Turbine nozzle cooling assembly

The present application provides an inner nozzle platform. The inner nozzle platform may include a platform cavity, an impingement plenum positioned within the platform cavity, a retention plate positioned on a first side of the impingement plenum, and a compliant seal positioned on a second side of...

Full description

Saved in:
Bibliographic Details
Main Authors FOSTER GREGORY THOMAS, TIPTON THOMAS ROBBINS, WINN AARON GREGORY, COIGN ROBERT WALTER, PAI NIRANJAN GOKULDAS, PHILLIPS JAMES STEWART, MEENAKSHISUNDARAM RAVICHANDRAN
Format Patent
LanguageEnglish
Published 03.02.2015
Subjects
Online AccessGet full text

Cover

Loading…
More Information
Summary:The present application provides an inner nozzle platform. The inner nozzle platform may include a platform cavity, an impingement plenum positioned within the platform cavity, a retention plate positioned on a first side of the impingement plenum, and a compliant seal positioned on a second side of the impingement plenum.
Bibliography:Application Number: US201213345776