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 |