|
||||
Department of Engineering |
|
University of Cambridge > Engineering Department > MMD |
Principal Investigator:
Project Details:
The need for energy-efficient and
sustainable, non-polluting gas turbines for aerospace propulsion and industrial power
generation is of major international importance. Components in the hot stage of current
gas turbines are thermally and chemically protected by a thermal barrier coating (TBC)
system. Particles either ingested into the engine or derived from internal spalls, impact
rotating components at ~300 m/s. The smaller particles cause erosion, while larger ones
cause segments of the TBC to spall, resulting in foreign object damage (FOD). Some of the
basic mechanics of impact and material removal have been established and scaling
relationships developed. Two main challenges remain. (a) Material removal due to kink
bands has yet to be modelled. (b) A probabilistic framework for integrating the material
loss caused by sequential impacts remains to be devised.
Background Required:
The successful candidates will have the equivalent of a first from a reputable university
in the field of mechanical engineering, physics or materials science. In finite element
modelling and materials testing will be an advantage but is not necessary.
Funding Source:
Full PhD studentship including fees and maintenance available for UK/EU or overseas students.
Research Groups Involved:
Application Deadline:
Open
For further information and to apply contact:
Professor N A Fleck Cambridge University Engineering Dept Trumpington Street Cambridge, CB2 1PZ United Kingdom |
Phone: +44 (0)1223 332650 Fax: +44 (0)1223 332662 email: div-c@eng.cam.ac.uk |
Initial letters of application and CVs should be sent to Professor Fleck.
| MMD | CUED | University | Search MMD | |
©
2005 Cambridge University Engineering Department (CUED) Information provided by www-mech |