A damper includes an upper connector configured to be connected to a cable. The damper also includes a lower connector configured to be connected to a load. The damper also includes a body extending between and connecting together the upper and lower connectors. The body includes a first portion and a second portion. The first portion is configured to experience greater plastic strain than the second portion.

A damping device is described that is designed to counter the transmission of vibrations to a further element and comprises: a beam element, which extends mainly parallel to an axis, is constrained to the further element and is designed to flexurally oscillate, in use, in a plane parallel to the axis to counter the transmission of vibrations to the further element; an actuator, which comprises a transmission element operatively connected to the beam element and extending mainly along the axis; the actuator being controllable to apply a direct tensile or compressive load along the axis on the transmission element that is variable according to the frequency of the vibrations to be dampened.

In the spring mechanism, the negative spring mechanism biasing the loading plate to the positive side in the z-direction has the spring shaft and interspring. The spring shaft is rotatably connected to the fixed part and is connected through the slider with respect to the loading plate so that it can rotate and can move in the x-direction. The connection part with the loading plate is positioned on the positive side in the z-direction and on the positive side in the x-direction relative to the connection part with the fixed part. An elastic force countering the compression is generated by the spring shaft. The interspring is connected to the loading plate and is connected through the slider to the spring shaft. It generates an elastic force countering the displacement to the positive side in the x-direction of the connection part of the spring shaft with the loading plate.

A bearing element (1) for mounting a component, especially a cooling module, with an elastomeric element (12), the elastomeric element (12) having an inner connection (6) for connecting to a bearing pin (7) of the component to be mounted, an outer connection (8) for connecting to a bearing frame (10), and at least one support arm (14), which extends between the inner connection (6) and outer connection (8) and elastically connects these together, with a force transfer surface (16) of the outer connection (8) to the bearing frame (10) formed by an outer end face of the support arm (10), and the bearing element (1) formed such that, in the event of an elastic displacement of the inner connection (6) relative to the outer connection (8) in a predetermined, radial displacement direction relative to the bearing element (1) the support arm (14) is stressed predominantly by thrust.

A cylindrically rolled energy absorber (10) is provided to absorb the energy of a user's fall from a worksite and includes a strip (18) of bi-layered webbing defining two parallel rolls (22, 24) of webbing centered on a central axis (40), with the width of the strip (18) in each roll (22, 24) extending parallel to the central axis (40). The strip (18) includes two layers (42, 44) of webbing joined together over the length of the strip by tear-apart connections (46). Each end (36, 38) of the strip (18) has end portions (54, 56) of each the layers (42, 44) that are separated from each other. A first connector loop (26) extends from the roll (22) and is fixed to a first end portion (54, 56) from end (36) of the strip and to a second end portion (54, 56) from the other end (38) of the strip (18). A second connector loop (28) extends from the other roll (24) and is fixed to a third end portion (54, 56) from the end (36) of the strip (18) and to a fourth end portion (54, 56) from the other end (38) of the strip (18).

A vibration damper including a frame having at least a first cavity, a frame first end and a frame second end spaced from the frame first end; a shaft slidably coupled to and extending into the frame where the shaft extends through the first cavity; a first vibration isolator disposed within the first cavity where the shaft extends through the first vibration isolator so as to capture the first vibration isolator within the first cavity where the first vibration isolator interfaces with the frame second end; and a second vibration isolator disposed on the shaft, where the shaft extends through the second vibration isolator so as to capture the second vibration isolator on the shaft where the second vibration isolator interfaces with the frame second end opposite the first vibration isolator, where the first vibration isolator and the second vibration isolator act only in compression.

A device (1) comprises: a cylindrical shell (4); a first spring (5) encased inside the cylindrical shell (4); a second spring (6) encased inside the cylindrical shell (4); a separator (13) in the cylindrical shell (4) separating the first and second springs (5, 6); a first end plate (12) on a first side (13a) of the separator (13) and a second end plate (11) on a second side (13b) of the separator (13); a first rod (2) and a second rod (3) passing openings (20a, 20b) provided at each end of the cylindrical shell (4), with the first rod (2) connected to the first end plate (12) and the second rod (3) connected to the second end plate (11); and a spacer (14) inserted between the first end plate (12) and the first spring (5).

There is described an aircraft configured to be able to hover, comprising a fuselage; and a support element adapted to support a load, made of elastically deformable material and constrained to said fuselage; the support element being movable in an operating position in which it is arranged at least partially outside said fuselage and supports said load; the aircraft comprises a sock surrounding the support element arranged in said operating position; the sock is configured to contain the elastic return of the support element, in case the support element arranged in said operating position is sheared off.

A method includes coupling a damper to a cable and a load, and moving the damper, the cable, the load, or a combination thereof. In response to the movement, slack is introduced into the cable, and the slack is suddenly released, which exerts a tensile load on the damper and the cable. The damper is configured to dampen the tensile load exerted on the cable.

A device for isolating shock and vibration transmitted to an audio device, such as a microphone, the device including a frame, a shock isolation assembly adapted to receive a bottom end of the microphone, a top suspension adapted to elastically suspend at least a partial section of the microphone, and a bottom suspension adapted to suspend the shock isolation assembly.