Abstract A diffuser provides a transition from a centrifugal compressor to the annular combustion chamber of a gas turbine engine. The diffuser comprises a plurality of linear passages which gradually merge radially outward from a circular cross-section to an outlet having a near rectangular cross-section defined by two flat opposing parallel sides and two opposing curved sides. The two opposing curved sides produce a razor sharp trailing edge which maximizes the diffuser efficiency. The linearity of the diffuser passage allows the diffuser to be manufactured to close tolerances by electric discharge milling an annular plate in a manner which assures uniformity and consistency between diffusers. The near rectangular shape of the outlet of the diffuser passages optimizes flow distribution to the annular combustion chamber. A transition region and deswirler section downstream of the near rectangular outlet may be provided to match the diffuser flow path to the combustor geometry.
A diffuser for diffusing the accelerated gas flow from a relatively high pressure centrifugal compressor to an annular combustion chamber comprising: an annular housing circumscribing the centrifugal compressor; a plurality of passages spaced about the circumference of the housing and extending therethrough, each passage having a substantially linear center line; wherein the inlet to each of the passages is circular in cross-section and disposed to receive the accelerated gases exiting the centrifugal compressor and each of the passages gradually merge to a near retangular cross-section at its outlet which is defined by two float opposing axial spaced parallel sides and two opposing curved circumferential sides formed as arcs of a circle, such that the internal walls of the passages in proximity to the diffuser outlet are formed as two flat parallel walls and two opposed slightly curved walls with the curved walls being convex with respect to the passage center line; and wherein the curved walls terminate in a relatively sharp edges at the diffuser inlet and outlet.
Claim 2
Dependent Claim
168 words
A diffuser for diffusing the accelerated gas flow from a relatively high pressure centrifugal compressor to an annular combustion chamber comprising: an annular housing circumscribing the centrifugal compressor; a plurality of passages spaced about the circumference of the housing and extending therethrough, each passage having a substantially linear center line; wherein the inlet to each of the passages is circular in cross-section and disposed to receive the accelerated gases exiting the centrifugal compressor and each of the passages gradually merge to a near retangular cross-section at its outlet which is defined by two float opposing axial spaced parallel sides and two opposing curved circumferential sides formed as arcs of a circle, such that the internal walls of the passages in proximity to the diffuser outlet are formed as two flat parallel walls and two opposed slightly curved walls with the curved walls being convex with respect to the passage center line; and wherein the curved walls terminate in a relatively sharp edges at the diffuser inlet and outlet.