ePrints@IIScePrints@IISc Home | About | Browse | Latest Additions | Advanced Search | Contact | Help

A synergy of atmospheric plasma and UV-additive incorporated PU and styrene–isoprene-styrene adhesive for improving inter-layer adhesion in PVF/Fabric/BOPET laminate for aerostat envelope

Kundu, S and Adak, B and Tomar, S and Joshi, M (2023) A synergy of atmospheric plasma and UV-additive incorporated PU and styrene–isoprene-styrene adhesive for improving inter-layer adhesion in PVF/Fabric/BOPET laminate for aerostat envelope. In: Composites Part A: Applied Science and Manufacturing, 173 .

[img] PDF
com_par_app_173_2023.pdf - Published Version
Restricted to Registered users only

Download (15MB) | Request a copy
Official URL: https://doi.org/10.1016/j.compositesa.2023.107650

Abstract

Engineers and material scientists face a significant challenge in finding the right adhesive and technology to join the layers of a multi-layered laminated composite for making lightweight aircrafts. This paper focuses on a novel method of exposing substrates to atmospheric-plasma using different purging gases and subsequent adhesive-lamination. Three separate plasma-exposed layers— polyvinyl fluoride (PVF) film, polyester fabric, and biaxially oriented polyethylene terephthalate (BOPET) film were joined together using two different solvent-borne/pressure-sensitive adhesives, based on polyurethane and styrene–isoprene-styrene. Both adhesives were compounded with organic UV-additives and nano-carbon black for improving weather resistance. The composite laminates were exposed to accelerated weathering for 100 h to qualify for the targeted application of aerostat envelope/hull. Among different gas combinations, the helium/oxygen-mixture (80:20) showed the best results in terms of surface etching/functionalization, which strongly attributed to improving adhesion-strength. Among two adhesives, styrene–isoprene-styrene-based adhesive performed much better. This adhesive was UV-cured after post-weathering cycle, and it improved inter-laminar adhesion strength by 81% and reached 16.2 N/cm. As a consequence, it prevented adhesive breakage from the weak bond layers and turned it into a cohesive failure from the adhesive layer. Most importantly, the laminated fabric showed excellent helium gas barrier property, which improved further after weathering cycle, making it ideal for the targeted application.

Item Type: Journal Article
Publication: Composites Part A: Applied Science and Manufacturing
Publisher: Elsevier Ltd
Additional Information: The copyright for this article belongs to the Elsevier Ltd.
Keywords: A: Fabrics/Textiles; A: Laminates; B: Adhesion; D: Chemical analysis; Gas barrier
Department/Centre: Division of Interdisciplinary Sciences > Centre for Nano Science and Engineering
Date Deposited: 20 Jul 2023 07:00
Last Modified: 20 Jul 2023 07:00
URI: https://eprints.iisc.ac.in/id/eprint/82486

Actions (login required)

View Item View Item