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Rib for blended wing-body aircraftStructural ribs for providing structural support for a structure, such as the pressure cabin of a blended-wing body aircraft. In a first embodiment, the ribs are generally Y-shaped, being comprised of a vertical web and a pair of inclined webs attached to the vertical web to extend upwardly and outwardly from the vertical web in different directions, with only the upper edges of the inclined webs being attached to a structural element. In a second embodiment, the ribs are generally trident-shaped, whereby the vertical web extends upwardly beyond the intersection of the inclined webs with the vertical web, with the upper edge of the vertical web as well as the upper edges of the inclined webs being attached to the same structural element.
Document ID
20080004535
Acquisition Source
Langley Research Center
Document Type
Other - Patent
Authors
Hawley, Arthur V.
Date Acquired
August 24, 2013
Publication Date
April 13, 1999
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-878628
Patent Number: US-PATENT-5,893,535
Funding Number(s)
CONTRACT_GRANT: NAS1-8673
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,893,535
Patent Application
US-PATENT-APPL-SN-878628
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