Inner cowl structure for aircraft turbine engine

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United States of America Patent

PATENT NO 9404507
APP PUB NO 20140319269A1
SERIAL NO

13862941

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An inner cowl structure for circumscribing at least a portion of a jet engine extending from an aircraft includes an apron configured to mount directly to the engine independent of the pylon and overly an upper portion of the jet engine, and an inner body configured to circumscribe a portion of the jet engine not circumscribed by the apron.

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Patent Owner(s)

Patent OwnerAddress
MRA SYSTEMS LLC103 CHESAPEAKE PARK PLAZA BALTIMORE MD 21220

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Janzon, Carol Marie Abingdon, US 2 14
Scarr, Antony Brett Bel Air, US 3 19
Weir, Thomas Joseph Lutherville, US 3 21
Woolley, Allen Madsen Rose Hill, US 4 40

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