US2006225376A1PendingUtilityA1

Reinforcement assembly for matrix materials

Assignee: COMPOSHIELD ASPriority: Jun 21, 2003Filed: Jun 17, 2004Published: Oct 12, 2006
Est. expiryJun 21, 2023(expired)· nominal 20-yr term from priority
E04C 5/07F41H 5/0492E04C 5/04E04C 5/162E04C 5/064
24
PatentIndex Score
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Claims

Abstract

An assembly of interlaced rods, suitable for use as embedded reinforcement in matrix materials, comprising first, second and third layers of rods, the rods of each layer being orientated generally parallel to one another, the second layer being located between the first and third layers, the rods of the first and third layers being longitudinally orientated in the same direction, with those of the second layer being longitudinally orientated generally at right angles thereto, the rods of the first and third layers being paired such that each nth rod of the first layer, herein designated rod n 1 , is paired with the nth rod of the third layer, herein designated rod n 3 , paired rods of the first and third layers being drawn together under tension by a flexible filament wound between them in a series of runs each comprising a forward and reverse sinusoidal winding which interlaces rods of the first and third layers, whereby each pair of rods n 1 and n 3 in the first and third layers is enclosed by and drawn together by a loop of filament formed by the forward and reverse winding patterns.

Claims

exact text as granted — not AI-modified
1 . An assembly of interlaced rods, suitable for use as embedded reinforcement in matrix materials, comprising first, second and third layers of rods, 
 the rods of each layer being orientated generally parallel to one another,    the second layer being located between the first and third layers,    the rods of the first and third layers being longitudinally orientated in the same direction, with those of the second layer being longitudinally orientated generally at right angles thereto,    the rods of the first and third layers being paired such that each nth rod of the first layer, herein designated rod n 1 , is paired with the nth rod of the third layer, herein designated rod n 3 ,    paired rods of the first and third layers being drawn together under tension by a flexible filament wound between them in a series of runs spaced along the length of the rods of the first and third layers, each such run extending transversely to the longitudinal orientation of the rods,    rods of the second layer being located generally parallel to and between adjacent transverse runs of filament,    each such transverse run of filament comprising a forward and reverse sinusoidal winding which interlaces rods of the first and third layers,    the forward sinusoidal winding following the pattern: rod  1   1 → 2   3 → 3   1 → 4   3 → . . . and then continuing in the reverse sinusoidal winding pattern: . . .  4   1 → 3   3 → 2   1 → 1   3 , whereby each pair of rods n 1  and n 3  in the first and third layers is enclosed by and drawn together by a loop of filament formed by the forward and reverse winding patterns.    
   
   
       2 . A rod assembly as claimed in  claim 1  wherein a single rod of the second layer is located between any adjacent pair of transverse runs of filament.  
   
   
       3 . A rod assembly as claimed in  claim 1  wherein more than one rod of the second layer is located between at least one adjacent pair of transverse runs of filament.  
   
   
       4 . A rod assembly as claimed in  claim 1  wherein each transverse run is formed by one continuously wound filament.  
   
   
       5 . A rod assembly as claimed in  claim 1  wherein all the transverse runs are formed by one and the same continuously wound filament.  
   
   
       6 . A rod assembly as claimed in  claim 1  wherein the filament is in the form of a wire, a monofilament, or a multifilament string or rope.  
   
   
       7 . A rod assembly as claimed in  claim 1  wherein the filament comprises carbon fibre.  
   
   
       8 . A rod assembly as claimed in  claim 1  wherein at least some of the rods are of steel or of fibre-filled resin.  
   
   
       9 . A rod assembly as claimed in  claim 1  wherein at least some of the rods are of glass fibre-filled resin.  
   
   
       10 . A rod assembly as claimed in  claim 1  which is embedded in matrix material.  
   
   
       11 . A rod assembly embedded in matrix material as claimed in  claim 10  wherein the matrix material is a synthetic polymer.  
   
   
       12 . A rod assembly embedded in matrix material as claimed in  claim 10  wherein the matrix material has additional plate or rod reinforcement embedded or partially therein in spaced or contiguous layered relationship to the rod assembly.  
   
   
       13 . A rod assembly embedded in matrix material as claimed in  claim 10  wherein the matrix has a flexible sheet material embedded or partially embedded therein in spaced or contiguous layered relationship to the rod assembly.  
   
   
       14 . A rod assembly embedded in matrix material as claimed in  claim 13  wherein the flexible sheet material is a woven mat of aramid fibre.  
   
   
       15 . A rod assembly embedded in matrix material as claimed in  claim 10  which is laminated as a backing to blast- or ballistic impact-resistant armour.  
   
   
       16 . A rod assembly embedded in matrix material as claimed in  claim 10  which is laminated as a backing to blast- or ballistic impact-resistant armour comprising contiguous cells filled with matrix material.  
   
   
       17 . A rod assembly embedded in matrix material as claimed in  claim 10  which is laminated to a backing mass which crushes or deforms progressively under impact.  
   
   
       18 . A rod assembly embedded in matrix material as claimed in  claim 17  wherein the backing mass is a cellular or foamed material.  
   
   
       19 . A rod assembly embedded in matrix material as claimed in  claim 12  which is in the form of a shaped article.  
   
   
       20 . A rod assembly embedded in matrix material as claimed in  claim 10  which is in the form of a panel.

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