Electro-hydrostatic actuation system for a thrust reverser for an aircraft turbojet engine nacelle (US Patent 12338780)

Patent number: 12338780 Cited as: US 12,338,780 B2; US12338780B2; US12338780 Kind code: B2 Granted: 2025-06-24 Filed: 2022-04-11 Inventors: Jean-Baptiste Kamis (Moissy-Cramayel, FR) Assignees: SAFRAN LANDING SYSTEMS (Velizy-Villacoublay, FR) CPC: B01D 61/10; F01B 25/04; F01D 17/20; F02K 1/58; F02K 1/76; F02K 1/763; F02K 1/766; F05D 2260/406; F15B 11/22; F15B 13/023; F15B 15/18; F15B 20/00; F15B 2211/20515; F15B 2211/20561; F15B 2211/40523; F15B 2211/426; F15B 2211/428;