NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Crescentic ramp turbine stageA turbine stage includes a row of airfoils joined to corresponding platforms to define flow passages therebetween. Each airfoil includes opposite pressure and suction sides and extends in chord between opposite leading and trailing edges. Each platform includes a crescentic ramp increasing in height from the leading and trailing edges toward the midchord of the airfoil along the pressure side thereof.
Document ID
20080009482
Acquisition Source
Glenn Research Center
Document Type
Other - Patent
Authors
Lee, Ching-Pang
Tam, Anna
Kirtley, Kevin Richard
Lamson, Scott Henry
Date Acquired
August 24, 2013
Publication Date
May 22, 2007
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-11/106,198
Patent Number: US-Patent-7,220,100
Funding Number(s)
CONTRACT_GRANT: NAS3-01135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,220,100
Patent Application
US-Patent-Appl-SN-11/106,198
No Preview Available