Safran Aircraft Engines

Gérald Diogo

Jérémy Guivarc'h

Thibault Ruf

Jean-Louis Romero

Alain Jacques Michel Bassot

The invention relates to the field of turbomachine blades, and more specifically to a leading-edge shield () for a turbomachine blade (), said leading-edge shield () having a pressure-side wing () and a suction-side wing (), each extending along a height and along a length, the wings being connected together over their height, the pressure-side wing () presenting a greater length than the suction-side wing () over a first segment (S) of the leading-edge shield (), and an equal or smaller length than the suction-side wing () over a second segment (S) of the leading-edge shield ().

Growing community of inventors

Moissy-Cramayel, France

Gérald Diogo