Combustion chamber air inlet
A combustor assembly comprising a combustor liner having an opening and a combustor chute, which is formed of a sheet material which is bent to form the desired chute. The chute allows the passage of cooling and dilution air into the combustor.
1. A combustor assembly comprising:
a combustor liner having at least one opening therethrough, said combustor liner defining a space adapted for the combustion of a fuel; and
a portion of sheet material bent to form a chute enclosing a passageway, the chute having a first end with a plurality of discrete tabs protruding radially outward from the chute, and having a second end inserted through said opening of the combustor liner with the tabbed end outside the combustor liner and with the second end within the combustor liner such that the passageway provides for the passage of a fluid from outside the combustor liner into said space defined by the combustor liner.
2. A combustor assembly according to claim 1 , wherein at least one tab provided at the tabbed end of the chute is bent to be substantially normal to the chute, and is engaged with the combustor liner to orientate the chute in a preferred direction relative to the combustor liner.
3. A combustor assembly according to claim 2 , wherein the at least one tab is engaged into a receptacle formed in the combustor liner.
4. A combustor assembly according to claim 1 , wherein the chute includes at least one flap which is located within the combustor liner and is bent outward from the chute to secure the chute within the combustor assembly.
5. A combustor assembly according to claim 1 , wherein at least one cooling aperture is formed from the passageway through the chute for fluid passage to cool the combustor liner or member.
6. A combustor assembly comprising:
a combustor liner having at least one opening therethrough, said combustor liner defining a space adapted for the combustion of a fuel; and
a chute cut from a tube and having a first end with a plurality of discrete tabs protruding radially outward from the chute, said chute enclosing a passageway, the chute being inserted through said opening of the combustor liner with the tabbed end outside the combustor liner and with a second end within the combustor liner such that the passageway provides for the passage of a fluid from outside the combustor liner into said space defined by the combustor liner.
7. A combustor assembly according to claim 6 , wherein at least one tab provided at the tabbed end of the chute is bent to be substantially normal to the chute, and is engaged with the combustor liner to orientate the chute in a preferred direction within the combustor assembly.
8. A combustor assembly according to claim 7 , wherein the at least one tab is engaged into a receptacle formed in the combustor liner.
9. A combustor assembly according to claim 6 , wherein the chute includes at least one flap which is located within the combustor liner and is bent away from the passageway to secure the chute within the combustor assembly.
10. A combustor assembly according to claim 6 , wherein at least one cooling aperture is formed from the passageway through the chute for fluid passage to cool the combustor liner or chute.