An elastic device is disposed on the second end, a fixing end of the elastic device is fixed on the second end, and an elastic end of the elastic device contacts the body.

However, the biaser (40) may be any elastic or non-elastic device to facilitate erection of collapsed dunnage (24).

An elastic device is accommodated in the housing.

The resilient device may exert a second force.

An elastic device is located close by the gap.

The spring device contains a fluid-encapsulating member (63).

Elastic means (10) link said body portions so that said body portions are biased towards each other when said elastic means is stretched to separate the body portions.

The torsionally-elastic device (28) is axially offset with regard to the automatically-disengaging torque transmission device.

The rear side plate (23) is equipped with an elastic device (30).

The spacecraft lands base first on a resilient landing device (300).

The holding clamp 1 has a pressure spring device 12 between both hooks 6, 7; the pressure spring device induces a spring force F to at least a portion of a jacket area 13 of the curler 2.

To this end, the spring device comprises a rubber spring element (1310; 1320) or a number of rubber spring elements (1310; 1320).

Said device includes a resilient device (6) and/or a permanently installed electric, pneumatic and/or hydraulic actuator.

Disclosed is an elastic and sticky hair-dusting device, comprising an elastic roller (1), an elastic duster frame (2), a handle (3) and sticky hair strips (4).

A spring device (26) strives to force the reversing member (16) into one of the two positions.