EP 2349833 A2 20110803 - ADJUSTER DEVICE FOR AN AIRCRAFT COMBINATION OF AN ADJUSTER DEVICE AND AN ADJUSTER DEVICE FAULT RECOGNITION FUNCTION, FAULT -TOLERANT ADJUSTER SYSTEM AND METHOD FOR RECONFIGURING THE ADJUSTER SYSTEM
Title (en)
ADJUSTER DEVICE FOR AN AIRCRAFT COMBINATION OF AN ADJUSTER DEVICE AND AN ADJUSTER DEVICE FAULT RECOGNITION FUNCTION, FAULT -TOLERANT ADJUSTER SYSTEM AND METHOD FOR RECONFIGURING THE ADJUSTER SYSTEM
Title (de)
VERSTELLVORRICHTUNG EINES FLUGZEUGS, KOMBINATION EINER VERSTELLVORRICHTUNG UND EINER VERSTELLVORRICHTUNGS-FEHLERERKENNUNGSFUNKTION, FEHLERTOLERANTES STELLSYSTEM UND VERFAHREN ZUR REKONFIGURATION DES STELLSYSTEMS
Title (fr)
DISPOSITIF DE RÉGLAGE POUR AÉRONEF, COMBINAISON D'UN DISPOSITIF DE RÉGLAGE ET D'UNE FONCTION DE DÉTECTION DES ERREURS D'UN DISPOSITIF DE RÉGLAGE, SYSTÈME DE RÉGLAGE À TOLÉRANCE D'ERREURS ET PROCÉDÉ DE RECONFIGURATION DU SYSTÈME DE RÉGLAGE
Publication
Application
Priority
- EP 2009007571 W 20091022
- DE 102008052754 A 20081022
- US 11448708 P 20081114
Abstract (en)
[origin: WO2010046111A2] Adjuster device (A11, A12, B11, B12, A21, A22, B21, B22) for coupling an adjuster flap (A1, A2; B1, B2) on an aircraft to an actuator (20), an adjuster mechanism (VK) for the kinematic coupling of the actuator (20) to the adjustment flap (A1, A2; B1, B2) and a gearbox (25), wherein the adjuster device (A11, A12, B11, B12, A21, A22, B21, B22) may be coupled to a control and monitoring device (5) for operation thereof, characterised in that the adjuster device comprises a first load sensor (S1; S11-a, S12-a, S21-a, S22-a), arranged at the input side (31) of the actuator (20) for recording the load occurring on the input side of the actuator (20) as a result of the operation of the adjustment flap (A1, A2; B1, B2), a second load sensor (S2; S11-b, S12-b, S21-b), arranged at the output side (32) of the actuator (20) for recording the load occurring on the output side (32) of the actuator (20) as a result of the operation of the adjustment flap (A1, A2; B1, B2), wherein the first load sensor (S1; S11-a, S12-a, S21-a, S22-a) and the second load sensor (S1; S11-b, S12-b, S21 -b, S22-b) are functionally connected to an adjuster device fault recognition function for receiving the sensor values delivered by the load sensors, in order to attribute a fault condition to the adjuster device and a combination of an adjuster device and an adjuster device fault recognition function, a fault-tolerant adjuster system and a method fro reconfiguring an adjuster system.
IPC 8 full level
B64C 13/38 (2006.01); B64D 45/00 (2006.01)
CPC (source: EP US)
B64D 45/0005 (2013.01 - EP US); B64D 2045/001 (2013.01 - EP US)
Citation (search report)
See references of WO 2010046111A2
Designated contracting state (EPC)
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 SE SI SK SM TR
DOCDB simple family (publication)
WO 2010046111 A2 20100429; WO 2010046111 A3 20100729; BR PI0919762 A2 20151208; CA 2741362 A1 20100429; CN 102196964 A 20110921; CN 102196964 B 20170118; DE 102008052754 A1 20100506; EP 2349833 A2 20110803; JP 2012506336 A 20120315; RU 2011120362 A 20121127; US 2011255968 A1 20111020
DOCDB simple family (application)
EP 2009007571 W 20091022; BR PI0919762 A 20091022; CA 2741362 A 20091022; CN 200980142191 A 20091022; DE 102008052754 A 20081022; EP 09740276 A 20091022; JP 2011532540 A 20091022; RU 2011120362 A 20091022; US 200913125381 A 20091022