• 专利标题:   Lightweight drone shell material formulation comprises phenolic epoxy resin, bisphenol F type epoxy resin, titanium nanoparticles, carbon fiber, aramid fiber, graphene, sodium dodecyl sulfate and colorant, and has low density.
  • 专利号:   CN108485205-A
  • 发明人:   LV J
  • 专利权人:   LV J
  • 国际专利分类:   C08K013/04, C08K003/04, C08K003/08, C08K007/06, C08L063/00, C08L063/04, C08L077/10
  • 专利详细信息:   CN108485205-A 04 Sep 2018 C08L-063/04 201866 Pages: 4 Chinese
  • 申请详细信息:   CN108485205-A CN10498628 23 May 2018
  • 优先权号:   CN10498628

▎ 摘  要

NOVELTY - Lightweight drone shell material formulation comprises 40-73 pts. wt. phenolic epoxy resin, 30-65 pts. wt. bisphenol F type epoxy resin, 6-14 pts. wt. titanium nanoparticles, 15-27 pts. wt. carbon fiber, 8-15 pts. wt. aramid fiber, 10-20 pts. wt. graphene, 2-8 pts. wt. sodium dodecyl sulfate, 1-4 pts. wt. colorant. USE - Lightweight drone shell material formulation for preparing a lightweight and high-strength drone housing having a wave transmission requirement. ADVANTAGE - The lightweight drone shell material formulation is suitable for low-pressure molding process, and has low density, high intensity, excellent dielectric properties, simple preparation process, high production capacity, and important practical application value.