Device for fastening a turboprop, preferably under an aircraft wing
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United States of America Patent
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Jul 2, 2013
Grant Date -
Jul 21, 2011
app pub date -
Jan 11, 2011
filing date -
Jan 15, 2010
priority date (Note) -
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Abstract
The present invention relates to an engine assembly for an aircraft comprising an attachment means, a turboprop on an attachment mast, this means including a plurality of front engine attachments (16) each having an engine vibration insulation system (20) including a housing (22), a stress transmitting member (24) extending along a first axis (26) parallel to an axis of rotation of the propeller and a hollow member (28) integrated in the housing and extending along a second axis (30) orthogonal to and intersecting the first axis. According to the invention, a support means for supporting the system (20) is formed by a plurality of clevises (32a, 32b) each having a middle plane parallel to its clevis heads, integrating one of the first and second axes and orthogonal to the other of said axes.
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