A supporting structure arrangement for fastening an aircraft gas turbine engine to an aircraft, including: a supporting structural element of the aircraft engine and a supporting structure with at least one support and at least one bearing, by means of which the support can be connected or is connected to the aircraft, wherein the support can be connected or is connected rigidly to the supporting structural element of the aircraft engine by means of a connecting device.
INTEGRATED SUPPORT STRUCTURE FOR AN AIRCRAFT ENGINE AND ITS AUXILLARY COMPONENTS
2019-06-06
Patent
Electronic Resource
English
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