Inventor
BRUNET ANTOINE ROBERT ALAIN
FR20 patents
⚠️ This page may combine multiple inventors who share the name “BRUNET ANTOINE ROBERT ALAIN”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
SAFRAN AIRCRAFT ENGINES
9 patentsUS10738650B2Aug 11, 2020
Device for deicing a splitter nose and inlet guide vanes of an aviation turbine engine
SAFRAN AIRCRAFT ENGINES3 citations66
US11585230B2Feb 21, 2023
Assembly for a turbomachine
SAFRAN AIRCRAFT ENGINES2 citations65
US12196504B2Jan 14, 2025
Heat exchanger comprising a baffle wall with hollow turbulence generators
SAFRAN AIRCRAFT ENGINES0 citations59
US11753953B2Sep 12, 2023
Heat exchanger comprising an inter-vane wall provided with hollow turbulence generators
SAFRAN AIRCRAFT ENGINES0 citations59
US11225879B2Jan 18, 2022
Abradable turbomachine element provided with visual wear indicators
SAFRAN AIRCRAFT ENGINES0 citations54
US10975716B2Apr 13, 2021
Assembly forming a labyrinth seal for a turbomachine comprising an abradable material and inclined fins
SAFRAN AIRCRAFT ENGINES0 citations49
US10330117B2Jun 25, 2019
Angular stator sector for a turbomachine compressor comprising a brush seal
SAFRAN AIRCRAFT ENGINES0 citations35
US12031444B2Jul 9, 2024
Sealing assembly for a turbine engine
SAFRAN AIRCRAFT ENGINES0 citations34
US10683805B2Jun 16, 2020
Anti-icing system for a turbine engine vane
SAFRAN AIRCRAFT ENGINES0 citations29
SNECMA
6 patentsUS7937951B2May 10, 2011
System for cooling the impeller of a centrifugal compressor
SNECMA8 citations82
US8029238B2Oct 4, 2011
System for cooling a downstream cavity of a centrifugal compressor impeller
SNECMA9 citations80
US7942630B2May 17, 2011
System for ventilating a downstream cavity of an impellor of a centrifugal compressor
SNECMA8 citations80
US9879607B2Jan 30, 2018
Sealing of turbine engine enclosures produced by brush seal and labyrinth
SNECMA5 citations65
US7937944B2May 10, 2011
System for ventilating a combustion chamber wall
SNECMA3 citations62
US8052381B2Nov 8, 2011
Turbomachine module provided with a device to improve radial clearances
SNECMA3 citations54