Title:
発熱体として使用される金属マトリックス複合材
Document Type and Number:
Japanese Patent JP6482759
Kind Code:
B2
Abstract:
A structural substrate (300) for an aircraft structure (606) and methods are presented. A multi-layer hybrid composite material comprises an outermost layer (302), an intermediate layer (304), and an innermost layer (306). The outermost layer comprises an electrically conductive metal matrix composite (308, 400) that conducts electricity to provide electric heating. The intermediate layer (304) comprises an electrical insulator (310) coupled to the outermost layer. The innermost layer (306) comprises a composite (312) coupled to the intermediate layer. The intermediate layer electrically insulates the outermost layer from the innermost layer.
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Inventors:
Nordman, Paul S.
Loftis, Richard J.
Almatrio, andrew
Loftis, Richard J.
Almatrio, andrew
Application Number:
JP2014020011A
Publication Date:
March 13, 2019
Filing Date:
February 05, 2014
Export Citation:
Assignee:
The Boeing Company
International Classes:
B32B7/025; B32B15/08; B64D15/18; H05B3/10; H05B3/12; H05B3/20
Domestic Patent References:
| JP2005517579A | ||||
| JP2011524265A | ||||
| JP2012516268A |
Attorney, Agent or Firm:
Sonoda/Kobayashi Patent Business Corporation