Accession Number : AD0481394
Title : DESIGN AND TEST OF TRANSPIRATION AIR COOLED TURBINE BLADES IN A FULL SCALE TURBOJET ENGINE
Descriptive Note : Final rept.
Corporate Author : CURTISS-WRIGHT CORP QUEHANNA PA
Personal Author(s) : Lauziere, N ; Kump, D
PDF Url : AD0481394
Report Date : 28 Nov 1958
Pagination or Media Count : 92
Abstract : The feasibility of achieving higher turbine inlet temperatures and increasing engine performance by the use of transpiration air cooled blades has been established. Compromises in the basic aerodynamic or mechanical design of the turbine are not necessary for the type of transpiration cooled blades developed. This transpiration air cooled turbine rotor blade can be fabricated by low cost, mass production techniques. Significant advances have been made in brazing of the porous material, but the brazing cycle is critical and requires additional research to broaden its time-temperature relationship.
Descriptors : *EVAPOTRANSPIRATION, *TURBOJET ENGINES, AIR COOLED, BRAZING, FEASIBILITY STUDIES, INSTRUMENTATION, OPTIMIZATION, PERFORMANCE(ENGINEERING), POROUS MATERIALS, ROTOR BLADES(TURBOMACHINERY), TEMPERATURE, TEST METHODS, TURBINE BLADES
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE