor and defining a first and second passageway; an upstream angled side, a downstream angled side, an apex positioned between the upstream and downstream sides and a cooling air inlet extending radially inward towards the venturi wall and defined by sidewalls that extend in a generally radial direction, are connected to the radially outer venturi wall, and located between the angled sides for supplying cooling air proximate the apex; the first passageway directing cooling air from the cooling air inlet along inner surface of downstream angled side and then upstream thereof along a liner; the second passageway directing cooling air from the cooling air inlet along upstream angled side; and a cooling discharge directing cooling air from the second passageway into combustor, upstream of the apex of the venturi. 14. The venturi of claim 13 wherein the cooling air inlet comprises a central plenum extending radially around the combustor, within the venturi. 15. The venturi of claim 13 wherein the cooling discharge is positioned upstream of the upstream angled side of the venturi.