Aircraft with a fuselage accommodating an unducted turbine engine

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United States of America Patent

PATENT NO 12030652
APP PUB NO 20230399114A1
SERIAL NO

17835280

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Abstract

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An aircraft comprising a fuselage and an unducted turbine engine. The fuselage having a divot with an upstream edge and a downstream edge. The divot is defined by a straight reference line having a length (L) and a maximum depth (h) relative to the straight reference line. The unducted turbine engine having an engine core, a nacelle, and a set of blades. A first flow ratio (FR1) is equal to:

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Patent Owner(s)

  • GENERAL ELECTRIC COMPANY

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Blodgett, Keith Edward James Milford, US 11 124
Bowden, William J Cleves, US 3 0
Geertsema, Egbert Cincinnati, US 11 46

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