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The Development of a Hollow Blade for Exhaust Gas TurbinesThe subject of the development of German hollow turbine blades for use with internal cooling is discussed in detail. The development of a suitable blade profile from cascade theory is described. Also a discussion of the temperature distribution and stresses in a turbine blade is presented. Various methods of manufacturing hollow blades and the methods by which they are mounted in the turbine rotor are presented in detail.
Document ID
19930093941
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kohlmann, H
Date Acquired
August 16, 2013
Publication Date
December 1, 1950
Report/Patent Number
NACA-TM-1289
Report Number: NACA-TM-1289
Accession Number
93R23267
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBINES - BLADES, HOLLOW
TURBINES - BLADES - TEMPERATURE
PRESSURE DISTRIBUTION - AIRFOILS - CASCADES
TURBINES - BLADES - STRESSES
TURBINES, EXHAUST - BMW 801
TURBINES - BLADES - COOLING
FLOW - AIRFOILS - CASCADES

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