A STRUCTURE FOR TRANSFERRING LOADS AT A GAS TURBINE ENGINE, AND AN ENGINE AND AN AIRCRAFT WITH SUCH A STRUCTURE

摘要

The invention relates to a structure for transferring loads in a gas turbine engine (1), and/or between a gas turbine engine (1) and an airframe (2). The structure comprises a collapsible element (513), and is adapted to operate in a first mode, and to operate, upon a collapse of the collapsible element (513), in a second mode, in which the stiffness of the structure is lower than in the first mode.