An in-process cure monitoring technique based on “guided wave” concept for carbon fiber reinforced polymer (CFRP) composites was developed. Key parameters including physical properties (viscosity and degree of cure) and state transitions (gelation and vitrification) during the cure cycle were clearly identified experimentally from the amplitude and group velocity of guided waves, validated via the semi-empirical cure process modeling software RAVEN. Using the newly developed cure monitoring system, an array of high-temperature piezoelectric transducers acting as an actuator and sensors were employed to excite and sense guided wave signals, in terms of voltage, through unidirectional composite panels fabricated from Hexcel® IM7/8552 prepreg during cure in an oven. Average normalized peak voltage, which pertains to the wave amplitude, was selected as a metric to describe the guided waves phenomena throughout the entire cure cycle. During the transition from rubbery to glassy state, the group velocity of the guided waves was investigated for connection with degree of cure, Tg, and mechanical properties. This work demonstrated the feasibility of in-process cure monitoring and continued progress toward a closed-loop process control to maximize composite part quality and consistency.
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Automated In-Process Cure Monitoring of Composite Laminates Using a Guided Wave-Based System With High-Temperature Piezoelectric Transducers
Tyler B. Hudson,
Tyler B. Hudson
Department of Mechanical and
Aerospace Engineering,
North Carolina State University,
911 Oval Drive—3306 EBIII,
Campus Box 7910,
Raleigh, NC 27695;
Aerospace Engineering,
North Carolina State University,
911 Oval Drive—3306 EBIII,
Campus Box 7910,
Raleigh, NC 27695;
National Institute of Aerospace,
100 Exploration Way,
Hampton, VA 23666
e-mail: tyler.b.hudson@nasa.gov
100 Exploration Way,
Hampton, VA 23666
e-mail: tyler.b.hudson@nasa.gov
Search for other works by this author on:
Fuh-Gwo Yuan
Fuh-Gwo Yuan
Department of Mechanical and
Aerospace Engineering,
North Carolina State University,
911 Oval Drive—3306 EBIII,
Campus Box 7910,
Raleigh, NC 27695;
Aerospace Engineering,
North Carolina State University,
911 Oval Drive—3306 EBIII,
Campus Box 7910,
Raleigh, NC 27695;
National Institute of Aerospace,
100 Exploration Way,
Hampton, VA 23666
100 Exploration Way,
Hampton, VA 23666
Search for other works by this author on:
Tyler B. Hudson
Department of Mechanical and
Aerospace Engineering,
North Carolina State University,
911 Oval Drive—3306 EBIII,
Campus Box 7910,
Raleigh, NC 27695;
Aerospace Engineering,
North Carolina State University,
911 Oval Drive—3306 EBIII,
Campus Box 7910,
Raleigh, NC 27695;
National Institute of Aerospace,
100 Exploration Way,
Hampton, VA 23666
e-mail: tyler.b.hudson@nasa.gov
100 Exploration Way,
Hampton, VA 23666
e-mail: tyler.b.hudson@nasa.gov
Fuh-Gwo Yuan
Department of Mechanical and
Aerospace Engineering,
North Carolina State University,
911 Oval Drive—3306 EBIII,
Campus Box 7910,
Raleigh, NC 27695;
Aerospace Engineering,
North Carolina State University,
911 Oval Drive—3306 EBIII,
Campus Box 7910,
Raleigh, NC 27695;
National Institute of Aerospace,
100 Exploration Way,
Hampton, VA 23666
100 Exploration Way,
Hampton, VA 23666
1Corresponding author.
Manuscript received September 11, 2017; final manuscript received January 22, 2018; published online February 23, 2018. Assoc. Editor: Andrei Zagrai.
ASME J Nondestructive Evaluation. May 2018, 1(2): 021008-021008-8 (8 pages)
Published Online: February 23, 2018
Article history
Received:
September 11, 2017
Revised:
January 22, 2018
Citation
Hudson, T. B., and Yuan, F. (February 23, 2018). "Automated In-Process Cure Monitoring of Composite Laminates Using a Guided Wave-Based System With High-Temperature Piezoelectric Transducers." ASME. ASME J Nondestructive Evaluation. May 2018; 1(2): 021008–021008–8. https://doi.org/10.1115/1.4039230
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