The demanding environment in aircraft turbine engines has driven
the development of many innovative high temperature materials. This
thesis examines one of the latest of these materials, an
oxide/oxide ceramic matrix composite (CMC), N720/A. This CMC
consists of a porous alumina matrix reinforced by Nextel 720 fibers
in a balanced 8 harness satin weave. To characterize this material,
monotonic tensile and cyclic fatigue tests were performed at room
temperature and at 1200 . The effects of moisture on fatigue
behavior were also investigated at 1200 . Modulus, maximum and
minimum strain and stress strain hysteresis were monitored during
the cycling to characterize fatigue damage mechanisms. Retained
strength of all specimens that survived I Os cycles was also
characterized. Microscopy and fractography were used to examine
microstructure, damage mechanisms, and fracture surfaces. N720/A
was found to have good room temperature and high temperature
properties.
General
Imprint: |
Biblioscholar
|
Country of origin: |
United States |
Release date: |
November 2012 |
First published: |
November 2012 |
Authors: |
Steven G. Steel
|
Dimensions: |
246 x 189 x 8mm (L x W x T) |
Format: |
Paperback - Trade
|
Pages: |
138 |
ISBN-13: |
978-1-288-28049-0 |
Categories: |
Books >
Social sciences >
Education >
General
Promotions
|
LSN: |
1-288-28049-1 |
Barcode: |
9781288280490 |
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