Affiliation:
1. Latvian State Institute of Wood Chemistry, Dzerbenes 27, LV-1006, Riga, Latvia
2. Institute of Polymer Mechanics, University of Latvia, Aizkraukles 23, LV-1006, Riga, Latvia,
Abstract
Studies on the effect of the foams’ polymeric matrix’ properties on the tension and compression properties of pour rigid polyurethane (PUR) foams, apparent core density 65—70 kg/m3, at 296 and 77 K were carried out. PUR foams were produced by the hand mixing method from polyol systems that comprised polyether, polyester polyols, and chain extenders. To produce PUR foams, crude MDI was used, and Solkane 365 mfc/227 ea was used as a blowing agent. The molecular weight per branching unit (Mc) of the polymeric matrix of PUR foams was varied in the range 300—1150. Cohesion energy densities of the blocks forming the polymeric matrix were calculated. The effect of Mc on the formation of hydrogen bonds between the urethane groups was estimated from FTIR spectroscopy data and ratio NHbonded /NHfree. It has been found that, with increasing polymeric matrix’ Mc, the tensile strength and elongation at break of PUR foams at 296 and 77 K increases, while Young’s modulus decreases. The increase in the parameter Mc promotes the decrease in the compressive strength and modulus of elasticity of PUR foams at 296 K, while compressive strength indices at 77 K are higher for the foams, whose polymeric matrix has the highest Mc. With increasing polymeric matrix’ M c, the concentration of the urethane groups bonded with hydrogen bonds increases. Structural and mechanical properties of layered spray polyurethane foams, apparent core density approx. 48 kg/m3, having two layers and polymeric matrix’ Mc = 740 were investigated.
Subject
Materials Chemistry,Polymers and Plastics,General Chemistry
Reference19 articles.
1. Thermal and Mechanical Properties of Polyurethane Foams at Cryogentic Temperatures
2. Polyisocyanurate Foams for Cryogenic, Petrochemical, and Solar Energy Applications
3. Gates TS, Johnson TJ and Whitley KS Assessment of technologies for the space shuttle external tank thermal protection systems and recommendations for technology improvement. NASA TM-2005-213778, Part 3, July 2005, pp.1-47.
Cited by
61 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献