Siemens Energy, Inc.

Diego L Caso, Jr

Anand A Kulkarni

Zafir A M Abdo

Mahesh Janarthanan

Navin J Manjooran

Ryan J Majkut

Anita Marie Hunt

An air separator in a gas turbine engine includes a cylindrical member and a seal flange having a flange body extending radially outward at a rearward end of the cylindrical member. A head portion is located at a radially outer free end of the flange body and includes an axial flange located axially rearward of the flange body and defining a rearward seal face for engagement with a blade disc forward face, and a forward cantilevered head mass extending axially forward from the flange body. An axial dimension of the head mass, from a connection with the forward side of flange body to an axially forward face of the head mass, is greater than a maximum radial dimension of the head mass, from a radially inner side of the head mass to a radially outermost side of the head mass.

Air separator for gas turbine engine

A composition and method for cleaning turbine engine components () during servicing. An embodiment of the invention includes a colloidal mixture or slurry () of nanoparticles. The slurry may be nontoxic and provide optimal cleaning of tiny surface-exposed crevices () of braze joints and components. When a colloidal mixture is in a polar solvent, the pH of the slurry is maintained at about 5 to 9 and at the isoelectric point of the nanoparticles to minimize or prevent agglomeration. When a colloidal mixture is in a nonpolar solvent, the pH of the slurry is maintained at about 5 to 9 and at the isoelectric point of the nanoparticles to minimize or prevent agglomeration by use of surfactant additives.

Repair of a turbine engine surface containing crevices

Growing community of inventors

Winter Garden, FL, United States of America

Diego L Caso, Jr