AIRCRAFT GAS TURBINE COMPRISING AN ENGINE COWLING WITH A THRUST-REVERSER DEVICE

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20150176527A1
SERIAL NO

14575597

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Abstract

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The present invention relates to an aircraft gas turbine comprising an engine cowling that has a rear area, with respect to the direction of the flow, which has a thrust-reverser device, wherein the rear area is embodied in such a manner as to be translatable in the axial direction, characterized in that the rear area is mounted in a translatable manner at two rails that are arranged in parallel to each other, and that it comprises a gear rack that is mounted at each rail, respectively, with the gear rack being in mesh with a respective cog wheel, which is coupled to a common motor via a gear unit, respectively.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE DEUTSCHLAND LTD & CO KGESCHENWEG 11 OT DAHLEWITZ 15827 BLANKENFELDE-MAHLOW 15827
LIEBHERR-AEROSPACE LINDENBERG GMBH88161 LINDENBERG/ALLGÄU

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
METZLER-STOERMER, Dirk Oberreute, DE 1 0
MUELLER, Frank Lindenberg/Allgaeu, DE 93 602
SCHUMANN, Uwe Tettnang, DE 21 179
TODOROVIC, Predrag Berlin, DE 49 152

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