Engine nacelle acoustic panel with integral wedge fairings and an integral forward ring

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United States of America Patent

PATENT NO 6173807
SERIAL NO

09059797

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An acoustic panel (26) for the nacelle (20) of a high bypass jet engine. The acoustic panel (26) has a perforated composite inner sheet (54), an outer composite sheet (96, 98), and a honeycomb-core material (74) sandwiched therebetween. The acoustic panel (26) includes an integral forward ring (36) and integral wedge fairings (44).

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Patent Owner(s)

Patent OwnerAddress
BANK OF AMERICA N A AS COLLATERAL AGENT101 SOUTH TRYON STREET NC1-002-15-36 CHARLOTTE NC 28255

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Kitt, Brian R Wichita, KS 5 91
Popp, Thomas D Wichita, KS 8 145
Stratton, Terry W Rose Hill, KS 2 53
Welch, John M Wichita, KS 25 493
Wikstrom, Robert F Derby, KS 2 53

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