Advanced Turbine Engine Gas Generator Conceptual Studies and Feasibility Experimental Test Program. Volume III: Materials Section (Table LXXV)

reportActive / Technical Report | Accession Number: AD0852062 | Open PDF

Abstract:

Materials research and development was performed on diffusion bonding of titanium, machining of small-diameter holes, determination of the abrasive properties of materials in a simulated jet-engine environment, and determination of the properties of selected materials in a high-temperature corrosive and erosive environment.

Author(s):
Groh, Frederick G.
Author Organization(s):
PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT
Descriptive Note:
Final rept. 1 Jun 1966-31 Aug 1967
Supplementary Note:
See also Volume 2, AD501544.
Pagination:
0147

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
PWA-3219-VOL-3, AFAPL-TR-69-35-VOL-3
Contract/Grant Number(s):
AF, 33(657)-15504
Project Number(s):
AF-681B
Monitor Series:
TR-69-35-VOL-3, AFAPL
 Subject Terms
Joint Capability Areas:
JCA_5_Command and Control; JCA_4.5.4_Requirements Definition; JCA_4.5_Operational Contract Support; JCA_1.2.5_Lessons Learned; JCA_5.3_Planning; JCA_5.5.2_Task; JCA_5.5_Direct
Communities of Interest:
Counter WMD
Descriptor(s):
*TURBOFAN ENGINES, *HEAT RESISTANT MATERIALS, THICKNESS, MANUFACTURING, AGING(MATERIALS), ALUMINUM ALLOYS, MACHINING, CRACKS, METAL COATINGS, DIFFUSION BONDING, LASERS, STEEL, EROSION, FEASIBILITY STUDIES, OXIDATION, PLANNING, BONDED JOINTS, JET TRANSPORT AIRCRAFT, GLASS TEXTILES, VANADIUM ALLOYS, ABRASIVES, MANDRELS, TURBOJET ENGINES, HONEYCOMB CORES, SANDWICH CONSTRUCTION, FATIGUE(MECHANICS), NICKEL ALLOYS, TITANIUM ALLOYS, WEAR RESISTANCE, DRILLING
Field(s)/Group(s):
Transport Aircraft, Refractory Fibers, Fabrication Metallurgy, Jet and Gas Turbine Engines
Keyword(s):
HOLES(CAVITIES), NICKEL ALLOY HASTELLOY, STEEL 1025, TITANIUM ALLOY 5AL 4V
Report Date:
1969 May 01