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Franco Di Paola

Pratt & Whitney Canada

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Archive | 2002

Blade retention scheme using a retention tab

Franco Di Paola; Eugene Gekht

Archive | 2008

Blade retention system for use in a gas turbine engine

Eugene Gekht; Franco Di Paola

Archive | 2002

Sheet metal turbine or compressor static shroud

Eugene Gekht; Franco Di Paola

Archive | 2010

BLADE OUTER AIR SEAL ANTI-ROTATION

Franco Di Paola; Bruno Chatelois

Archive | 2010

BLADE OUTER AIR SEAL COOLING

Franco Di Paola; Kapila Jain

Archive | 2009

Gas turbine engine balancing

Bruno Chatelois; Franco Di Paola

Archive | 2009

TURBINE DISC AND RETAINING NUT ARRANGEMENT

Alain Carrieres; Franco Di Paola

Archive | 2010

HIGH PRESSURE TURBINE VANE COOLING HOLE DISTRUBUTION

Franco Di Paola; Larry Lebel; Francois Doyon

Archive | 2009

Sealing and cooling at the joint between shroud segments

Yves Martin; Franco Di Paola

Archive | 2014

GAS TURBINE ENGINE EXHAUST EJECTOR/MIXER

Franco Di Paola; Guy Lefebvre; Patrick L'esperance; Gabriel Emard-Parent

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