Conjoint Controls TRIZ Cases
- Brake Assembly with Independently Activated Actuators
A brake assembly uses independently activatable actuators to compress a friction stack for variable braking force.
- Aircraft RTA Control Adapting Parameters to Weather
Adapting arrival parameters via weather data resolves fuel inefficiency from fixed airspeeds in required time of arrival modes.
- Flying Body Control Apparatus for Dynamic Communication Capacity
A control apparatus selects and combines multiple flying bodies to form a unified system with increased communication capacity.
- Aircraft Rudder Control Mechanism with Movable Carriage
Segmented carriage assembly enables easy removal for repair while asymmetric linkages improve pedal response comfort.
- Fiber Optic Landing Gear Fire Detection and Fatigue Monitoring
Optical fiber loops transmit signals to monitor temperature and strain across aircraft landing gear zones.
- Flat Plate Airfoil Solar Aircraft Tow Configuration
A flat plate airfoil solar aircraft uses a towed platform design to optimize lift-to-drag ratios for efficient flight.
- Autothrottle Control System for Turbopropeller Aircraft
A digital autothrottle control system manages engine power requests and manual input positions through integrated actuators.
- Aircraft Braking Distributed Sensor Processor Wiring Reduction
Distributed sensor processor unit concentrates braking command signals from multiple sensors to generate a single brake control signal.