Autobraking interlock for an aircraft electric brake system
作者： David T. Yamamoto , Andreea D. Uta , T. Todd Griffith
DOI:
关键词: Automotive engineering 、 Control engineering 、 Power (physics) 、 Actuator 、 Interlock 、 Brake 、 Mechanism (engineering) 、 Engineering
摘要: An electric autobrake interlock system for an aircraft includes power mechanism that prevents inadvertent (uncommanded) application of brakes. The removes operating from the brake actuators whenever actuation data does not indicate a legitimate condition. processing occurs in parallel with command such even if is generated, will be unable to act upon command. In this regard, are apply brakes automatically unless following two actions happen concurrently: provided enable and control commanded response
lens.org 参考文章(14)
James L. Hill, Lee E. McFarland, Fail safe electrical brake control system for aircraft ,(1999)
Johan N Hopland, Sherman M Bissell, Rejected take-off (RTO) control for automatic braking system ,(1974)
Ervin Gordon Romero, Aircraft automatic braking system ,(1975)
Garrett Howard DeVlieg, Aircraft automatic braking system ,(1974)
Mihai Ralea, Electric brake position and force sensing and control ,(2005)
Gunsang Lim, Ben Khoshnood, Richard D. Marowsky, Electrical connector having reduced cross-talk ,(1994)
Stephen A. Mascarella, Robert L. Brundrett, Franklin C. Christ, Lawrence F. Corio, Aircraft brake and method with electromechanical actuator modules ,(1998)
Bijan Salamat, Robert F. Mackness, Dual redundant active/active brake-by-wire architecture ,(1999)
John M. Redfield, Cliff R. Curry, Communication connector with inductive compensation ,(2001)
Luc Adriaenssens, Troy Long, Amid Hashim, Near-end crosstalk compensation at multi-stages ,(2004)