作者: David E Kranbuehl , Al Loos
DOI: 10.1007/978-94-011-4437-7_12
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摘要: The resin transfer moulding (RTM) process has been used in the past primarily for production of lower performance composite structures. These structures typically have low fibre volumes and use relatively low-temperature matrices such as polyester resins. Advanced constructed with high-temperature resins require high void contents to be qualified aircraft service [1].