An apparatus includes a strain relief formed in helical shape and formed with a U-shaped channel. The strain relief can be used around a cable of a component or a spool extension of a fiber tray.

An apparatus includes a strain relief formed in helical shape and formed with a U-shaped channel. The strain relief can be used around a cable of a component or a spool extension of a fiber tray.

Disclosed is an anti-vibration device. An anti-vibration device according to the embodiment of the present disclosure reduces vibration between an object and an installation surface on which the object is installed, and the anti-vibration device includes a first elastic member, a first support member disposed to cover the first elastic member and fastened to the first elastic member, a second elastic member disposed on an upper portion of the first support member, and a second support member disposed to cover the second elastic member and fastened to the first support member.

Disclosed is an anti-vibration device. An anti-vibration device according to the embodiment of the present disclosure reduces vibration between an object and an installation surface on which the object is installed, and the anti-vibration device includes a first elastic member, a first support member disposed to cover the first elastic member and fastened to the first elastic member, a second elastic member disposed on an upper portion of the first support member, and a second support member disposed to cover the second elastic member and fastened to the first support member.

A projection exposure apparatus has a vibration damper with a holder and a mass that is connected to the holder via a damping element. The vibration damper comprises a temperature control device for the temperature control of the damping element. The disclosure also relates to a method for designing a vibration damper.

An isolation system and method are disclosed. The isolation system includes a beam that includes a first end and a second end. The isolation system may include at least one clamping block comprising first elastomeric material, and the first end may be coupled with the first elastomeric material by the at least one clamping block. An end condition of the buckling beam may be varied based on compression stiffening of the first elastomeric material.

An isolation system and method are disclosed. The isolation system includes a beam that includes a first end and a second end. The isolation system may include at least one clamping block comprising first elastomeric material, and the first end may be coupled with the first elastomeric material by the at least one clamping block. An end condition of the buckling beam may be varied based on compression stiffening of the first elastomeric material.

A cutting machining apparatus includes a rectangular box-shaped housing as a whole, a base member fixed to the housing via a cushioning member, a workpiece holder disposed inside the housing to be apart from the housing, fixed to the base member, and holding a workpiece, and a machining unit disposed inside the housing to be apart from the housing, fixed to the base member, and machining the workpiece.

An isolator assembly is configured for damping vibrations of a sensor deployed outside of an aircraft. The isolator assembly includes a platform configured for mechanically supporting the sensor, a lift mechanism configured to raise and lower the platform for stowing the sensor inside the aircraft and deploying the sensor outside the aircraft, and a plate secured inside the aircraft beneath the platform. The plate includes a through-hole for the sensor to extend through. A pin extends below the platform and an isolator mount is disposed on a top side of the plate. The isolator mount includes a slot configured to receive the pin upon deploying the sensor outside the aircraft. The platform and the plate are configured to stabilize the sensor and the isolator assembly is configured to damp vibrations imparted on the sensor by the airstream during flight.

An isolator assembly is configured for damping vibrations of a sensor deployed outside of an aircraft. The isolator assembly includes a platform configured for mechanically supporting the sensor, a lift mechanism configured to raise and lower the platform for stowing the sensor inside the aircraft and deploying the sensor outside the aircraft, and a plate secured inside the aircraft beneath the platform. The plate includes a through-hole for the sensor to extend through. A pin extends below the platform and an isolator mount is disposed on a top side of the plate. The isolator mount includes a slot configured to receive the pin upon deploying the sensor outside the aircraft. The platform and the plate are configured to stabilize the sensor and the isolator assembly is configured to damp vibrations imparted on the sensor by the airstream during flight.