• 专利标题:   Composite used for forming aircraft and projectiles e.g. nose cones, leading edges, and control surfaces, consists of substrate, subsurface layer comprising graphite having cellular structure, and graphitic layer comprising graphite in specified ratio.
  • 专利号:   WO2022192547-A1
  • 发明人:   CAREY B J, BUURMA C F, RATEICK R G, CHENEY P P
  • 专利权人:   BATTELLE MEMORIAL INST
  • 国际专利分类:   B32B027/18, B32B005/18, B32B009/04
  • 专利详细信息:   WO2022192547-A1 15 Sep 2022 B32B-005/18 202283 Pages: 69 English
  • 申请详细信息:   WO2022192547-A1 WOUS019761 10 Mar 2022
  • 优先权号:   US159425P, US210952P

▎ 摘  要

NOVELTY - A composite (100) consists of a substrate (101), a subsurface layer (103) comprising graphite having a cellular structure, and a graphitic layer (105) comprising graphite in an amount higher than that of graphite contained in the subsurface layer. USE - Composite is used for forming aircraft and projectiles e.g. nose cones, leading edges, and control surfaces. ADVANTAGE - The composite has excellent mechanical performance, durability, and thermal insulation properties in thickness direction, and high lateral thermal conductively along the surface, and is formed by fast process. DETAILED DESCRIPTION - An INDEPENDENT CLAIM is included for formation of the composite, which involves providing the substrate comprising a polymer resin and an additive(s), performing a primary heating treatment with respect to the polymer resin and the additive using a laser for forming the subsurface layer on the substrate, and carrying out a secondary heating treatment with respect to the subsurface layer using a laser for forming the graphitic layer on the subsurface layer. DESCRIPTION OF DRAWING(S) - The drawing shows the block diagram of composite. 100Composite 101Substrate 103Subsurface layer 105Graphitic layer T1Thickness of subsurface layer T2Thickness of graphitic layer