A tolerance compensation subassembly in the form of a tolerance compensation element or a tolerance compensation region to improve the production, maintenance and repair of aircraft. The tolerance compensation subassembly contains an actuator which is formed from an electro-active polymer so that the tolerance compensation subassembly is electrically switchable between a fixed state and a non-fixed state. As a result, automation of the assembly of aircraft components on each other can be enabled or facilitated.
TOLERANCE COMPENSATION SUBASSEMBLY, AIRCRAFT COMPONENT PROVIDED THEREWITH AND AIRCRAFT
29.10.2020
Patent
Elektronische Ressource
Englisch
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