Brake Regulators TRIZ Cases
- Coordinated Nose and Main Wheel Steering for Tighter Aircraft Taxi Turns
Coordinated nose and main wheel steering with sliding mode control cuts aircraft taxi turning radius and runway space use.
- Locked Wheel Protection with Paired Brake Pressure Yaw Control
During hydroplaning, paired brake pressure modulation releases the locked wheel and trims the opposite brake to reduce aircraft yaw.
- Aircraft Emergency Braking Control for Runway-Adaptive Force Limits
A controller sets emergency brake force from aircraft and runway conditions to limit skidding and tyre bursts during landing.
- Synchronous Subsampling Circuit for Precise Wheel Speed Sensing
Synchronized excitation and subsampling measure wheel speed accurately while avoiding fast ADCs and heavy processing.
- Aircraft Emergency Braking Control for Tyre Skid Prevention
Dynamic emergency brake limits based on aircraft and runway conditions help prevent tyre skidding and bursts during landing.
- Aircraft Brake Pressure Balancing for Locked Wheel Yaw Control
When one aircraft wheel locks, paired-wheel brake pressure is reduced to balance braking forces and limit yaw during landing.
- Aircraft Brake Actuation Using Piezoelectric Anti-Skid Modulation
A series piezoelectric actuator modulates aircraft brake pressure faster than hydraulics alone, cutting energy loss and wear in anti-skid braking.
- Aircraft Anti-Lock Braking With Hybrid Piezoelectric Pressure Control
A hybrid actuator pairs conventional brake stroke with piezoelectric pressure modulation for faster aircraft anti-skid response and lower wear.
- Dump Valve Brake Architecture for Aircraft Antiskid Pressure Release
A parallel dump valve gives aircraft brakes a direct hydraulic release path, cutting wheel lockup response time while preserving servo-valve control.
- Electric Nose Landing Gear Actuation Without Central Hydraulics
Distributed electro-hydraulic and electro-mechanical actuators cut hydraulic tubing, fluid weight, and maintenance in nose landing gear.
- Electric Nose Landing Gear Layout for Low-Fluid Actuation
Localized electro-hydraulic and electro-mechanical actuators reduce hydraulic fluid, aircraft weight, and leak-prone nose gear maintenance.
- Emergency Autoland Braking With Single-Actuator Cable Calibration
A single actuator and calibrated brake cables simplify emergency autoland braking while balancing wheel pressure and preserving pilot input.
- Aircraft Deceleration Feedback Algorithm Maintains Brake Pressure
Deceleration feedback algorithm maintains minimum brake pressure demand during aircraft braking operations.
- Adaptive Noise Thresholds for Aircraft Antiskid Control
Dynamic noise thresholds adjust braking pressure based on wheel speed, preventing false antiskid activations from electrical interference.
- Electromechanical Braking Controller Anti-Slip Integration
Controller merges anti-slip protection into actuator management, eliminating redundant brake control units and data concentrators.
- Steerable Axle Landing Gear One-Way Castoring Lock
Deformable telescopic strut automatically locks pivotable bogie axle in landing position, eliminating complex angular positioning mechanisms.
- Aircraft Lateral Steering via Automatic Differential Braking
Automatic braking system distributes symmetrical values as differential forces between main landing gear wheels to generate yaw moments for ground steering.
- Aircraft Brake Update Rate Detection System
Force command update rate detection identifies brake signal frequencies using parallel variation and similarity detectors.
- Aircraft Brake Proportioning for Yaw Torque and Wear
Segments brake systems into independent groups to optimize yaw torque and deceleration while minimizing wear under adverse conditions.
- Aircraft Brake Control System Friction Mapping
Brake control system estimates tire runway friction using wheel speed and location data to reduce stop distances on varying surfaces.