发明名称 Method for manufacture of an infused spar cap using a low viscosity matrix material
摘要 Embodiments of the present application generally provide for wind turbine blade spar caps comprising composite materials prepared using a low viscosity resin system and a high density fabric and methods for their manufacture. In particular embodiment, the low viscosity resin system has a viscosity in the range of about 1 to about 100 centipoises at a temperature in the range of about 0° C. to about 125° C. during the preparation of the composite material. By using low viscosity resin systems, composite materials have been prepared having a fiber volume fraction of greater than about 65% and a composite modulus of greater than 48000 MPa.
申请公布号 US8900671(B2) 申请公布日期 2014.12.02
申请号 US201113036853 申请日期 2011.02.28
申请人 General Electric Company 发明人 Lin Wendy;Koeniger Rainer;Suffield Rachel Marie;Sultan Mohamad;Testa Jason
分类号 B05D3/02;B29C70/28;F03D1/06;B29K105/00;B29L31/08 主分类号 B05D3/02
代理机构 Sutherland, Asbill & Brennan LLP 代理人 Sutherland, Asbill & Brennan LLP
主权项 1. A method of manufacturing a wind turbine blade spar cap using a low viscosity resin system, comprising: laminating a high density fabric with a low viscosity resin system to provide a composite material; and curing the composite material, wherein the composite material has a fiber volume fraction of greater than about 65%, and wherein the low viscosity resin system has a viscosity in the range of about 1 to about 100 centipoises at a temperature in the range of about 0° C. to about 125° C.
地址 Schenectady NY US