Launching/Towing Gear TRIZ Cases

See how a guided transfer device with adjustable lifting and gripper mechanisms prevents fragil

See how an unmanned transport device pairs with a receiving container using geocoordinates and

See how a window-mounted landing pad with trapdoor and lockable compartment reduces package the

See how unmanned transport devices pair with receiving containers using authorization codes to

A container-integrated transfer mechanism guides lowering and lifting from unmanned transport devices to prevent fragile shipment damage.

Movable legs retract for compact storage and deploy wheels for smooth flight vehicle transfer across floor-to-ground level differences.

A movable elevated ring with wind generators turns takeoff airflow into power, helping compact UAM vertiports reduce grid dependence.

A pivoting launch frame lets a towed aircraft weathervane into the wind while yaw damping preserves stability for smoother UAV takeoff.

Processor-built carrier segments let UAVs ride, recharge, and switch vehicles to cut flight time while keeping battery charge above target.

A window-mounted pad guides drones by RF signal and drops parcels into a locked compartment to reduce theft in dense urban delivery.

Tilting the rotor axis lets this convertible drone steer horizontally in rotary-wing flight without complex cyclic-pitch control.

A sensor-guided towbar interface steers nose landing gear from towbar position, enabling standard towing of aircraft with difficult gear geometry.

A weighted pivoting lever and modular base arms enable uniform jettisoning of multiple aerial objects without excessive launch structure complexity.

A dual signal path powers onboard electronics before squib firing, enabling launch telemetry and guidance without added hardware.

A gas generator drives a sabot through the launch tube while a clasp maintains detachable UAV coupling for rapid, controlled launch.

A gas-driven sabot uses an expandable skirt and rotationally constrained clasp to secure and rapidly eject a UAV from its launch tube.

A drone delivery hub uses elevated linking conveyors to transport unmanned aerial vehicles between structural arms for autonomous parcel handling.

Replacing hydraulic lag, electromotor winches maintain cable tension below maximum load limits during rapid sea state changes.

Multiple tow vehicles couple to main landing gear wheels to propel aircraft forward with independent synchronized propulsion.

Automatic steering control switches to free orientation mode during towing operations.

Front-facing operator cab and computer-controlled transmission resolve mechanical complexity while maintaining roadworthiness.

Magnetic studs secure the drone without power, while a scissor lift automates deployment.

An automatic umbilical connector separating mechanism aligns male and female connectors parallel to the flight path using tension springs and guide pins.

Rotary tube catapult system uses automatic loading mechanism for continuous unmanned aerial vehicle launching.

Conductive roadway surface imparts forward, lateral, and levitation forces on vehicles via electromagnetic induction.

Segmented tread sections with dynamic pivot joints navigate uneven topography in confined aircraft bays, eliminating large access ports.

A surface vehicle tows a UAV using a towline with resilient sections, eliminating bulky guide systems and reducing energy consumption.

Modular rail sections and adjustable power variance enable portable, lightweight UAV launching without bulky pneumatic systems.

Segmented motors and real-time feedback resolve the contradiction between device complexity and manufacturing precision in airborne payload retrieval.

An electromagnetic catapult accelerates aircraft via a maglev sled, reducing runway length requirements and airport land constraints.

A ground handling facility moves aircraft between landing and takeoff platforms using a dedicated conveying device.

External lifting converts energy to potential energy, reducing UAV power consumption while increasing payload capacity.

Projecting capturing element engages oleo shock absorber to automate towing, reducing taxi cycle time when wheels are covered by aerodynamic fairings.

A surveillance vehicle launches from a mortar tube and deploys a parasail to gather visual intelligence.

Carrier vehicle propels payload to altitude using solid rocket propulsion, resolving climb rate versus cruise efficiency trade-offs.

A drone launching mechanism uses a pressure generator to axially displace a dynamic element, propelling the drone out of its container.

Ground-based electromagnetic catapult accelerates aircraft using a magnetic sled, reducing runway length requirements and airport land constraints.

Collet shaft release mechanism connects aircraft to runway rod via electric actuation for controlled takeoff restraint.

Nested sliding frames extend the launch stroke to reduce UAV acceleration loads while keeping the base frame compact for transport.

Rotary-wing reflectors use aerodynamic lift to position ultralight sheets in the upper atmosphere, avoiding high deployment costs of space-based systems.

Vertical pneumatic launch enables stealthy UAV deployment at periscope depth without surfacing the submarine.

Angular sensors measure steering angle and transmit data to a controller for real-time tracking.

Dual towing slings connect to main landing gears and drive a lateral direction control member on the front gear for automatic steering.

Pivoting wheel constraint mechanism confines aircraft wheels on a base plate, eliminating manual attachment complexity.

Capture mechanism with deployable flaps engages a near-vertical towline to secure an unmanned aerial vehicle during mid-air recovery.

Segmented constraint ropes release sequentially to reduce launch impact and improve flight control.

An electric motor drives a tape to launch UAVs, eliminating heavy hydraulic systems and nitrogen pre-charging requirements.

Removable adapter assemblies interface with launcher carriages to propel unmanned aerial vehicles without runways.

Powered track assemblies enable lateral helicopter movement without initializing the drive system, resolving cumbersome manual tugging in confined hangars.

A towline system with a weighted section and drogue enables mid-air retrieval of unmanned aerial vehicles.

A fuselage cavity release mechanism uses a pressurized gas pin to deploy air vehicle fins after launcher exit, preventing premature contact with rifled walls.

An electric motor drives a tape to propel a shuttle along a launcher rail for unmanned aerial vehicle deployment.

An elastic effective member automatically varies the radius of rotation during launch, improving lift generation without adding complex control mechanisms.

Multi-rail UAV catapult launcher partitions overall force across independent rails to eliminate launch misalignment and hysteresis issues.

A microcontroller unit automates UAV winch activation by monitoring battery voltage and towline encoder data.