Aircraft Components TRIZ Cases

A lighter-than-air drone adjusts balloon volume to maintain altitude without constant motor operation.

Segmented modules with front-panel connectors improve ventilation and reduce wiring weight in aircraft cabinets.

A drone cable reel module uses multiple driving devices to manage cable extension and retraction.

Electronic device derives photography information from images to set unmanned aerial vehicle movement paths.

A UAV authorization management system cryptographically signs approved flight commands to verify operator authority levels.

A suspended load control system exerts dynamic thrust via electric ducted fans to stabilize cargo orientation.

Actuator linkage adjusts tether attachment point to reduce retraction energy requirements.

An integrated aircraft control unit consolidates communication, surveillance, navigation, and other systems into a single module with a display screen and user interface.

A UAV jettison apparatus uses a spring-loaded ejector plate to launch drones, reducing drag by keeping bomb bay doors closed during flight.

A UAV delivery structure uses a reset assembly to drive cargo release upon landing.

A platform integrates real-time and non-real-time information to calculate flight paths for unmanned aerial vehicles.

A radiofrequency tag reader detects configuration data from a frame-mounted tag, freeing connector pins for functional use.

Multi-modal UAV sensors replace manual inspections to resolve accessibility constraints and enable real-time insurance payouts.

Single-layer coiling around a rotating drum reduces aerodynamic interference and drag on aircraft refueling pods.

Segmented power and reservoir modules enable automated exchange at a charging station, eliminating manual refilling downtime.

Infrared imaging units detect adverse airborne phenomena to prevent flight risks and fuel waste.

A steerable drogue twists support arms via a control ring to generate directional aerodynamic force, resolving probe alignment complexity in refueling systems.

Multidirectional mini turbines enable rapid aerial deployment, bypassing ground barriers to deliver critical incident data.

Continuous ground monitoring updates flight parameters to resolve dynamic drop zone targeting challenges during cargo airdrops.

Multiple storage reservoirs collect rainwater to refill primary tanks, extending wildfire suppression duration without relying on municipal sources.

An unmanned aerial vehicle holding member releases a lifebuoy via support arms, bypassing slow boat-based rescue operations.

Autonomous UAVs navigate fog banks using image detection to harvest moisture without obstructing land use.

A UAV-mounted LED matrix enables omnidirectional light shows by synchronizing flight and lighting programs to minimize power consumption.

A magnetometer calibration system adapts rotation paths based on magnetic inclination to ensure accurate orientation determination.

A status indicating light unit conveys operational data via pulsed power draw patterns to the external supply.

An unmanned aerial vehicle monitors electrical outlets to detect energy consumption and environmental conditions.

A hoist cable sensor uses a differential drive mechanism with coaxial ring gears to track deployment length via a single-turn transducer.

An extendible tubular member and floater allow non-amphibious aircraft to scoop large water volumes from surfaces, eliminating airport refills.

A drone-based system delivers tools and tailored instructions to users during object assembly.

Buoyant lift from a gas chamber enables a transport aircraft to deploy unmanned aerial systems in flight, reducing delivery time and costs.

A display management system synthesizes multiple camera images to create a clear, unobstructed view of the aircraft surroundings on the cockpit screen.

Removable sizing sections on a flexible kite canopy reduce equipment complexity and safety risks from wind speed variations.

Calculates true airspeed and Mach number via GPS, IRS, and radio altimeter data to replace unreliable pitot static sensor readings.

Onboard carriage avionics consolidate control signals through one MIL-STD-1760 connection, eliminating costly aircraft wiring modifications.

Acoustic sensors replace pneumatic couplings to measure angle-of-attack and sideslip, eliminating icing susceptibility and common-mode errors.

Transversely hinged jaws maintain drill bit perpendicularity to prevent chipping and delamination in thin composite aerospace parts.

Calculates aircraft angle of attack and sideslip by analyzing leading edge temperature distributions, avoiding external sensor damage from ice or debris.

RAAS processor merges flight plan data with ground proximity signals to generate precise runway advisories.

A UARV mounting mechanism secures the vehicle to objects using grip arms and clamps.

A non-cylindrical pressure vessel uses Kevlar and carbon fiber strands wrapped through shell tubes to contain high-pressure gas.

Offset conduits and capillary bulkheads prevent particle ingestion and moisture accumulation, reducing measurement errors in air data probes.

Segmented sensors attached to individual plants measure localized water usage and microclimate data, reducing waste through precise monitoring.

A three-dimensional curved display surface extends laterally to increase information area while maintaining unobstructed pilot visibility.

Control unit detects screen failure and reconfigures cockpit displays to ensure immediate access to critical flight information.