Flow redirector for compressor inlet

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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F02C 7/04 (2006.01) F15D 1/02 (2006.01)

Patent

CA 2570467

A flow redirector (10) for channeling flow from an upstream source to a compressor has a circular inlet (20) located on its upstream end. The inlet (20) is disposed off of the main axis (55) of the compressor. The compressor is configured to receive annular shaped, axial flow from the flow redirector (10). The flow redirector (10) channels the flow from the off-axis circular inlet (20) to an annular shaped outlet (30) disposed about the axis (55) of the compressor. The flow redirector (10) has a generally symmetrical and converging cross section.

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