Aircraft Components TRIZ Cases

A rotatable fastener secures aircraft stores using dynamic orientation changes to minimize aerodynamic resistance during flight.

Movable screens push against particulate carriers to prevent clogging and ensure regular dispensing.

Primary flight display system scales secondary textual objects to larger font sizes than primary data.

A mounting device secures illuminated signs to junction boxes using integrated biasing elements that prevent sagging.

A replenishment planning device calculates optimal chemical refill points and times along unmanned helicopter flight routes.

An aerial-based fluid application system deposits oil onto elevated nests to reduce avian pest populations without lethal methods.

Automatic folding mechanism retracts aircraft attachment device to reduce aerodynamic drag and minimize crash damage risk.

Segmented housing and flyaway plates enable reusable actuation, eliminating refurbishment needs while reducing angular errors.

Isolation FETs electrically disconnect inactive driver circuits to prevent back biasing and premature failure in redundant avionics LCD systems.

Automated aerial sampling replaces manual labor to overcome imprecise visual identification and enable rapid ex-situ disease detection.

A clutch mechanism selectively engages a pecking mechanism in a micro-peck feed drill to control periodic retraction of the spindle.

A foldable flap unmanned aerial vehicle transforms shape for storage or flight while harvesting solar, electromagnetic, and thermal energy.

Segmented containers with localized weak seams enable precise altitude control, resolving the trade-off between high-altitude safety and accurate placement.

An ultrasonic anemometer uses a reflecting surface to bounce acoustic signals, enabling reliable flow speed measurement without Pitot tube obstructions.

A redundant flight control system uses a main unit on the unmanned aerial vehicle and a backup unit at the ground facility to manage airframe actuators.

A machine-learned operating system uses ML processors to identify operational parameters and determine program instruction modifications.

Concave walls inside the sealed cabin dampen severe water flow shaking during flight, enabling reliable rescue operations in convective weather.

Interactive electronic charts automate data transfer to avionics systems, eliminating manual entry errors and reducing pilot workload.

A detector captures images during controlled light illumination periods to identify objects using synchronized temporal emission patterns.

Aircraft canister housing integrates heat sink fins and a fan to dissipate thermal energy from processing modules.

A 3-axis gimbal uses common gears in driving units to minimize friction, reducing weight and cost for stable image capturing on small drones.

Mobile display screens translate within the instrument panel to eliminate external view obstruction while maintaining critical piloting information.

An automatic locking keeper control unit prevents dynamic rollout by mechanically securing the pivot connection against spring-loaded inadvertent release.

Longitudinal tubes route water from a modular tank to the aircraft rear door, resolving installation complexity and flow rate trade-offs.

A flight management system calculates target aircraft positions from altitude or time targets and displays travel distance to those coordinates.

A tow control handle uses sensors to enable hands-free unmanned aerial vehicle towing.

An autonomous drone camera eliminates blind spots and reduces equipment damage by flying above the forklift during load handling.

Segmented projectors converge beams to achieve high intensity without overheating the rotorcraft skin.

A prism disperses electromagnetic radiation across wavelengths to enable precise relative positioning between moving objects.

An adjustable helical capstan rope brake secures rope wraps via interlocking puck teeth, reducing supply losses during aerial payload delivery.

A laser air data sensor transmits beams through a fixed window oriented away from occupied vehicle areas.

An infrared vision system detects laser signatures to guide drilling, overcoming line-of-sight blockage by the drill head.

Thermal shells conduct heat from the gimbal assembly to an isothermal dome, replacing unpredictable convection cooling for stable temperature control.

A triangular seesaw hook apparatus balances multiple aerial loads using a self-locking latch and eye loop mechanism.

Segmented mounting structure and intermediary sealing ring resolve pressure sealing integrity issues while maintaining measurement precision.