Device for testing load of fuselage barrel in air travel and space travel, comprises two pressure bulkheads for pressure tight locking of fuselage barrel at their front sides

摘要

The device (1) comprises two pressure bulkheads (8,9) for a pressure tight locking of a fuselage barrel (2) at their front sides (10,11). A carrier unit (15) is provided, which is coupled on one side with the former pressure bulkhead and on the other side with the latter pressure bulkhead extending through the fuselage barrel. A tensioning unit (23,24) is provided, which is coupled on one side with the carrier unit and on the other side with a section (5,7) of the fuselage barrel for introducing load into the fuselage barrel.