Patent classifications
D07B2205/2042
Small Diameter, High Strength, Low Elongation, Creep Resistant, Abrasion Resistant Braided Structure
A braided structure that includes a core and a sheath is provided. The core includes a yarn formed at least in part from an aromatic polymer (e.g., an aromatic polyester/liquid crystalline polymer or an aramid polymer), and the sheath, which includes a plurality of ultra high molecular weight polyolefin yarns, is braided around the core. The sheath has an overall diameter ranging from about 60 micrometers to about 650 micrometers. Despite its small diameter, the braided structure can be creep resistant and abrasion resistant while at the same time exhibiting low elongation, a high load at break, and high stiffness. The braided structure can be used in medical applications such as sutures, load bearing orthopedic applications, artificial tendons/ligaments, fixation devices, actuation cables, components for tissue repair, etc.
ROPE MADE OF TEXTILE FIBRE MATERIAL
The invention relates to a rope (1) made of textile fibre material, which is characterized by the combination of features whereby
a) the load-bearing fibre material of the rope (1) consists of high-strength synthetic fibres
b) the rope (1) is in the form of a spiral strand rope
c) the rope (1) has at least two, preferably at least three concentric load-bearing strand layers (3,4,5)
d) the individual strands (7,8,9,10,11,12) of the strand layers (3,4,5) are movable with respect to one another
e) the degree of filling of the rope (1) with textile fibre material is ≧75%, preferably ≧85%
f) the outermost ply (5,6) of the rope has a coefficient of frictionμ with respect to steel of μ<0.15.
ROPE MADE OF TEXTILE FIBRE MATERIAL
The invention relates to a rope (1) made of textile fibre material, which is characterized by the combination of features whereby
a) the load-bearing fibre material of the rope (1) consists of high-strength synthetic fibres
b) the rope (1) is in the form of a spiral strand rope
c) the rope (1) has at least two, preferably at least three concentric load-bearing strand layers (3,4,5)
d) the individual strands (7,8,9,10,11,12) of the strand layers (3,4,5) are movable with respect to one another
e) the degree of filling of the rope (1) with textile fibre material is ≧75%, preferably ≧85%
f) the outermost ply (5,6) of the rope has a coefficient of frictionμ with respect to steel of μ<0.15.
TOW CABLE
A tow cable for a decoy on a fast jet aircraft is described. The tow cable has a composite structure with a high friction fibre outer containment braiding, and low friction fibre internal strength members. Additional to these internal fibres may be electrical conductors and optical fibres. The whole composite providing a tow cable with high towing endurance and reliable in-flight performance, for flight profiles including high performance manoeuvres and in-flight refuelling.
TOW CABLE
A tow cable for a decoy on a fast jet aircraft is described. The tow cable has a composite structure with a high friction fibre outer containment braiding, and low friction fibre internal strength members. Additional to these internal fibres may be electrical conductors and optical fibres. The whole composite providing a tow cable with high towing endurance and reliable in-flight performance, for flight profiles including high performance manoeuvres and in-flight refuelling.
Tension member for elevator system belt
A belt for an elevator system includes a plurality of tension members arranged along a belt width and extending longitudinally along a length of the belt, each tension member including a plurality of load carrying fibers, the plurality of load carrying fibers including a plurality of aromatic polyester based fibers. A jacket material at least partially encapsulates the plurality of tension members.
Tension member for elevator system belt
A belt for an elevator system includes a plurality of tension members arranged along a belt width and extending longitudinally along a length of the belt, each tension member including a plurality of load carrying fibers, the plurality of load carrying fibers including a plurality of aromatic polyester based fibers. A jacket material at least partially encapsulates the plurality of tension members.
Small diameter, high strength, low elongation, creep resistant, abrasion resistant braided structure
A braided structure that includes a core and a sheath is provided. The core includes a yarn formed at least in part from an aromatic polymer (e.g., an aromatic polyester/liquid crystalline polymer or an aramid polymer), and the sheath, which includes a plurality of ultra high molecular weight polyolefin yarns, is braided around the core. The sheath has an overall diameter ranging from about 60 micrometers to about 650 micrometers. Despite its small diameter, the braided structure can be creep resistant and abrasion resistant while at the same time exhibiting low elongation, a high load at break, and high stiffness. The braided structure can be used in medical applications such as sutures, load bearing orthopedic applications, artificial tendons/ligaments, fixation devices, actuation cables, components for tissue repair, etc.
Synthetic fiber rope
A synthetic fiber rope comprising:—a core, said core being a laid or braided synthetic fiber strand,—a polymer layer, said polymer layer covering said core,—a first layer, said first layer having at least six first synthetic fiber strands laid in a first direction surround said polymer layer, and—a second layer, said second layer having at least twelve second synthetic fiber strands laid in a second direction surround said first layer.
Synthetic fiber rope
A synthetic fiber rope comprising:—a core, said core being a laid or braided synthetic fiber strand,—a polymer layer, said polymer layer covering said core,—a first layer, said first layer having at least six first synthetic fiber strands laid in a first direction surround said polymer layer, and—a second layer, said second layer having at least twelve second synthetic fiber strands laid in a second direction surround said first layer.