Wear during Rubbing of a Sintered Metal Powder Body.
Abstract
Rub interactions were carried out between an abradable nickel-chromium seal material and titanium alloy blades at slow speeds. Square-ended and negative rake angles blades with blade tip lays parallel and perpendicular to rubbing were fed at six different rates ranging from 0.16 to 100 x .000001 m/pass. The specific energy of seal material displacement increased substantially with feed. A relationship between feed and specific energy of seal material displacement was suggested. The modulus of elasticity of the seal material was found to vary with strain. Results from tensile tests accomplished during this work were combined with data from compression tests to derive a relationship between modulus of elasticity and strain. Based on the results of these tests, it is suggested that the primary mechanism of seal material wear was fatigue.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1983
- Accession Number
- ADA132354
Entities
People
- John R. Rogacki
Organizations
- Air Force Institute of Technology