Stowage Devices TRIZ Cases

A switchable gas spring and push-button lock cut manual closing force for aircraft storage compartments without electrical complexity.

A self-supporting hull with vertical connectors cuts overhead bin weight while simplifying aircraft installation and layout customization.

Ceiling-mounted flexible and rigid partitions isolate aircraft seats to contain respiratory droplets with minimal cabin layout disruption.

Adjustable support pairs form a triangular truss that bridges cabin tolerance gaps while keeping component mounting simple and stable.

A recessed upper corner lets the aircraft luggage door pivot into the bin, cutting aisle protrusion, noise, and mechanism complexity.

A universal strongback uses standardized couplings to fit different aircraft stowage bin sizes and shapes, cutting replacement time and part variety.

Standardized pivot couplings and latch strikes let one cabin strongback fit different stowage bins, reducing replacement time and part variety.

Pre-assembling lights and wiring on a chassis enables inspection before aircraft installation in confined cabin space.

Thin-walled hulls and separate vertical connectors reduce weight and installation complexity while maintaining structural integrity.

A simple pivoting mechanism with a spring and damper helps overhead compartments open in confined aircraft spaces without complex coupling gears.

Fully loaded aircraft stowage compartments demand high closing force; a push-button gas spring supplies assistance only when needed without electrical components.

Angled rails and eccentric bushes help adapt aircraft cabin connections to frame tolerances while distributing loads.

This case enlarges an aircraft bin opening by cutting the bucket and adding a new bullnose and hinge brackets.

Shaft bearing and guide element prevent cable damage from improper bending radii during luggage bin pivoting.

Spring resetting device reduces manual closing force by 72 Newtons for easier aircraft loading.

Storage compartment resonance behavior analysis determines object volume and distribution, resolving measurement precision limits in occupancy detection.

A pivoting aircraft storage compartment uses a selectively activated spiral spring to reduce manual closing effort without adding electrical system complexity.

A movable luggage compartment element pivots on a joint with a load-responsive force transmission element that adjusts its position to manage holding torque.

A pivoting luggage bin uses a cylindrical rear section to rotate and reveal storage space for diagonal suitcase placement.

A spring-loaded main pin extends automatically into aligned suspension eye lugs to secure overhead storage bins without tools.

Relocating baggage storage below the cabin floor preserves seat motion freedom while a displacement restriction prevents luggage loss.

Modular carrier elements with through holes allow maintenance access without removing piping or wiring from the ceiling structure.

A pivoting intermediate floor divides a vehicle cabin storage housing into upper and lower compartments for efficient luggage placement.

Segmented doors and dynamic floor lower access height to improve usability for shorter passengers.

Removable couplers on the section divider assembly attach to stowage bin fittings and fixed rails, enabling quick cabin reconfiguration without tools.

A movable seat pan retracts to expose a fixed additional luggage compartment, increasing storage capacity without adding structural complexity.

Protective panel displacement triggers proximity sensors to halt moveable assembly motion.

A swivel compartment housing uses a mechanical support force unit to pivot stowed goods, reducing manual closing effort while preventing accidental activation.

Asymmetric pivot bin interior uses unequal bucket widths to maximize luggage storage volume within standard aircraft cabin modules.