A staggered dual-latch unlock sequence uses door-position sensing to detect latch failure and improve landing gear door reliability.
A tension cord, dual springs, and a ball-ramp shunt detect high-lift surface skew with far fewer sensors while maintaining coverage.
A tension cord, opposing springs, and shunt actuator detect high-lift control surface skew with far fewer sensors and lower maintenance cost.
Frequency-domain analysis of boom sensor signals detects tanker boom connection in real time without contact sensors or operator judgment.
Sequentially unlocking dual landing gear door housings verifies lock integrity, detects failures in flight cycles, and supports maintenance alerts.
An automatic release pin drives a spring-loaded push pin and signal switch at the required cap angle, preventing premature flight activation.
Decoupling bay door opening from gear retraction enables earlier gear stowage to reduce drag while maintaining structural protection against damage.
A system compares altitude, distance to destination, and airspeed against thresholds to generate a landing scenario indication for timely gear deployment.
Sensor arrangement detects movable element presence in landing gear hook gap, preventing uncommanded movements from undetected uplock failures.
Integrating arms with the base eliminates separate springs and hinge pins, reducing assembly complexity and misassembly risks in aircraft motion sensors.
A hard landing indicator on aircraft torque links leaves a visual mark upon impact.