Loading patent…
AssigneesRolls-Royce Deutschland Ltd & Co KG, Liebherr-Aerospace Lindenberg GmbH
InventorsPredrag TODOROVIC, Josef BAER, Frank MUELLER, Uwe SCHUMANN
Estimating the term…
The present invention relates to an aircraft gas turbine comprising a thrust-reverser device that is arranged at the rear area of an engine cowling and that has multiple cascade elements which are distributed at the circumference and which divert a stream, characterized in that the cascade elements are mounted in a displaceable manner, in that on both sides of each cascade element at least one gear rack is formed that can be displaced via a respective cog wheel which is coupled to a driving device, and in that each cascade element is connected to a rear area of the engine cowling via a coupling element for the purpose of displacing the engine cowling in the axial direction.
Aircraft gas turbine comprising a thrust-reverser device that is arranged at the rear area of an engine cowling and that comprises multiple cascade elements that are distributed at the circumference and that divert a stream, characterized in that the cascade elements are mounted in a displaceable manner, in that on both sides of each cascade element at least one gear rack is formed which can be displaced via a respective pinion that is coupled to a driving device, and in that each cascade element is connected to a rear area of the engine cowling via at least one coupling element for the purpose of displacing the engine cowling in the axial direction.
Dependencies are inferred from the claim text.