Aeronautics and astronautics – Aircraft structure – Fuselage and body construction
Patent
1995-12-22
1999-04-13
Grant, William
Aeronautics and astronautics
Aircraft structure
Fuselage and body construction
244131, 2940215, 298971, 298972, B64C 110
Patent
active
058935347
ABSTRACT:
The problem solved by this invention is to eliminate an oil can movement of the web of an aircraft pressurized bulkhead. A hat section support stiffener is attached to the web by an adhesive. Two end brackets are attached by Hi-Loc bolts to bulkhead stiffeners and the end brackets are attached and arranged to provide a downward pressure on the hat section stiffener to assist in holding it in place. This invention is characterized by the absence of any new fasteners passing through the fatigue critical bulkhead web and also is characterized by the absence of any requirement for removal of existing fasteners, including, but not limited to those passing through the bulkhead web.
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Donahue Bernard A.
Grant William
The Boeing Company
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