Loading...
Please wait, while we are loading the content...
Similar Documents
Fretting fatigue of gamma tial studied
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Miyoshi, Kazuhisa Lerch, Bradley A. Draper, Susan L. |
| Copyright Year | 2003 |
| Description | Gamma titanium-aluminum alloy (g-TiAl) is an attractive new material for aerospace applications because of its low density and high specific strength in comparison to currently used titanium and nickel-base alloys. Potential applications for this material are compressor and low-pressure turbine blades. These blades are fitted into either the compressor or turbine disks via a dovetail connection. The dovetail region experiences a complex stress state due to the alternating centrifugal force and the natural high-frequency vibration of the blade. Because of the dovetail configuration and the complex stress state, fretting is often a problem in this area. Furthermore, the local stress state becomes more complex when the influence of the metal-metal contact and the edge of the contact is evaluated. Titanium and titanium-based alloys in the clean state exhibit strong adhesive bonds when in contact with themselves and other materials (refs. 1 and 2). This adhesion causes heavy surface damage and high friction in practical cases. Although the wear produced by fretting may be mild, the reduction in fatigue life can be substantial. Thus, there is the potential for fretting problems with these TiAl applications. Since TiAl is an emerging material, there has been limited information about its fretting behavior. |
| File Size | 43968 |
| Page Count | 3 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20050214733 |
| Archival Resource Key | ark:/13960/t9m37s674 |
| Language | English |
| Publisher Date | 2003-03-01 |
| Access Restriction | Open |
| Subject Keyword | Metals And Metallic Materials Metal Fatigue Fretting Vibration Turbine Blades Aluminum Alloys Adhesive Bonding Aerospace Engineering Titanium Alloys Friction Wear Low Pressure Titanium High Strength Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |