Compressor diffuser and diffuser pipes therefor
AssigneePratt & Whitney Canada Corp.
InventorsHien Duong, Jason Nichols
Life of this patent
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AssigneePratt & Whitney Canada Corp.
InventorsHien Duong, Jason Nichols
Estimating the term…
A diffuser for a compressor of a gas turbine engine is disclosed. The diffuser has a plurality of diffuser pipes circumferentially distributed about an axis of the compressor, each of the plurality of diffuser pipes extending from an inlet to an outlet and having a bend section between the inlet and the outlet, a low pressure side and an opposite high pressure side. A recirculation conduit defines a recirculation path from a first flow region to a second flow region in one or more of the plurality of the diffuser pipes, the first flow region having a greater static pressure than that of the second region, the recirculation conduit having a conduit inlet and a conduit outlet, at least the conduit outlet located within the low pressure side of one of the plurality of the diffuser pipes.
A diffuser for a compressor of a gas turbine engine, the diffuser comprising:
A diffuser pipe for a diffuser of a gas turbine engine compressor, the diffuser pipe comprising:
A diffuser for a compressor of a gas turbine engine, the diffuser comprising:
A diffuser for a compressor of a gas turbine engine, the diffuser comprising:
Dependencies are inferred from the claim text.