초록 ▼

A plurality of circumferentially spaced props are attached to the outer overlapping segments of a combustor liner to prevent the thermal outward growth of the inner segment. Placement of the props on the outer segment allows them to remain relatively cool to thereby minimize stresses and, when combi

A plurality of circumferentially spaced props are attached to the outer overlapping segments of a combustor liner to prevent the thermal outward growth of the inner segment. Placement of the props on the outer segment allows them to remain relatively cool to thereby minimize stresses and, when combined with a liner design which centrifuges the cooling air to the radially inner side of the cooling slot, such placement coincides with a separation bubble so as to minimize flow blockage and resulting hot streaks.

대표청구항 ▼

An improved combustor liner structure of the type having overlapping portions of telescoping outer and inner liner segments which together define an annular gap and means for transferring a cooling fluid from an outer plenum to flow through the annular gap for attachment to the inner surface of the

An improved combustor liner structure of the type having overlapping portions of telescoping outer and inner liner segments which together define an annular gap and means for transferring a cooling fluid from an outer plenum to flow through the annular gap for attachment to the inner surface of the outer liner segment downstream of said annular gap as a protective film barrier, wherein the improvement comprises: (a) an annular enlargement section interconnecting the outer surfaces of said outer and inner liner segments and defining with the upstream end of said outer liner segment and the downstream end of said inner liner segment a chamber which fluidly communicates with the annular gap by way of a curvilinear surface adjacent the upstream end of said annular enlargement section; (b) aperture means in the downstream side of said annular enlargement section for introducing the flow of cooling air into said chamber where it is then centrifuged radially inward by said curvilinear surface to pass through the radially inward side of said annular gap before attaching to the inner surface of the outer liner segment; and (c) a plurality of circumferentially spaced props attached to the inner surface of the upstream end of the outer liner segment and disposed in the radially outer side of said annular gap for thereby restricting the outward thermal growth of the downstream end of the inner liner segment, said props being elongated in the downstream direction and having tapered downstream ends for thereby facilitating attachment of said cooling air to said inner surface of said outer liner segment.