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Class Information
Number: 244/123.13
Name: Aeronautics > Aircraft structure > Airfoil construction > Honeycomb in skin panels
Description: Subject matter in which the outermost layer of the airfoil is formed of a structure having interconnected hollow, thin-walled, substantially parallel cells.










Patents under this class:

Patent Number Title Of Patent Date Issued
8607924 Anchoring of septums in acoustic honeycomb Dec. 17, 2013
8490365 Aircraft side fairing Jul. 23, 2013
8491743 Composite ply stabilizing method Jul. 23, 2013
8418962 Distribution of point loads in honeycomb panels Apr. 16, 2013
8262024 Aircraft frames Sep. 11, 2012
8245972 Leading edge for aircraft wings and empennages Aug. 21, 2012
8066222 Energy absorbing impact band Nov. 29, 2011
7866605 Energy absorbing impact band and method Jan. 11, 2011
7628358 Wing panel structure Dec. 8, 2009
7510757 Cellular composite grid-stiffened structure Mar. 31, 2009
7338694 Method for an integral composite forward flange in a composite Mar. 4, 2008
6405978 Double-walled panel Jun. 18, 2002
4667905 High strength to weight horizontal and vertical aircraft stabilizer May. 26, 1987
4565595 Method of making composite aircraft wing Jan. 21, 1986
4411380 Metal matrix composite structural panel construction Oct. 25, 1983
4395450 Composite structural skin spar joint and method of making Jul. 26, 1983
4310132 Fuselage structure using advanced technology fiber reinforced composites Jan. 12, 1982
4206895 Loop-tension joint Jun. 10, 1980











 
 
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