Alignment and safety device for the cowls of aircraft engine nacelles
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United States of America Patent
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Jan 30, 2018
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N/A
app pub date -
Sep 29, 2015
filing date -
Sep 29, 2014
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Abstract
The disclosure herein provides an alignment and safety device for the cowls of the nacelle of an aircraft engine formed by first and second parts to be arranged opposite of each other at the lower edges of the cowls that include first and second alignment arms configured with a portion arranged to enter inside the inner space of the nacelle covered by the opposite cowl. One of the parts includes a blocking member configured to be interposed between the cowls after being unlatched to facilitate their opening operation and also when they return to the closed position from an open position if they are misaligned to facilitate its alignment and subsequent latching applying a force F on the blocking member.
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