POWER TURBINE COOLING AIR METERING RING

A power turbine section for a gas turbine engine includes a heat shield assembly mounted to a bearing support to form a first annular compartment and a second annular compartment.

Saved in:
Bibliographic Details
Main Authors KORZENDORFER JOHN J, BETANCOURT FABIAN D, GRANT FERNANDO K
Format Patent
LanguageEnglish
Published 14.04.2016
Subjects
Online AccessGet full text

Cover

Loading…
More Information
Summary:A power turbine section for a gas turbine engine includes a heat shield assembly mounted to a bearing support to form a first annular compartment and a second annular compartment.
Bibliography:Application Number: US201414512532