|
CN105190365A
|
|
Proximity sensor
|
|
US2014210647A1
|
|
Switch assembly and over-steer detection system
|
|
US2014208935A1
|
|
Locking mechanism for locking an actuator
|
|
WO2013075210A1
|
|
Landing gear shock absorber metering using pivoting joint
|
|
CA2767791A1
|
|
Positoning tool, specificallly for the extremity of a sliding rod or a landing gear housing on an aircraft
|
|
CA2759570A1
|
|
Landing gear shock absorber metering using pivoting joint
|
|
WO2012061921A1
|
|
Rotary machine tool with telescopic arms
|
|
CA2711199A1
|
|
Hydraulic shimmy damper for aircraft landing gear
|
|
KR20120112509A
|
|
Electric accumulator utilizing an ultra-capacitor array
|
|
KR20110091538A
|
|
Landing gear bay door with double hook mechanism
|
|
CA2710202A1
|
|
Landing gear uplock mechanism employing thermal phase-change actuation
|
|
BRPI0807122A2
|
|
SELF-LUBRICATING PIN DEVICE
|
|
BRPI0715524A2
|
|
hydraulic / pneumatic loading valve with integrated pressure transducer
|
|
CA2610835A1
|
|
System and method for determining aircraft hard landing events from inertial and aircraft reference frame data
|
|
BRPI0518305A2
|
|
Method and system for monitoring the operating conditions of an aircraft's landing gear
|
|
CA2587750A1
|
|
Method and system for health monitoring of aircraft landing gear
|
|
EP1784577A1
|
|
Lock sensor for an internally locking actuator
|
|
CA2576805A1
|
|
Structural deflection and load measuring device
|
|
CA2576801A1
|
|
Lock sensor for an internally locking actuator
|
|
CA2509742A1
|
|
System and method for determining aircraft hard landing events from inertial and aircraft reference frame data
|
