JET ENGINE WITH A RADIALLY VARIABLE WALL
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United States of America
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Feb 22, 2018
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Feb 22, 2018
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Abstract
A jet engine having a flow duct that is arranged in an engine nacelle and is delimited radially on the inside by a central body and radially on the outside by an outer nozzle wall is described. The free cross section of the flow duct is variable by an elastically embodied, radially variable wall of at least one of these components. The radially variable wall at least regionally has an at least approximately wavelike structure and is connected to at least one adjusting device having an adjusting unit. The variable wall of one of these components is variable in a radial direction at two defined control sections, at least one of which defines an axial wall end of the radially variable wall.
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