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US Patent 11926410 Drag recovery scheme for nacelles

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Patent abstractTimelineTable: Further ResourcesReferences
Is a
Patent
Patent
1

Patent attributes

Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
1
Patent Number
119264101
Patent Inventor Names
Mark A. Page1
Brendan Kennelly1
John Winkler1
Date of Patent
March 12, 2024
1
Patent Application Number
167265421
Date Filed
December 24, 2019
1
Patent Citations
‌
US Patent 9540113 De-couple geared turbo-fan engine and aircraft
1
‌
US Patent 10850859 Aircraft with a propulsion unit with offset fan
1
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US Patent 7752834 Aircraft propulsion systems
1
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US Patent 9650954 Gas turbine engine with distributed fans
1
Patent Primary Examiner
‌
Joshua J Michener
1
CPC Code
‌
B64C 2039/105
1
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B64C 39/10
1
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B64C 21/06
1
Patent abstract

Technologies are described herein for a drag recovery scheme. In various examples, a recovery engine is placed within a vortex flow of air caused by the impingement of air upon a nacelle of a main engine. The propeller of the recovery engine can use the vortex flow of air to provide additional thrust the aircraft, thus reducing the load on the main engines or providing an increased velocity.

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