Title :
A comparative study on failure pressure estimations of GFRP pressure vessels using Acoustic Emission technique
Author :
Joselin, R. ; Enamuthu, M. ; Usha, K.M. ; Vasudev, E.S. ; Chelladurai, T.
Author_Institution :
JNTU Hyderabad, Hyderabad, India
Abstract :
There is a need of design a reliable light weight composite pressure vessel for a launch vehicle or missile system. The composite pressure vessel acted upon by static internal pressure and dynamic during flight, but for practical structural integrity purposes, consideration of internal pressure is all that is necessary. This paper examines the performance of 6-litre capacity cylindrical Glass fiber reinforced plastic (GFRP) pressure vessel under cyclic loading cum burst tests using Acoustic Emission (AE) technique. AE data was acquired only up to 50% of the theoretical burst pressure. Based on the inferences a relation was developed to predict the burst performance of this class of bottles. In fact, one could infer that impending failure was significant even at 50 to 60% of maximum expected operating pressure (MEOP) with a reasonable error margin. Comparative studies were performed with identically machined GFRP pressure vessels which are also within the limit.
Keywords :
acoustic emission; bottles; failure (mechanical); glass fibre reinforced plastics; lightweight structures; pressure vessels; GFRP pressure vessels; acoustic emission technique; bottles; burst tests; cyclic loading; failure; failure pressure estimations; glass fiber reinforced plastic; launch vehicle; light weight composite pressure vessel; maximum expected operating pressure; missile system; practical structural integrity; static internal pressure; Acoustic emission; Hardware; Machining; Monitoring; Sensors; Windings; Wounds; Acoustic Emission; GFRP pressure vessel; MEOP; Machining; Prediction;
Conference_Titel :
Recent Advances in Space Technology Services and Climate Change (RSTSCC), 2010
Conference_Location :
Chennai
Print_ISBN :
978-1-4244-9184-1
DOI :
10.1109/RSTSCC.2010.5712807