Thrust reverser inner wall structure comprising a thermally conductive
nonmetallic carbon pitch fiber honeycomb core sandwiched between a top and
bottom layer. The core is adhered by a reticulated layer of adhesive to a
perforated carbon fiber top layer, and adhered to a base layer of
nonmetallic, nonperforated carbon fiber reinforced fabric.
Current U.S. Class: | 428/116; 239/265.19; 244/110B; 428/118; 60/226.2 |
Current CPC Class: |
B32B 3/12 (20130101); B32B 5/12 (20130101); E04C 2/365 (20130101); B29C 70/08 (20130101); B29C 70/088 (20130101); F01D 25/24 (20130101); F02K 1/70 (20130101); Y10T 428/24273 (20150115); Y10T 428/236 (20150115); Y10T 428/30 (20150115); Y10T 428/24149 (20150115); Y10T 428/24165 (20150115); Y10T 428/2918 (20150115); Y02T 50/672 (20130101); F05D 2250/283 (20130101) |
Current International Class: |
B32B 3/12 (20060101); B32B 5/12 (20060101); B29C 70/08 (20060101); E04C 2/34 (20060101); E04C 2/36 (20060101); F01D 25/24 (20060101); B32B 017/00 () |
Field of Search: |
;428/116,118 ;60/226.2 ;239/265.19 ;244/11B
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