Segmented retaining plates with elastically deformable tongues simplify assembly and ensure stability within narrow internal shells.
Integrating the rear wall into the bearing housing eliminates heat shield deformation, maintaining compact axial space while preventing thermal collisions.
Crimping secures a retainer plate and one-way clutch within a stator hub bore.
A single row vane assembly redirects engine airflow through a transcowl aperture to generate reverse thrust.
A slide-in nozzle block design uses inner and outer retaining rings to secure the component within a steam turbine nozzle chamber.
A gas turbine stator assembly uses a deformable non-metallic embedded component within the potting material to secure the vane to the ring structure.
A twin-vaned nozzle ring assembly directs exhaust gas streams through interleaved passages to maintain flow separation.