Compliant crown panel for an aircraft

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8434716
APP PUB NO 20110101164A1
SERIAL NO

12965451

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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An aircraft forward pressure bulkhead and an aircraft crown panel are described herein. The forward pressure bulkhead includes a malleable and deformable dome that is configured to “catch” foreign objects, such as birds. The dome is intentionally designed to deform in response to a foreign object strike that imparts at least a threshold amount of impact energy to the bulkhead. The dome is free of rigid stiffeners and non-deformable reinforcement members that would otherwise hinder the flexible characteristic of the dome. Practical embodiments of the bulkhead utilize fewer parts, are less heavy, and are less expensive than traditional bulkheads that utilize rigid stiffeners. The crown panel has similar compliant characteristics. The crown panel is designed to simultaneously deform and deflect in response to foreign object impacts such as birds and hail. The crown panel is formed from a monolithic one-piece material, such as aluminum, and various reinforcing features are integrally formed in the material.

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Patent Owner(s)

Patent OwnerAddress
THE BOEING COMPANYARLINGTON VA

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Koch, William J Bellevue, US 15 309
Matheson, Donald P Redmond, US 13 535

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