Aircraft Assembly TRIZ Cases
- Pre-consolidated Chopped Fiber Charges for Composite Molding
Pre-consolidated chopped fiber charges eliminate air gaps to reduce heating time and die size during composite part fabrication.
- Single-Sided Clamp-Up via Fastener Hole Suction
Air suction through a fastener hole pulls panels together to maintain clamp-up without mechanical actuators.
- Rotorcraft Service Fixture Interference Fit
Interference fit connectors immobilize partially detached components during maintenance.
- Joint Molding Apparatus with Inflatable Bladders for Composite Panel Curing
Inflatable bladders apply radial pressure to maintain joint configuration during curing, preventing resin escape without requiring a curing oven.
- Aircraft Interior Module Preassembly for Efficient Mounting
Preassembled interior modules connect to an assembly apparatus, reducing time-consuming individual positioning.
- Indexed Support Beam for Aerospace Workpiece Orientation
An indexed support beam engages frame assemblies to orient large aerospace structures, enabling precise transfer between work cells.