Blade Accessories TRIZ Cases
- Silicon Bond Coating Contained Between Refractory Layers
A silicon-based bond coating contains a molten silicon phase within a refractory matrix to maintain structural integrity during thermal cycling.
- Rotor Blade Stub Spar and Thick Skin Load Distribution
Segmenting the spar into a stub configuration while thickening skins resolves strength versus manufacturing complexity trade-offs.
- Turbine Coating Apparatus with Segmented Chamber and Cut-Out Plate
Segmented coating vessels use plates with cut-outs to direct gas into internal turbine passages, preventing external aluminum deposition.
- Annulus Filler Composite Material Impact Resistance
A composite annulus filler combines high-modulus and tough polymer reinforcement elements to balance stiffness with impact resistance.
- Monolithic Composite Aircraft Leading Edge Co-Curing
Co-curing a monolithic composite leading edge eliminates separate assembly steps, reducing manufacturing complexity while maintaining structural integrity.
- Fe-Ni-Co Superalloy Grain Boundary Precipitation for Low Thermal Expansion
Austenite matrix with granular intermetallic compounds reduces thermal expansion in Fe-Ni-Co alloys.
- Non-continuous abradable coating blocks for turbine sealing
Discrete coating blocks minimize leakage by reducing residual stress and bond strength loss in high-temperature turbine systems.
- Friction Joining Preheating for Reduced Load and Burr Discharge
Preheating metal joining surfaces to 20% of melting point allows burr discharge without increasing pressing mechanism size.
- Non-linear Cooling Conduit for Turbine Nozzle Fillet Spallation
Curved drilling forms a non-linear cooling conduit in the turbine nozzle fillet, eliminating spallation from direct mechanical stress.