A co-bonded acoustic liner uses a thermoset plastic septa film to dampen sound while maintaining structural integrity.
Interchangeable winding core sections vary longitudinal extent and diameter, reducing production costs for variable rotor blades.
Angled core gas turbine engines mount propulsors at skew angles to prevent fragmentation interference between adjacent units.
A replacement motor mount displaces a wind turbine pitch motor to avoid damaged bearing regions, enabling in-situ repairs without removing the rotor.
Mechanical interference fits join turbine diaphragm components, eliminating welding defects and reducing manufacturing costs.
Scalloped turbine platforms with bulges and bowls redirect flow to reduce secondary vortex strength, lowering pressure losses at blade junctions.
Synchronized nozzle vane angular positioning aligns injector heads with dilution air holes to maintain uniform thermal exposure across the turbine outlet.
Inwardly bent stiffening elements reinforce hydraulic machine volute casing segments to distribute mechanical stress peaks at transition points.