发明名称 COMPRESSION MOLDED FIBER REINFORCED FAN CASE ICE PANEL
摘要 An ice panel for a fan case of a gas turbine engine is disclosed. The ice panel may comprise a facesheet located on an inner surface of the fan case and it may comprise a chopped prepreg tape that is cured. The chopped prepreg tape may comprise randomly oriented chips of fibers impregnated with a resin matrix.
申请公布号 US2016245175(A1) 申请公布日期 2016.08.25
申请号 US201415029465 申请日期 2014.05.23
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 CLARKSON Steven;ROBERTSON Thomas J.
分类号 F02C7/047;F02C3/04 主分类号 F02C7/047
代理机构 代理人
主权项 1. An ice panel for a fan case of a gas turbine engine, comprising: a facesheet formed of a chopped prepreg tape that is cured, the chopped prepreg tape comprising randomly oriented chips of fibers; and a resin matrix impregnated in the randomly oriented chips of fibers.
地址 Hartford CT US