• 专利标题:   High thermal conductivity composite film used for, e.g. aerospace comprises premixed material layer comprising thermally conductive filler, auxiliary agent and adhesive, and in-plane reinforcement layer.
  • 专利号:   CN113276487-A, CN113276487-B
  • 发明人:   DUAN C, LIU J, WANG Q, ZHENG D, LIANG W, XU W
  • 专利权人:   CHN ENERGY INVESTMENT GROUP CO LTD, NAT INST CLEAN LOW CARBON ENERGY
  • 国际专利分类:   B32B003/24, B32B037/06, B32B037/10, B32B007/12, B32B009/00, B32B009/04, C08J005/18, C08K003/04, C08K007/00, C08K007/24, C08L023/06, C08L009/08
  • 专利详细信息:   CN113276487-A 20 Aug 2021 B32B-003/24 202186 Pages: 10 Chinese
  • 申请详细信息:   CN113276487-A CN10102004 19 Feb 2020
  • 优先权号:   CN10102004

▎ 摘  要

NOVELTY - A high thermal conductivity composite film comprises premixed material layer and in-plane reinforcement layer laminated together. The premixed material layer comprises thermally conductive filler, auxiliary agent and adhesive. The weight ratio of thermally conductive filler and auxiliary agent is 0.1-40:1. The ratio of total content of thermally conductive filler and auxiliary agent and adhesive content is 5.5-49:1. USE - The high thermal conductivity composite film is used for high-end applications, such as military, aerospace and other high-end requirements for thermal conductivity. ADVANTAGE - The composite film can maintain high horizontal thermal conductivity and vertical thermal conductivity, and has large thickness. DETAILED DESCRIPTION - INDEPENDENT CLAIMS are included for: (1) preparation of the high thermal conductivity composite film comprising mixing thermally conductive filler, auxiliary agent and adhesive to obtain premixed material, adding in-plane reinforcement layer at mass ratio of 0.8-2:1, compounding, and molding; and (2) a high thermal conductivity composite film.