Inventor

DE GAILLARD THOMAS ALAIN

FR28 patents

⚠️ This page may combine multiple inventors who share the name “DE GAILLARD THOMAS ALAIN”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

DE GAILLARD THOMAS ALAIN

SAFRAN AIRCRAFT ENGINES

Fibrous texture for turbine engine blade made of composite material

Fibrous texture for producing a fan blade made of composite material

Preform and one-piece vane for turbomachine

Blade equipped with platforms comprising a retaining leg

Blade comprising lands with a stiffener

Hybridization of fibers of the fibrous reinforcement of a fan blade

Blade body and a blade made of composite material having fiber reinforcement made up both of three-dimensional weaving and also of short fibers, and method of fabrication

Composite blade comprising a platform equipped with a stiffener

Hybridization of the fibers of the fibrous reinforcement of a fan blade with elastic fibers

Fabric comprising aramid fibres for protecting a blade against impacts

Fan blade comprising an insert of stiff fibers

Blade platform and a fan disk for an aviation turbine engine

Inter-blade platform with a sacrificial box section

Vane made of composite material having a three-dimensional woven fibrous reinforcement and two-dimensional woven skin and method for manufacturing same

Fan blade comprising a thin shield and a stiffener

Aviation turbine engine fan assembly including a fitted platform

Hybridization of the fibers of the fibrous reinforcement of a fan blade

Turbmachine fan disc

Turbomachine rotary-fan blade, fan and turbomachine provided therewith

Turbomachine rotary fan blade, fan, and turbomachine provided therewith

Sealing arrangement between two ring-shaped walls of an aircraft engine

Fairing ring for a bladed wheel

Rotary assembly of an aeronautical turbomachine comprising an added-on fan blade platform

Stiffened platform

Blade made of composite material with integrated platform for an aircraft turbine engine

Rotary assembly of a turbomachine equipped with an axial retention system of a blade

SNECMA

Blade provided with platforms possessing attachment portions

Rotary assembly for an aviation turbine engine, the assembly comprising a separate fan blade platform mounted on a fan disk