Blade Accessories TRIZ Cases
- Airfoil Cooling Hole Pad Design for L/D Ratio Control
Segmented metering and diffuser sections preserve flow control direction in thin gas turbine blades despite reduced wall thickness.
- Rotor Connection via Hollow Space Negative Pressure
Vacuum in a hollow space connects rotor components, eliminating thermal loading and weight from welding or screws.
- Transition Nozzle Combustor Liner Tangential Flow Contouring
A transition nozzle liner directs combustion products tangentially to induce turbine rotation without a separate nozzle stage.
- Lanthanum Molybdate Abradable Coatings for Gas Turbine Blade Tip Protection
A lanthanum molybdate abradable coating protects ceramic matrix composite blade tips from wear during rub events with metal shrouds.
- Integral Composite Stator Vane Ring Manufacturing
Fibre jointing and resin infusion form an integral stator vane ring, reducing manufacturing complexity while maintaining structural load transfer.