Propeller blade
US-2024109645-A1 · Apr 4, 2024 · US
US9238720B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9238720-B2 |
| Application number | US-201013202829-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 16, 2010 |
| Priority date | Feb 25, 2009 |
| Publication date | Jan 19, 2016 |
| Grant date | Jan 19, 2016 |
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Official abstract text for this publication.
This invention relates to a prepreg having a low thermal expansion coefficient in plane direction and a high rigidity, and more particularly to a prepreg comprising a glass cloth (A), and a resin composition including a cyanate ester resin (B), a non-halogen based epoxy resin (C) and an inorganic filler (D), wherein the glass cloth (A) is characterized that when the weight per 1 m 2 is W (g/m 2 ), the thickness is t (μm), the number of warp threads per inch is X (thread/inch), and the number of weft threads per inch is Y (thread/inch), the total of X and Y is 150 to 240, t is 17 to 35, and the value of W/t as the apparent density is 1.1 to 1.5, and that the volume fraction of the glass cloth (A) in the prepreg is 32% to 42%.
Opening claim text (preview).
The invention claimed is: 1. A prepreg composed of (A) a glass cloth with a resin composition comprising (B) a cyanate resin, (C) a non-halogen based epoxy resin and (D) an inorganic filler, wherein the weight per 1 m 2 in said glass cloth (A) is W (g/m 2 ), thickness is t (μm), end count of warp threads per inch is X (thread/inch), and end count of weft threads per inch is Y (thread/inch), the total of X and Y is 150 to 240, t is 17 to 35, and the value of W/t as an apparent density is 1.1 to 1.5, and that volume content of the glass cloth (A) in the prepreg is 32% to 42%. 2. A prepreg according to claim 1 , wherein the cyanate resin (B) is a cyanate resin represented by the following general formula (1), wherein each R independently represents a hydrogen atom or a methyl group, and n represents an integer of not less than 1. 3. A laminate obtained by curing a prepreg as claimed in claim 1 . 4. A metal foil-clad laminate obtained by curing a laminate of a prepreg as claimed in claim 1 and a metal foil. 5. A laminate obtained by curing a prepreg as claimed in claim 2 . 6. A metal foil-clad laminate obtained by curing a laminate of a prepreg as claimed in claim 2 and a metal foil.
bonded with or embedded in a plastic substance · CPC title
Woven fibrous reinforcement or textile · CPC title
Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs · CPC title
comprising aluminium or copper {(B32B15/016 and B32B15/017 take precedence)} · CPC title
characterised by weave density or surface weight · CPC title
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