Development of High Temperature Seal-Lubricant Deposit Evaluation Techniques

Item

Title
Development of High Temperature Seal-Lubricant Deposit Evaluation Techniques
Date
1965
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
AFAPL TR 65-3
Creator
Pfoutz, Billy D.
Knox, William G.
Gannon, Frank
Corporate Author
Koppers Co Inc Monroeville PA
Laboratory
Air Force Aero Propulsion Laboratory
Date Issued
1965-05-03
Extent
23
NTRL Accession Number
AD617072
Identifier
AD0617072
Access Rights
Notice(s)
Distribution Classification
1
Contract
AF 33(615)-1112
DoD Project
3044
DoD Task
304401
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Distribution Conflict
No
Abstract
Testing techniques for evaluating experimental gas turbine lubricants in face-riding main shaft jet engine seals at temperatures representative of high mach aircraft have been under development. Using the ASD Seal Rig, repeatable evaluation techniques were developed for MIL-L-9236 type lubricants that were indicative of performance in engines. The present phase of the program is directed towards refining evaluation equipment and preparing the rig for more advanced research work. During the period covered, internal seal head air heating to 1160F, preliminary evaluation studies using 0-60-19 and 0-60-18 lubricants, and engineering features of a new seal head design were investigated. An adaptor to permit the use of the seal head with Erdco test equipment is being designed.
Report Availability
Full text available
Publisher
Wright-Patterson Air Force Base, OH : Air Force Aero Propulsion Laboratory, Research and Technology Division, Air Force Systems Command
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource