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Erwan Daniel Botrel

Snecma

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Archive | 2004

Cooling circuits for a gas turbine blade

Erwan Daniel Botrel; Patrice Eneau

Archive | 2000

Turbine vane with enhanced profile

Erwan Daniel Botrel; Christophe Germain Brisset; Bertrand Petot

Archive | 2007

Optimized aerodynamic profile for a turbine blade

Erwan Daniel Botrel; Grégory Lafarge; Philippe Picot

Archive | 2007

Turbomachine turbine ring sector

Erwan Daniel Botrel; Claire Dorin

Archive | 2009

COOLING OF THE TIP OF A BLADE

Erwan Daniel Botrel; Régis Grohens

Archive | 2007

Turbomachine turbine shroud sector

Erwan Daniel Botrel; Claire Dorin

Archive | 2004

Cooling circuit for a turbine blade

Erwan Daniel Botrel; Patrice Eneau

Archive | 2009

MEMBER FOR LOCKING RING SECTORS ON A TURBINE ENGINE CASING, INCLUDING RADIAL PASSAGES FOR GRIPPING SAME

Alain Dominique Gendraud; Erwan Daniel Botrel

Archive | 2000

Turbine blade with improved section

Erwan Daniel Botrel; Christophe Germain Brisset; Bertrand Petot

Archive | 2012

Gas turbine vane offset towards the lower surface of the head sections and with cooling channels

Régis Grohens; Erwan Daniel Botrel

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