72652 ⎘
Aircraft indicators or protectors not otherwise provided for; Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection
FAILURE DETECTION AND/OR HEALTH MONITORING SYSTEM FOR A HIGH LIFT SYSTEM OF AN AIRCRAFT, AND METHOD
#2SYSTEM AND METHOD FOR MONITORING AND/OR DETECTING AN OPERATIONAL STATE OF A MOVABLE COMPONENT OF AN AIRCRAFT
#3MONITORING ADAPTABLE SEGMENTS OF AN AIRFOIL
#4SYSTEM AND METHOD FOR DETECTING THE POSITION AND/OR THE OPERATING STATE OF A MOVABLE COMPONENT OF AN AIRCRAFT
#5HIGH LIFT SKEW SYSTEM
#6Systems and methods for detecting a jam of a flap of a wing of an aircraft
#7Drive system with integrated torque sensing device
#8Aircraft control surface element monitoring system
#9Control surface element skew and/or loss detection system
#10Aircraft uplock
#11Dynamic no-back brake having a damping element
#12AIRCRAFT SKEW DETECTION SYSTEM AND METHOD OF OPERATING THE SAME
#13Distributed linear hydraulic high lift actuation system with synchronization members
#14Methods and apparatus for a distributed aircraft actuation system
#15Variable camber system
#16Flight control surface assembly
#17Distributed trailing edge wing flap systems
#18Proportional control brake
#19Flight control surface assembly
#20Slat skew detection system and method
#21Methods and apparatus for a distributed aircraft actuation system
#22Methods and apparatus for operating flight control systems of aircrafts
#23Methods and apparatus for detecting airflow control surface skew conditions
#24Wing slat actuator disconnection detection
#25Aircraft wing flap skew detection systems and methods
#26Slat disconnect sensor
#27ELECTRICAL ARCHITECTURE FOR SLAT/FLAP CONTROL USING SMART SENSORS AND EFFECTORS
#28System and method for controlling aircraft wing flap motion
#29Aerodynamic control surface movement monitoring system
#30Integrated torque limiter/no-back device
#31Aircraft flight control surface actuation monitoring system and method
#32Monitoring component asymmetry
#33Differential motion sensor
#34FIBER OPTIC SENSING AND CONTROL SYSTEM
#35Methods and apparatus for operating flight control systems of aircrafts
#36System and method for angle of attack indication with no dedicated sensors and aircraft information
#37Aircraft wing slat skew detection systems and methods
#38Motionless flight control surface skew detection system
#39Sensor system for a wing panel assembly and method of monitoring a wing panel assembly
#40Method for adjusting the play in a high-lift system of an aircraft
#41Method for determining a state of a component in a high lift system of an aircraft, high lift system of an aircraft, and aircraft having such a high lift system
#42Methods and apparatus for operating flight control systems of aircrafts
#43Differential motion sensor
#44High lift control method and system for aircraft
#45Skew sensing arrangement
#46High lift system for an aircraft, aircraft having a wing and a high lift system and method for moving a high lift surface relative to the wing of an aircraft
#47Method for determining the position of a component in a high lift system of an aircraft, high lift system of an aircraft and aircraft
#48Aircraft wing and an aircraft comprising such aircraft wing
#49Monitoring of high-lift systems for aircraft
#50Control surface skew detection systems
#51Flap system for an aircraft high lift system or an engine actuation and method for monitoring a flap system
#52Actuation system for flight control surface
#53Drive system for a high lift system of an aircraft and method for detecting a misalignment between a transmission shaft and an opening in a drive system for a high lift system of an aircraft
#54Method for diagnosing a trailing edge flap fault
#55Monitoring of high-lift systems for aircraft
#56Method for predicting a trailing edge flap fault
#57High lift system for an aircraft with two separate drive units
#58Method of operating actuators simultaneously for moving aircraft flaps, an aircraft flap drive device, and an aircraft provided with such a device
#59Device for an adjustable flap of a wing
#60Integrated torque limiter/no-back device
#61System for detecting misalignment of an aero surface
#62Connecting rod for aeronautical mechanism and aeronautical mechanism comprising such a connecting rod
#63High-lift system for a wing of an aircraft
#64Adjustment system of an aeroplane with an adjustable flap
#65Deployment system
#66Control surface element skew and / or loss detection system
#67ELECTRONICALLY SYNCHRONIZED FLAP SYSTEM
#68Slat monitoring system
#69Flap adjusting system of an aircraft with a regulating flap
#70Resolver type skew sensor with gimbal attachment
#71Aircraft having a vertical lift system
#72Cantilevered differential motion sensor and associated frame
#73High lift system for an aircraft and method for detecting faults in a high lift system for an aircraft
#74Skew detection
#75ADJUSTER 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
#76Aircraft slat disconnect sensor
#77Aircraft control surface methods
#78Fault-tolerant actuating system for adjusting flaps of an aircraft, comprising adjustment kinematics with a fixed pivot, and a method for monitoring an actuating system
#79Aircraft high lift system and method for determining an operating condition of an aircraft high lift system
#80Systems and methods for controlling aircraft flaps and spoilers
#81System for actuating at least one positioning flap of an aircraft and a method for monitoring the system
#82Slat skew detection system
#83Shuttle stop force limiter
#84Flap malfunction detection system
#85In-flight detection of wing flap free wheeling skew
#86Aircraft flight control actuation system with direct acting, force limiting, actuator
#87Sensor system for monitoring the synchronism of control surfaces of an aircraft
#88Airfoil for an aircraft and aircraft
#89High gain asymmetry brake
#90Aircraft control surface drive system and associated methods
#91Variable speed flap retraction and notification
#92Disconnect sensor
#93Device for error detection of adjustable flaps
#94Actuator and flap arrangement with actuator interconnection
#95Interconnecting strut for arranging between adjacent landing flaps of an aircraft
#96Drive system for a variable camber aircraft wing
#97Device for monitoring the synchronism of flaps of an aircraft wing
#98Landing flap drive system
#99EGPWS flap position enhancement
#100EGPWS FLAP POSITION ENHANCEMENT
#101Method for load limiting in drive systems for aircraft high lift systems
#102Device for detecting synchronous errors of high-lift surfaces on aircraft
#103Systems and methods for controlling aircraft flaps and spoilers
#104Device for monitoring tiltable flaps on aircraft wings
#105Apparatus for monitoring an aircraft flap and application of a dynamometric rod
#106Apparatus for driving and adjusting flaps hinged to an aircraft
#107Adaptive flap and slat drive system for aircraft
#108Aircraft control surface drive system and associated methods
#109Aircraft flap or slat drive system with redundant drives and shaft drive lines
#110Automated flight control functional testing