United Technologies Corporation

Christopher Charles Williams

George P Liang

Hans R Przirembel

Timothy J Remley

J Tyson Balkcum, Iii

The present invention relates to a lightweight shrouded turbine blade. The turbine blade comprises an airfoil section and a hollow blade tip shroud joined to the airfoil section. The hollow tip shroud is preferably a cast, compartmentalized structure and has a plurality of ribs acting as load bearing structures and defining a plurality of shroud core sections. Each of the shroud core sections communicates with a supply of cooling fluid and has a plurality of apertures for supplying cooling fluid to exterior portions of the shroud.

Thin walled cooled hollow tip shroud

A brush seal for an apparatus having a stationary member and a rotating member is provided comprising a seal element and a seal ring. The seal element includes a plurality of bristles and is attached to one of the stationary or rotating members. The seal ring is detachably attached to the other of the stationary or rotating members, aligned with the seal element. The seal ring may be readily detached from the stationary or rotating member and may be replaced in the event of mechanical damage to the seal ring by the seal element. The seal ring isolates the stationary or rotating member, to which the seal ring is attached, from mechanical damage caused by the seal element.

Growing community of inventors

Lake Worth, FL, United States of America

Christopher Charles Williams