Reinforcement of Gas Turbine Blades by Technological Methods,

reportActive / Technical Report | Accession Number: ADA046222 | Open PDF

Abstract:

The article discusses the more important methods and means which increase the durability, dependability, and heat resistance of gas turbine blades. New materials from which blades are constructed are discussed as well as the technology of their manufacture. The protective coatings used to reinforce the blades and increase their resistance to corrosion are presented.

Author(s):
Lunarski, J.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited trans. of Technika Lotnicza i Astronautyczna (Poland) n5 p14-18 May 74, by F. Zaleski.
Annotation:
Reinforcement of Gas Turbine Blades by Technological Methods--Translation.
Pagination:
0022

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-ID(RS)I-0477-77
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means
Modernization Areas:
Microelectronics
Communities of Interest:
Air Platforms
Descriptor(s):
*GAS TURBINE BLADES, *REFRACTORY COATINGS, *HEAT RESISTANT ALLOYS, TRANSITION METALS, MANUFACTURING, HIGH TEMPERATURE, ALLOYS, COOLING, GAS TURBINES, TRANSLATIONS, NICKEL ALLOYS, SILICON CARBIDES, REINFORCING MATERIALS, POLAND, TUNGSTEN ALLOYS, METAL FIBERS
Field(s)/Group(s):
Metallurgy and Metallography, Jet and Gas Turbine Engines
Report Date:
1977 Apr 26