Abstract: The present disclosure is directed to a combustor having an annularly shaped liner that at least partially defines a hot gas path of the combustor. A flow sleeve circumferentially surrounds at least a portion of the liner. The flow sleeve is radially spaced from the liner to form a cooling flow annulus therebetween. A bluff body extends radially between the flow sleeve and the liner through the cooling flow annulus. A guide vane is disposed within the cooling flow annulus and extends between the flow sleeve and the liner proximate to the bluff body.

Abstract: The present disclosure is directed a combustor. The combustor includes an annularly shaped liner having a downstream end that is rigidly connected to an aft frame. A flow sleeve circumferentially surrounds at least a portion of the liner and is radially spaced from the liner to form a cooling flow annulus therebetween. A plurality of fuel injector assemblies is circumferentially spaced about the flow sleeve. Each fuel injector assembly extends radially through the flow sleeve and the liner. Each fuel injector assembly is rigidly connected to the flow sleeve and to the liner. An aft portion of the flow sleeve terminates axially short of the aft frame to form an axial gap between the aft end and the aft frame to allow for unrestrained axial expansion and contraction of the aft end.

Abstract: The present disclosure is directed to a combustor having an annularly shaped liner that at least partially defines a hot gas path of the combustor. A flow sleeve circumferentially surrounds at least a portion of the liner. The flow sleeve is radially spaced from the liner to form a cooling flow annulus therebetween. A bluff body extends radially between the flow sleeve and the liner through the cooling flow annulus. A guide vane is disposed within the cooling flow annulus and extends between the flow sleeve and the liner proximate to the bluff body.