Wear of seal materials used in aircraft propulsion systems

Wear

Volumn 59, Issue 1, 1980, Pages 165-189

  Bill, Robert C ^a   Ludwig, Lawrence P ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

SEALS - WEAR;

AIRCRAFT ENGINES, JET AND TURBINE;

EID: 0018446148     PISSN: 00431648     EISSN: None     Source Type: Journal    
DOI: 10.1016/0043-1648(80)90277-X     Document Type: Article

References (23)

1. Investigation and analysis of reliability and maintainability problems associated with Army aircraft engines
2. Advanced seal technology
3. Dynamic sealing principles
4. Mating materials and environment combinations for specific contact and clearance type seals
5. Development of seal ring carbon-graphite materials
6. Fundamentals of fluid sealing
7. Design considerations in mechanical face seals for improved performance. I. Basic configurations
8. Design considerations in mechanical face seals for improved performance. II. Lubrication
9. Wear and friction of impregnated mechanical carbons at temperatures to 1400°F (760°C) in air or nitrogen
10. Graphite lubrication
11. Am. Soc. Mech. Eng. Pap., 57-Lub-1
12. Breakdown and surface fatigue of carbons during repeated sliding
13. Pressure distribution for patchlike contact in seals with frictional heating, thermal expansion, and wear
14. Thermocracking of seal faces in mechanical seals
15. Fretting in aircraft turbine engines
16. Development of materials resistant to wear and corrosion for mechanical-face-seal applications
17. Abradable compressors and turbine seals
18. Friction and wear of several compressor gas path seal materials
19. Compressor seal rub energetics study
20. Friction and wear of sintered fibermetal abradable seal materials
21. Aerodynamic performance of conventional and advanced design labyrinth seals with solid-smooth, abradable, and honeycomb lands—gas turbine engines
22. Development of abradable gas path seals