Material for the fabrication of sails

• US 5,333,568 A
• Filed: 11/17/1992
• Issued: 08/02/1994
• Est. Priority Date: 11/17/1992
• Status: Expired due to Term

• Current Assignee: Cubic Tech Corporation (DSM-Firmenich AG)
• Original Assignee: America3 Foundation
• Inventors: Downs, Roland J., Meldner, Heiner
• Primary Examiner(s): BELL, JAMES J
• Application Number:
  US07/978,095
• Time in Patent Office: 623 Days
• Field of Search: 428/284, 428/902, 428/295, 428/297, 428/447, 428/109, 114/103
• US Class Current: 114/102.31
• CPC Class Codes: B29C 70/44 using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
• CPC Class Codes: B32B 2262/105 Ceramic fibres
• CPC Class Codes: B32B 2262/106 Carbon fibres, e.g. graphite fibres
• CPC Class Codes: B32B 2605/12 Ships
• CPC Class Codes: B32B 27/12 next to a fibrous or filamentary layer
• CPC Class Codes: B32B 27/36 comprising polyesters
• CPC Class Codes: B32B 5/12 characterised by the relative arrangement of fibres or filaments of different layers, e.g. the fibres or filaments being parallel or perpendicular to each other
• CPC Class Codes: B32B 5/26 another layer next to it also being fibrous or filamentary relative arrangement of fibres or filaments of different layers B32B5/12
• CPC Class Codes: B63H 9/067 Sails characterised by their construction or manufacturing process
• CPC Class Codes: B63H 9/0678 Laminated sails
• CPC Class Codes: Y10S 428/902 High modulus filament or fiber
• CPC Class Codes: Y10T 428/24058 including grain, strips, or filamentary elements in respective layers or components in angular relation
• CPC Class Codes: Y10T 428/24091 with additional layer[s]
• CPC Class Codes: Y10T 428/24099 On each side of strands or strand-portions
• CPC Class Codes: Y10T 428/249942 Fibers are aligned substantially parallel
• CPC Class Codes: Y10T 428/249945 Carbon or carbonaceous fiber
• CPC Class Codes: Y10T 428/31663 As siloxane, silicone or silane

Abstract

An improved reinforced laminate for use in sails or other flexible sheet or membrane applications utilizes a pull-truded thin lightweight reinforcing sheet of unidirectional extruded monofilaments in which the reinforcing sheet or sheets form one or more uni-tapes laminated to a polymer film such as Mylar, or other extended sheet of material. The monofilaments are uniformly embedded in the uni-tape via an elastomeric polymer matrix, with the reinforcing sheet, when incorporated into sails via lamination resulting in sails with reinforcing monofilaments having diameters 5 times less than conventional strands or threads. The use of small diameter monofilaments greatly increases the monofilament-over-monofilament crossover density, resulting in a dramatic increase in shear strength, and Youngs'"'"' Modulus, with an accompanying dramatic decrease in weight. In one embodiment the improvement in specific modulus over conventional sail laminates is about six-fold. For example, at only one-third the weight, stretch resistance is two times better. In a preferred embodiment, autoclaving is used in the lamination process to rid the laminate of voids which dramatically reduce shear strength by as much as 30 percent. Alternative void-free laminating processes include a silicone interliner/heated platen technique.

Claims

1. A sail comprising:

a number of panels of material, each panel comprising

a laminate including a unitary film and crossed monofilaments in a flexible elastomeric polymer matrix bonded to said film, said panels together forming a sail having a head, a tack and a clew.

2. The sail of claim 1, wherein said monofilaments have a diameter less than 20 microns.

3. The sail of claim 2, wherein said monofilaments are on centers such that the crossover density of the crossed monofilaments is on the order of 1/4.

4. The sail of claim 1, wherein said reinforcing means includes a number of uni-tapes, each including monofilaments aligned in a single direction in said flexible elastomeric polymer matrix.

5. The sail of claim 4, wherein each of said uni-tapes is made by a process including pull-trusion so as to produce tow.

6. The sail of claim 5, wherein the monofilaments of each of said tows are etched prior to pull-trusion.

7. The sail of claim 6, wherein said etching step is selected from the group of steps consisting of plasma arc etching, corona discharge etching and chemical etching.

8. The sail of claim 4, wherein each of said uni-tapes is made by the process of passing side-by-side tows carrying extruded monofilaments through a resin and then through a fixed gap rotary die which marries the side-by-side tows together to produce a unidirectional tape having a lateral extent corresponding to the sum of the widths of the side-by-side spread tows, and having a thickness commensurate with the diameter of the monofilaments therein, said monofilaments being elongated when pulled through the fixed gap rotary die to improve the strength thereof.

9. The sail of claim 8, wherein said process includes the step of heat treating the uni-tape after it passes through said die.

10. The sail of claim 1, wherein at least some of said monofilaments are carbon.

11. The sail of claim 1, wherein said monofilaments include carbon monofilaments and organic polymer monofilaments.

12. The sail of claim 11, wherein the polymer for said monofilaments is selected from the group consisting of ordered polymers such as aramids, liquid crystals, extended chain polyethylenes and polyesters, nylons and engineering thermoplastics.

13. The sail of claim 1, wherein said monofilaments include carbon monofilaments and monofilaments of inorganic material.

14. The sail of claim 13, wherein the inorganic material for said monofilaments is selected from the group consisting of silicon, boron, carbon and ceramic.

15. The sail of claim 1, wherein said laminate is formed by the process of autoclaving, including the application of pressure and heat to the laminate, said autoclaving removing any voids in the resulting material.

16. The sail of claim 15, wherein said autoclaving process includes the steps of providing the laminate between two supports and providing a silicone layer between one of said supports and the laminate, whereby when said laminate is formed in said autoclaving process, the heat associated with the autoclaving process causes the silicone to expand to put uniform increased pressure on the laminate for ridding the laminate of voids.