Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
05/2002
05/02/2002EP0927313B1 Vibration isolation insert for aircraft floor panels and the like
05/02/2002EP0854821B1 Hybrid aircraft
05/01/2002CN1083899C Net form article of aluminium alloys contg. beryllium and investment casting method and use thereof
04/2002
04/30/2002US6378806 Aircraft door structure
04/30/2002US6378805 Pressure frame designed in particular for an aircraft
04/30/2002US6378803 Aircraft lift arrangement
04/25/2002WO2002032763A1 Sound-proofing panel, in particular a rotorcraft structural or lining panel
04/25/2002WO2001096094A3 Conformable locating aperture system and method for alignment of members
04/25/2002US20020047070 Method and apparatus for aircraft inlet ice protection
04/24/2002CN1083553C Three-dimensionally reinforced ablative/insulative composite
04/23/2002US6375122 Reinforced elastomer panel
04/23/2002US6375121 Method for making a composite panel and resulting panel
04/23/2002US6375120 Method and apparatus for building a metal/composite hybrid airplane component
04/23/2002US6374570 Apparatus and method for joining dissimilar materials to form a structural support member
04/18/2002WO2002030745A1 Bottom discharge drainmast for an aircraft
04/18/2002WO2002030743A1 Aircraft provided with carrying fuselage
04/18/2002US20020046371 Random-access multi-directional CDMA2000 turbo code interleaver
04/18/2002US20020043807 Safety enhancement method and apparatus
04/18/2002US20020043588 Skin of an airplane door and method of making door with same
04/18/2002DE10102146C1 Making composite strip for vehicle internal trim comprises press-bonding partial second- and bonding layers to first layer and substrate, finishing irregularities with a plastic lacquer and surface coating
04/17/2002EP1197669A1 Insert intended for the fixing of a device and methods for realization and fixing of this insert
04/17/2002EP1196325A2 Monolithic structure with redundant load paths
04/16/2002US6372072 Composite laminate manufacture with multiaxial fabrics
04/16/2002US6371411 Method and apparatus for aircraft inlet ice protection
04/12/2002CA2346253A1 Wing spar modification kit
04/11/2002WO2002028709A1 Composite skin panel opening edge and method for manufacture
04/11/2002CA2423665A1 Composite skin panel opening edge and method for manufacture
04/10/2002CN1082438C Sandwich panel made of composite material and prodn. method
04/09/2002US6367200 Quick release and fastening cover
04/04/2002WO2002026559A1 Drainmast with integral electronic temperature control
04/04/2002US20020039664 0.6-1.15 wt. % silicon, 0.6-1.0 wt. % copper, 0.8-1.2 wt. % magnesium, 0.55-0.86 wt. % zinc, less than 0.1 wt. % manganese, 0.2-0.3 wt. % chromium, the balance aluminum, incidental elements and impurities.
04/03/2002EP1193088A1 Viewing aid for doors and windows
04/03/2002CN1342619A Glass for sealed cabin of space environment or polar region
04/03/2002CN1082003C Latch-lock mechanism for load carring airplane cargo doors
04/02/2002US6364250 Shell component for an aircraft fuselage and method of manufacturing the same
03/2002
03/28/2002DE10046568A1 Flugzeugtürfenster eines Verkehrsflugzeuges Aircraft door window of a commercial aircraft
03/27/2002EP1189808A1 Grooved profile for diverting liquid
03/21/2002US20020033433 Window with a lens for an aircraft door
03/21/2002DE10042413A1 Kabinenfensteranordnung für ein Flugzeug Cabin window assembly for an aircraft
03/20/2002EP1188665A1 Pallet system and method for loading freight on an aircraft
03/20/2002EP1188664A2 Aircraft door window
03/20/2002EP1188547A1 Sound absorbing multi-layered panel
03/20/2002EP1187762A1 Laminar flow control system and suction panel for use therewith
03/20/2002EP1187761A1 Improved fire-blocking insulation blanket and method for attaching same
03/19/2002US6358591 Fire-blocking insulation blanket
03/14/2002WO2002020248A1 Stiffening means for structural components, method of manufacturing and apparatus therefor
03/14/2002US20020030136 Years two thousand of new safety helicopter
03/14/2002DE10041458A1 Sound absorber with microperforations over surface, used for cladding in aircraft, vehicle or ship, is made from porous material, e.g. fiber-reinforced magnesia or melamine resin
03/13/2002EP1186531A2 Aircraft decompression panel assembly
03/12/2002US6355337 Structural element of high unidirectional rigidity
03/12/2002US6355133 Forming reinforcing components
03/07/2002WO2002018203A1 Cabin window arrangement for an aeroplane
03/07/2002US20020028332 Wavy composite tubular structures
03/07/2002US20020027997 Structure and method of absorbing and shielding sound
02/2002
02/28/2002WO2002016784A2 Apparatus and method for joining dissimilar materials to form a structural support member
02/28/2002WO2002016197A1 Composite material support structures with sinusoidal webs and method of fabricating same
02/28/2002US20020025242 Non-removable structural threaded fastener with threads of lesser outer diameter than the shank and method of forming same
02/28/2002CA2418646A1 Composite material support structures with sinusoidal webs and method of fabricating same
02/26/2002CA2020932C High-capacity fuselage for aircraft
02/21/2002US20020021016 Vehicle seat arrangement
02/21/2002DE10056994C1 Aircraft passenger door opening and closing control method has all or individual function steps controlled by door control unit switched between mechanical or electromechanical control mode
02/21/2002DE10040058A1 Device for securing of loads on transporting vehicle has extended safety component anchored in locking unit by retaining element which comprises at least one locking cam and at least one safety cam
02/21/2002DE10037621A1 Steuerung für eine Passagiertür eines Flugzeuges Control for a passenger door of an aircraft
02/21/2002DE10037307A1 Strukturelement für ein Flugzeug, insbesondere Flugzeugtür Structural element for an aircraft, in particular aircraft door
02/14/2002US20020017592 Method and device for improving the thermal comfort in passenger airplanes
02/14/2002US20020017590 Burn through resistant systems for transportation, especially aircraft
02/14/2002US20020017414 Collapsible panel and method for controlled collapsing thereof
02/13/2002EP1179465A2 Device for securing of loads on a transport vehicle
02/07/2002WO2002010013A1 Structural element for an aircraft, especially an aircraft door
02/07/2002WO2001047771A3 Severance of polycarbonates with linear shaped charge
02/07/2002US20020015631 Non-removable structural threaded fastener with threads of lesser outer diameter than the shank and method of forming same (div. 1)
02/07/2002US20020015630 Non-removable structural threaded fastener with threads of lesser outer diameter than the shank and method of forming same (div. 3)
02/07/2002US20020014557 Control for a passenger door of an aircraft
02/07/2002US20020014101 Process for the monolithic molding of superplastic material
02/07/2002DE10035334A1 Außenhaut einer Flugzeugtür Outer skin of an aircraft door
02/07/2002DE10035301A1 Klimaanlagenaufhängung für ein Großraum-Verkehrsflugzeug Air Conditioning suspension for a widebody airliner
02/07/2002DE10034990A1 Multilaminar board to reduce sound propagation has slots in core layer distributed in a pattern over bottom or top surface, to which they are perpendicular
02/06/2002EP1177975A2 Aircraft door control sytem
02/06/2002EP1177564A1 Materials and composites activable into a state of enhanced conductivity
02/05/2002US6343452 Tubular frame
02/05/2002CA2100428C Fuselage structure for helicopter
01/2002
01/31/2002US20020012578 Reduced weight aircraft collar and method of making same
01/31/2002US20020011541 Collapsible panel and method for controlled collapsing thereof
01/31/2002US20020011033 Building for containing human occupants in an adverse arctic or antarctic environment and structures for containing and protecting occupants in an adverse environment
01/30/2002EP1175333A1 Multiple glazed insulating unit, especially for an aircraft window, with electromagnetic armour
01/29/2002US6341748 Emergency exit system
01/25/2002CA2314518A1 Aircraft based sensing, detection, targeting, communications and response apparatus
01/24/2002US20020008179 Aircraft door
01/24/2002US20020008176 Suspension for air generation units in aircraft
01/23/2002EP1174337A2 Air conditioning device suspension for wide-body aircraft
01/23/2002EP1173679A1 Electrical terminal blind grounding stud
01/23/2002EP0877707A4 Aircraft based sensing, detection, targeting, communications and response apparatus
01/23/2002EP0800474B1 Hollow, integral asymmetrical metal structure such as an aircraft wing slat trailing edge and method of manufacture
01/22/2002US6340134 Wing combination for drag reduction, aircraft including such a wing, and a method of reducing the drag of an existing aircraft
01/22/2002CA2032225C Electrically heated glass
01/17/2002US20020005454 Liquid hydrogen stratospheric aircraft
01/17/2002DE10032851A1 Einrichtung zum elektrischen Betätigen einer Tür eines Luftfahrzeugs Means for electrically actuating a door of an aircraft
01/17/2002DE10031714A1 Dekompressionseinheit für den explosiven Luftdruckausgleich Decompression for the explosive air pressure equalization
01/17/2002DE10031510A1 Strukturbauteil für ein Flugzeug Structural component for an aircraft
01/16/2002EP1171342A1 Method of sealing a panel to an aircraft structure