EP 2353951 B8 20160224 - Aircraft electric brake actuation system and method
Title (en)
Aircraft electric brake actuation system and method
Title (de)
Elektrisches Flugzeugbremsenbetätigungssystem und -verfahren
Title (fr)
Système électrique d'actionnement du frein d'un avion et procédé
Publication
Application
Priority
US 69308810 A 20100125
Abstract (en)
[origin: EP2353951A1] Aircraft brakes in an aircraft that includes a brake pedal and an electric brake actuator are controlled by at least determining an aircraft operational state and determining an application force that is supplied to the brake pedal. When the determined aircraft operational state is a ground-idle state and the determined application force is greater than a set force magnitude, an actuator brake is moved to engage the electric brake actuator and the electric brake actuator is de-energized.
IPC 8 full level
B60T 8/17 (2006.01); B60T 13/74 (2006.01)
CPC (source: EP US)
B60T 8/1703 (2013.01 - EP US); B60T 13/741 (2013.01 - EP US); B64C 25/44 (2013.01 - US)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
EP 2353951 A1 20110810; EP 2353951 B1 20151125; EP 2353951 B8 20160224; US 2013297101 A1 20131107; US 9440735 B2 20160913
DOCDB simple family (application)
EP 11150347 A 20110106; US 69308810 A 20100125