ALENIA AERONAUTICA S.P.A.

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Patent Activity in the Last 10 Years

Technologies

Intl Class Technology Matters Rank in Class
 
  
 
B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM9148
 
  
 
B29C SHAPING OR JOINING OF PLASTICS; SHAPING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL; AFTER- TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING 8117
 
  
 
B64C AEROPLANES; HELICOPTERS 569
 
  
 
B29K INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS 130
 
  
 
B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES 125
 
  
 
B31B MAKING BOXES, CARTONS, ENVELOPES, OR BAGS 126
 
  
 
B60L ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL 175
 
  
 
B64D EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS167
 
  
 
C08G MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING CARBON-TO-CARBON UNSATURATED BONDS 1119
 
  
 
C08K USE OF INORGANIC OR NON-MACROMOLECULAR ORGANIC SUBSTANCES AS COMPOUNDING INGREDIENTS 1101

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Recent Publications

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Recent Patents

Patent # Title Filing Date Issue Date Intl Class
8980152 Method of manufacturing an integral profile monolithic wing structureJun 30, 08Mar 17, 15[B29C, B29K, B64C, B29L]
8869631 Method for detecting the thickness of the walls of hollow manufactured bodies made from non-ferromagnetic materialNov 08, 11Oct 28, 14[G01L, G01B]
8860586 Test arrangement for a laser threats identifying system of an aircraftSep 08, 09Oct 14, 14[G08B, F41H, G01S]
8815044 Method of manufacturing spars, longerons and fuselage beams having a variable H cross-sectionMar 03, 11Aug 26, 14[B32B]
8712608 System and method of automatic piloting for in-flight refuelling of aircraft, and aircraft comprising said systemDec 15, 10Apr 29, 14[G06F, G01C]
8706447 Procedure for the prognostic of a structure subject to loadsDec 04, 09Apr 22, 14[G21C]
8505697 Brake system for aircraft undercarriageFeb 16, 11Aug 13, 13[F16D, B60L]
8485467 Air intake, in particular for an aircraft chaff dispenserFeb 24, 09Jul 16, 13[B64D]
8479591 Apparatus for testing fuselage panelsDec 21, 09Jul 09, 13[G01M, G01N]
8481615 Process for preparing self-healing composite materials of high efficiency for structural applicationsNov 11, 10Jul 09, 13[C08G, B32B]

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Expired/Abandoned/Withdrawn Patents

Patent # Title Status Filing Date Issue/Pub Date Intl Class
2010/0170,637 PRE-IMPREGNATED MATERIAL WITH SEMI-CRYSTALLINE MATRIX AND AMORPHOUS SURFACE LAYERAbandonedFeb 04, 08Jul 08, 10[B32B]
2009/0314,893 Door Structure for a Compartment in the Fuselage or Wing of an AircraftAbandonedFeb 06, 09Dec 24, 09[B64D, B64C]
2009/0277,996 Wing and empennage leading edge structure made of thermoplastic material with a stiffened double shell configurationAbandonedMay 05, 09Nov 12, 09[B29C, B64C]
2006/0011,289 Method of manufacturing composite structural beams for aircraftAbandonedJun 16, 05Jan 19, 06[B29C]
2005/0257,847 Multi-layer duct for air distribution in air conditioning systems for vehicles, in particular aircrafts, and an element for fixing the duct to the structure of an aircraftAbandonedMay 24, 04Nov 24, 05[F16L]
2005/0211,082 Fabrics, tows of continuous filaments and strands for forming layers of reinforcement for a composite element with a resin matrixAbandonedMar 17, 05Sep 29, 05[D03D, D04C, G02B, D02G]
2003/0168,555 Methods of manufacturing a stiffening element for an aircraft skin panel and a skin panel provided with the stiffening elementAbandonedJan 22, 03Sep 11, 03[B64C]
2002/0157,961 Anodizing process, with low environmental impact, for a woodpiece of aluminum or aluminum alloysAbandonedFeb 19, 02Oct 31, 02[C25D]

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