发明名称 Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials
摘要 Methods and apparatus are described to use real-time measurement systems to detect the onset of compression induced micro-fracturing of fiber-reinforced composite materials. Measurements are described to detect the onset of compression induced micro-fracturing of fiber-reinforced composite materials to prevent catastrophic failures of aircraft components containing such materials. Methods and apparatus are described to prevent fluids and gases from invading any compression induced microfractures by coating surfaces of fiber-reinforced materials to reduce the probability of failure of such fiber-reinforced materials.
申请公布号 US9625361(B1) 申请公布日期 2017.04.18
申请号 US201313966172 申请日期 2013.08.13
申请人 Smart Drilling and Completion, Inc. 发明人 Vail, III William Banning
分类号 G01N15/08;G01L1/00;G01N3/08;B64C1/26;B64C1/00 主分类号 G01N15/08
代理机构 Sheridan Ross P.C. 代理人 Sheridan Ross P.C.
主权项 1. A real time electronics measurement system to assess failure of a portion of an aircraft made at least in part with fiber reinforced composite material comprising, measurement means fabricated within the wing and wing-box portion of an aircraft to detect the invasion of fluids and gases into compression induced microfractures of the fiber-reinforced composite materials, communication means for outputting data generated by the measurement means, and a remote receiver for receiving the data output.
地址 Bothell WA US