Device for improved air and fuel distribution to a combustor
A flow conditioning device for a can annular gas turbine engine, including a plurality of flow elements disposed in a compressed air flow path leading to a combustor, configured such that relative adjustment of at least one flow directing element with respect to an adjacent flow directing element during operation of the gas turbine engine is effective to adjust a level of choking of the compressed air flow path.
1. A flow conditioning device for a can annular gas turbine engine, comprising:
a combustor;
a plurality of flow directing elements disposed in a compressed air flow path leading to said combustor;
said plurality of flow directing elements configured for relative adjustment of at least one flow directing element with respect to an adjacent flow directing element during operation of said can annular gas turbine engine effective to adjust a level of choking of the compressed air flow path;
a fuel injector associated with at least one of said plurality of flow directing elements,
wherein said relative adjustment of the at least one flow directing element comprises rotating at least one airfoil to open at a downstream end of a flow conditioning path, wherein the at least one airfoil comprises a fuel path leading to the fuel injector; and
wherein said plurality of flow directing elements comprise a plurality of airfoils establishing flow conditioning paths between respective airfoils, wherein said relative adjustment of said plurality of flow directing elements comprise moving at least one airfoil relative to an adjacent airfoil.
2. The flow conditioning device of claim 1 , configured such that adjustment of the at least one flow directing element during operation of the gas turbine engine is effective to increase a level of choking of the compressed air flow path without increasing a level of swirl in a compressed air flow through the compressed air flow path.
3. The flow conditioning device of claim 1 , wherein said plurality of flow directing elements are configured in a reduced-swirl configuration.
4. The flow conditioning device of claim 1 , wherein said plurality of airfoils are disposed circumferentially about a combustion assembly comprising the combustor and a transition duct.
5. The flow conditioning device of claim 1 , wherein said plurality of airfoils are disposed in a flow turning region of the compressed air flow path.
6. The flow conditioning device of claim 1 , further comprising an adjustment mechanism comprising a concentric ring secured to the at least one flow directing element such that circumferential motion of the concentric ring adjusts the at least one flow directing element.