P

Assignee

OROSA JOHN

US3 patents

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US8147207B2Apr 3, 2012

Compressor blade having a ratio of leading edge sweep to leading edge dihedral in a range of 1:1 to 3:1 along the radially outer portion

OROSA JOHN63 citations95
US8668449B2Mar 11, 2014

Turbine exhaust diffuser with region of reduced flow area and outer boundary gas flow

OROSA JOHN4 citations69
US8647057B2Feb 11, 2014

Turbine exhaust diffuser with a gas jet producing a coanda effect flow control

OROSA JOHN3 citations60