TY - JOUR
T1 - Processing out-of-autoclave honeycomb structures: Internal core pressure measurements
AU - Kratz, James
AU - Hubert, Pascal
PY - 2011/8
Y1 - 2011/8
N2 - A strong desire to reduce manufacturing costs in the aerospace industry, coupled with recent advancements in out-of-autoclave prepreg materials, has created the potential to manufacture composites with only vacuum pressure. As a step towards better manufacturing of sandwich structures, we focus on the behaviour of air inside a honeycomb core during vacuum bag processing. The pressure of the air inside the core was measured in a lab-scale test fixture to simulate full-scale manufacturing. The lab-scale tests revealed pressure fluctuations if the internal core pressure equalled atmospheric pressure during processing. Furthermore, an increasing number of pressure fluctuations were observed for increasing cure temperatures. Sandwich panels cured at higher temperatures had a higher void content and a worse bond between the skin and core.
AB - A strong desire to reduce manufacturing costs in the aerospace industry, coupled with recent advancements in out-of-autoclave prepreg materials, has created the potential to manufacture composites with only vacuum pressure. As a step towards better manufacturing of sandwich structures, we focus on the behaviour of air inside a honeycomb core during vacuum bag processing. The pressure of the air inside the core was measured in a lab-scale test fixture to simulate full-scale manufacturing. The lab-scale tests revealed pressure fluctuations if the internal core pressure equalled atmospheric pressure during processing. Furthermore, an increasing number of pressure fluctuations were observed for increasing cure temperatures. Sandwich panels cured at higher temperatures had a higher void content and a worse bond between the skin and core.
KW - D. Mechanical testing
KW - D. Process monitoring
KW - E. Prepreg
KW - Out-of-autoclave
UR - http://www.scopus.com/inward/record.url?scp=79957720213&partnerID=8YFLogxK
U2 - 10.1016/j.compositesa.2011.04.009
DO - 10.1016/j.compositesa.2011.04.009
M3 - Article (Academic Journal)
AN - SCOPUS:79957720213
SN - 1359-835X
VL - 42
SP - 1060
EP - 1065
JO - Composites Part A: Applied Science and Manufacturing
JF - Composites Part A: Applied Science and Manufacturing
IS - 8
ER -