D07B2205/2014

Rope made of textile fiber material, comprising a twine of excess length
20220074136 · 2022-03-10 ·

The invention relates to a rope made of textile fiber material, comprising a rope core and a sheath surrounding the rope core, wherein the sheath, an intermediate sheath located between the sheath and the rope core and/or a reinforcement located between the sheath and the rope core comprise(s) a twine of excess length, the twine of excess length being formed in that it comprises at least a first yarn and a second yarn which are twisted together, the first yarn having a greater length than the second yarn, measured in an untwisted state of a unit length of the twine. In a further aspect, the invention relates to a method of manufacturing a twine of excess length for the above-mentioned rope.

Aircraft fuselage and structural cable for aircraft fuselage

A wide body aircraft is discussed having a fuselage with a first structural element, a second structural element, a wide-body fuselage section, and a plurality of tension members. Each of the first structural element and the second structural element may be arranged to traverse a longitudinal length of the wide-body fuselage section. The wide-body fuselage section may comprise a set of side-by-side fuselage subassemblies, where the set of side-by-side fuselage subassemblies can be coupled to one another via the first structural element and the second structural element. The plurality of tension members can be arranged to manage tension between the first structural element and the second structural element. The plurality of tension members can be configured to remain flexible under a compression load, while managing tension therebetween.

Aircraft fuselage and structural cable for aircraft fuselage

A wide body aircraft is discussed having a fuselage with a first structural element, a second structural element, a wide-body fuselage section, and a plurality of tension members. Each of the first structural element and the second structural element may be arranged to traverse a longitudinal length of the wide-body fuselage section. The wide-body fuselage section may comprise a set of side-by-side fuselage subassemblies, where the set of side-by-side fuselage subassemblies can be coupled to one another via the first structural element and the second structural element. The plurality of tension members can be arranged to manage tension between the first structural element and the second structural element. The plurality of tension members can be configured to remain flexible under a compression load, while managing tension therebetween.

Fibre Rope and Hoisting System Including Such a Fibre Rope

There is described a hoisting system and method of lifting that make use of a particular fibre rope. The fibre rope includes a plurality of magnets that are embedded within the fibre rope and spaced apart along the rope with a known axial distance between the magnets. The system may include a fibre rope hoisting speed sensor, and a magnetic field sensor that can sense the presence of the magnetic field of the embedded magnets. Using the sensors, the hoisting speed of the rope may be determined by: measuring the time between the passing of consecutive magnets by using the magnetic field sensor; calculating the distance between consecutive magnets using the hoisting speed sensor and the measured time between the passing of the consecutive magnets; and comparing the calculated distance between the magnets with an original, predefined distance between the magnets.

Fibre Rope and Hoisting System Including Such a Fibre Rope

There is described a hoisting system and method of lifting that make use of a particular fibre rope. The fibre rope includes a plurality of magnets that are embedded within the fibre rope and spaced apart along the rope with a known axial distance between the magnets. The system may include a fibre rope hoisting speed sensor, and a magnetic field sensor that can sense the presence of the magnetic field of the embedded magnets. Using the sensors, the hoisting speed of the rope may be determined by: measuring the time between the passing of consecutive magnets by using the magnetic field sensor; calculating the distance between consecutive magnets using the hoisting speed sensor and the measured time between the passing of the consecutive magnets; and comparing the calculated distance between the magnets with an original, predefined distance between the magnets.

SLING
20210238013 · 2021-08-05 ·

The disclosure provides a sling including a sleeve, a first eye formed by a first splice, and a second eye formed by a second splice. The sleeve includes braided strands and has a first end portion, a second end portion, and an intermediate portion between. The sleeve also defines a hollow inner volume. The first splice is made by the first end portion extending into and along part of the hollow inner volume proximate the first eye. The second splice is made by the second end portion extending into and along part of the hollow inner volume proximate the second eye. A hollow load bearing portion is defined in the intermediate portion between the first splice and the second splice.

SLING
20210238013 · 2021-08-05 ·

The disclosure provides a sling including a sleeve, a first eye formed by a first splice, and a second eye formed by a second splice. The sleeve includes braided strands and has a first end portion, a second end portion, and an intermediate portion between. The sleeve also defines a hollow inner volume. The first splice is made by the first end portion extending into and along part of the hollow inner volume proximate the first eye. The second splice is made by the second end portion extending into and along part of the hollow inner volume proximate the second eye. A hollow load bearing portion is defined in the intermediate portion between the first splice and the second splice.

DEVICE FOR ADJUSTING THE DISCARD STATE DETECTION OF HIGH-STRENGTH FIBER ROPES AND LIFTING GEAR COMPRISING SUCH A DEVICE

The present invention generally relates to the detection of the discard state of high-strength fiber ropes. The invention relates to a device for detecting the discard state of high-strength fiber ropes for various operating conditions, wherein a rope core of the fiber rope is sheathed with a rope sheath which is intended to wear more quickly than the rope core, comprising an optical detection device for detecting the rope surface and/or a load spectrum counter for detecting the load cycles to which the fiber rope is subjected, and on the other hand to a lifting gear such as a crane comprising such a device. According to the invention, there is provided a detection device for detecting the light absorption coefficient and/or the degree of reflection of the rope sheath and an adaptation device for adapting the algorithm, by means of which the discard state is determined, in dependence on the detected light absorption coefficient and/or the detected degree of reflection.

HYBRID HOISTING CABLE, METHOD OF FORMING THE SAME, AND WINCH USING SUCH A CABLE
20210156085 · 2021-05-27 ·

The invention concerns a hoisting cable formed of a steel core coated at its periphery with a textile sheath, wherein said textile sheath is a sheath directly braided on the steel core and made of an abrasion-resistant synthetic material.

HYBRID HOISTING CABLE, METHOD OF FORMING THE SAME, AND WINCH USING SUCH A CABLE
20210156085 · 2021-05-27 ·

The invention concerns a hoisting cable formed of a steel core coated at its periphery with a textile sheath, wherein said textile sheath is a sheath directly braided on the steel core and made of an abrasion-resistant synthetic material.