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Rutan Fiberglass Cloths
Uni-Directional
Bi-Directional
FREE Shipping
Overview
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Note: 38" wide. Sold by the yard The most basic structural material in building a composite aircraft is glass cloth. The use of glass in aircraft structures, particularly structural sandwich composites, is a recent development. Glass cloth is available commercially in hundreds of different weights, weaves, strengths and working properties. Very few of these, however, are compatible with aircraft requirements for high strength and light weight. Even fewer are suitable for the hand-layup techniques developed by Burt Rutan for the homebuilder. The glass cloth featured here has been specifically selected for the optimum combination of workability, strength and weight. Two types of glass cloth, a bi-directional cloth and a uni-directional cloth are used. BID cloth has half of the fibers woven parallel to the selvage edge of the cloth and the other half at right angles to the selvage, giving the cloth the same strength in both directions. UND cloth has 95% of the glass fibers woven parallel to the selvage, giving exceptional strength in that direction and very little at right angles to it. BID is generally used for pieces which are cut at a 45° angle to the selvage, a bias cut, which enables the builder to lay BID into contours with very little effort and provides the needed shear and torsion stiffness for flying surfaces. UND is used in areas where the primary loads are in one direction, such as wing skins and spar caps. Multiple layers of glass cloth are laminated together to form the aircraft structure. Each layer of cloth is called a "ply". |
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WARNING: Cancer and Reproductive Harm - www.P65Warnings.ca.gov. |
Specifications
Uni-Directional:- 7 oz 38" Width Threads per inch
- Construction: 80 Warp Tow Count X 18 Fill Tow Count
Bi-Directional:
- 8.8 oz 38" Width Threads per inch
- Construction: 54 Warp Tow Count X 48 Fill Tow Count
Reviews
Cloth for Fiberglass repairs, I like to keep some on hand.
Verified Purchase
Bid Fiberglass 38 RA7725/38W F16
Great material to work with
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Bid Fiberglass 38 RA7725/38W F16
No wonder this is the standard. Drapes just right and wets out easily with aeropoxy
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Bid Fiberglass 38 RA7725/38W F16
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Bid Fiberglass 38 RA7725/38W F16
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Uni. Fiberglass RA7715/38W F16
Now to get into the build. Thanks Aircraft Spruce
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Bid Fiberglass 38 RA7725/38W F16
Excellent product, very well wrapped and shipped
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Bid Fiberglass 38 RA7725/38W F16
Got it on time
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Bid Fiberglass 38 RA7725/38W F16
Verified Purchase
Uni. Fiberglass RA7715/38W F16
BID, hey, it is what it is. Order was filled and sent promptly, rolled, sealed in plastic, and outer wrapped in paper.
Verified Purchase
Bid Fiberglass 38 RA7725/38W F16
Q&A
Please note, Aircraft Spruce's personnel are not certified aircraft mechanics and can only provide general support and ideas, which should not be relied upon or implemented in lieu of consulting an A&P or other qualified technician. Aircraft Spruce assumes no responsibility or liability for any issue or problem which may arise from any repair, modification or other work done from this knowledge base. Any product eligibility information provided here is based on general application guides and we recommend always referring to your specific aircraft parts manual, the parts manufacturer or consulting with a qualified mechanic.
You can buy by the roll. The roll is approximately 125 yards. 15 percent discount kicks in at 500 yards.
The thickness of the unidirectional cloth (01-00641) is 0.19 mm. The thickness of the bidirectional cloth (01-00642) is 0.23 mm.
The thickness of the unidirectional cloth (01-00641) is 0.19 mm. The thickness of the bidirectional cloth (01-00642) is 0.23 mm.
The uni (p/n 01-00641) is approximately 7.0 oz / yd. The bid (p/n 01-00642) is approximately 8.8 oz / yd.
Part number 01-00642 is 8.8 oz/yd. The breaking strength of P/N# 01-00642 is warp- 440 lbf/in,Filling- 366 lbf/in. P/N# 01-00641 is warp- 650 lbf/in, 70 lbf/in.
This is uni-directional E-Glass.
You can use Aeropxy Strucural Adhesive Part # 01-00295.
