http://rdf.ncbi.nlm.nih.gov/pubchem/patent/ES-2396328-A1

Outgoing Links

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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C1-06
filingDate 2010-06-30^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9092242b03beed118aa9f2f657dee9d3
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publicationDate 2013-02-20^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber ES-2396328-A1
titleOfInvention AIRCRAFT FUSELAGE IN COMPOSITE MATERIAL AND PROCEDURES FOR MANUFACTURING.
abstract Aircraft fuselage in composite material and manufacturing procedures. The fuselage structure (11) comprises a lining (13), a plurality of frames (17) disposed transversely to the longitudinal axis (9) of the fuselage (11) and a plurality of longitudinal stiffening elements that can be stringers (14) or beams (15), the relationship between the passage (X) of frames (17) and the passage (Y) of longitudinal stiffening elements (14, 15) being smaller in the unit. If the stiffeners are stringers (14), the manufacturing process is based on assembling the fuselage (11) joining the lining (13) with the stringers (14) to the frames (17). If the stiffeners are beams (14), the manufacturing process is based on the joining of the lining (13) to an internal structure formed by frames (17) and beams (15).
priorityDate 2010-06-30^^<http://www.w3.org/2001/XMLSchema#date>
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