Patent US5126091A successfully refreshed from Google Patents.
US5126091A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for manufacturing composite material
Assignee: GKN Westland Aerospace Avonmouth Ltd
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Filing: 1991-01-22
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Granted: 1992-06-30
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Expires: 2011-01-22
Abstract
Abstract A method for manufacturing perforate, fibre-reinforced, composite material, comprising the steps of laying up reinforcing fibres and resin in a mould having needles, the mould including a stripper plate having perforations into which the needles pass when the mould is assembled; curing the resin; and withdrawing the composite from the mould along with the stripper plate.
Inventors
- 👤 Adrian W. Melton
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 17:10
CPC Classifications
B; B29; B29C; B29C33/00; B29C33/0033; B29C37/00; B29C37/0003; B29C70/00; B29C70/04; B29C70/28; B29C70/40; B29C70/42; B29C70/46; B29C70/54; B29C70/545; B29D; B29D28/00; B29D28/005; B29C43/00; B29C43/32; B29C43/36; B29C2043/3665; B29L; B29L2031/00; B29L2031/737
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
204 words
A method of manufacturing perforate, fibre-reinforced, composite material, said method comprising the steps: (a) laying up a reinforcing fibre material in one part of a mould, said mould being capable of receiving reinforcing fibre material and resin to be moulded into a fibre-reinforced, composite material, said mould comprising: a first part having needles, a complementary second part, and a stripper plate having perforations into which corresponding needles of said first part of the mould are capable of passing when the mould is assembled, (b) enclosing said reinforcing fibre material in said mould, by assembling the remaining parts of said mould so that said needles of said first part of said mould pass into said corresponding perforations of said stripper plate, and perforate said reinforcing fibre material substantially by parting the fibres of said reinforcing fibre material without breaking said fibres, (c) impregnating said reinforcing fibre material in said mould with resin, with said needles still within said perforations, and (d) curing said resin in said mould, whereby the perforate, fibre-reinforced composite material withdraws from said mould with said stripper plate rather than with said first part of the mould having needles when said mould parts are disassembled to release the perforate, fibre-reinforced composite material.
Claim 2
Independent Claim
204 words
A method of manufacturing perforate, fibre-reinforced, composite material, said method comprising the steps: (a) laying up a reinforcing fibre material in one part of a mould, said mould being capable of receiving reinforcing fibre material and resin to be moulded into a fibre-reinforced, composite material, said mould comprising: a first part having needles, a complementary second part, and a stripper plate having perforations into which corresponding needles of said first part of the mould are capable of passing when the mould is assembled, (b) enclosing said reinforcing fibre material in said mould, by assembling the remaining parts of said mould so that said needles of said first part of said mould pass into said corresponding perforations of said stripper plate, and perforate said reinforcing fibre material substantially by parting the fibres of said reinforcing fibre material without breaking said fibres, (c) impregnating said reinforcing fibre material in said mould with resin, with said needles still within said perforations, and (d) curing said resin in said mould, whereby the perforate, fibre-reinforced composite material withdraws from said mould with said stripper plate rather than with said first part of the mould having needles when said mould parts are disassembled to release the perforate, fibre-reinforced composite material.
Claim 3
Dependent Claim
53 words
A method according to claim 1 in which, when the mould is assembled with resin impregnated reinforcing fibre therein, the area of contact between said stripper plate and said resin impregnated fibre is greater than the area of contact between said first part of the mould having needles and said resin impregnated fibre.
Claim 4
Dependent Claim
32 words
A method according to claim 2 in which said area of contact with said stripper plate is at least 5% greater than said area of contact with said first part having needles.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1995-06-30 | 1995-12-30 | 1996-06-30 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1999-06-30 | 1999-12-30 | 2000-06-30 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2003-06-30 | 2003-12-30 | 2004-06-30 | $7700.00 | Window Closed / Lapsed |