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US Patent 10005545 Aircraft wing rib

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Patent abstract

There is disclosed an aircraft wing rib comprising a structural rib section to which a wing skin can be attached; and a suction conduit to which, in use, a negative pressure can be applied so as to cause air to be drawn through suction holes provided in the outer surface of the wing skin. There is also disclosed an aircraft wing including such a wing rib.

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Patent Inventor Names
James Alderman0
Jonathan Meyer0
Stephen Rolston0
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Patent Citations Received
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US Patent 11565795 Vertical tail unit for flow control
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US Patent 11433990 Active laminar flow control system with composite panel
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US Patent 11040769 Leading edge structure for a flow control system of an aircraft
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US Patent 10974817 Vertical tail unit for flow control
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US Patent 10967955 Vertical tail unit for flow control
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 US Patent 10005545 Aircraft wing rib

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
10005545
Date of patent
June 26, 2018
Patent application number
14964032
Date Filed
December 9, 2015
Patent primary examiner
‌
Timothy D Collins

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