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US 2019/0168883 A1Published application
Integrated support structure for an aircraft engine and its auxillary components
AssigneeRolls-Royce Deutschland Ltd & Co KG
InventorCarsten BUCHHOLZ
Life of this patent
Estimating the term…
Abstract
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.
Claims14
A supporting structure arrangement for fastening an aircraft gas turbine engine to an aircraft, comprising:
- 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.
Dependencies are inferred from the claim text.