Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
09/2006
09/20/2006EP1701882A1 Insulation arrangement for the internal insulation of a vehicle
09/20/2006EP1701881A2 Aircraft fuselage
09/20/2006EP1701880A1 Panel arrangement for an interior lining of a passenger cabin in an aircraft
09/20/2006EP1701867A2 Insulation structure for the internal insulation of a vehicle
09/20/2006EP1453726B1 Method and system for producing a potential over a body
09/19/2006US7108230 Aircraft with topside only spoilers
09/19/2006US7108228 Hydrogen-fueled spacecraft
09/19/2006US7108227 Insulation package and use thereof
09/19/2006US7108224 Aircraft engine rear suspension with thrust recovery
09/14/2006WO2006095018A1 Aircraft structural element provided with a cavity and drainage element
09/14/2006WO2006036214A3 Vtol aircraft external load drag reduction system
09/14/2006WO2006025855A3 Self extinguishing composite primary structure
09/14/2006US20060202508 Airflow control devices based on active materials
09/14/2006US20060202088 Apparatus and method for air-to-air arming of aerial vehicles
09/14/2006US20060202087 Aircraft door hinge assembly
09/14/2006US20060202086 Fairing and installation methodology for sensor pressure belts
09/14/2006US20060202085 Arrangement of a first and a second furnishing
09/14/2006DE102005011531A1 Strukturelement eines Flugzeugs mit einem Hohlraum Structural element of an aircraft with a cavity
09/13/2006EP1699689A1 Device and method for floor heating in an aircraft
09/13/2006EP1567774B1 Method for assembling sealed components
09/13/2006CN1832883A Surface temperature control system
09/13/2006CN1274430C Device for processing a metal slab or billet, and product produced using said device
09/08/2006WO2006071207A3 Dynamic cmg array and method
09/08/2006WO2005010410A3 Composite seal and window assembly
09/07/2006DE102005008443A1 Ladevorrichtung zum zumindest teilautomatischen Beladen und Entladen eines Frachtraums eines Verkehrsmittels sowie Fördereinrichtung Loading device for at least partially automatic loading and unloading of a cargo compartment of a means of transport and conveyor
09/06/2006EP1697212A2 Dynamic cmg array and method
09/06/2006EP1697210A2 Systems and methods for configuring aircraft to meet performance goals and shock wave disturbance constraints
09/06/2006EP1395489A4 Anti-torque and yaw-control system for a rotary-wing aircraft
09/06/2006CN1829812A High-damage tolerant aluminium alloy product in particular for aerospace applications
09/05/2006US7100885 Seat mounting rail, particularly for a commercial aircraft
09/05/2006US7100871 Lightweight structural component made of metallic ply materials
09/05/2006US7100827 Aircraft cargo loading logistics system
08/2006
08/31/2006WO2006091217A1 In-flight refueling system, alignment system, and method for automatic alignment and engagement of an in-flight refueling boom
08/31/2006WO2006072749A3 Improvement to aircraft cabin doors
08/31/2006US20060192051 Reconfigurable interior sidewall
08/31/2006DE102005008479A1 Resin-Transfer-Molding-device for manufacturing component comprises trough, cover that can be attached to trough, and heating device for manufacturing component by heating starting material that can be enclosed between trough and cover
08/30/2006EP1694560A2 Area ruling for supersonic vehicles
08/30/2006EP1414890B1 Surface-modified methyl methacrylate polymer based transparent sheet material
08/30/2006CN1826451A Contact stiffeners for structural skins
08/29/2006US7099753 Automatic generation of telemetry flight software, accompanying specifications, and decode files
08/29/2006US7099752 Safelander
08/29/2006US7097136 Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea
08/24/2006WO2006087778A1 Method of surface treatment for titanium alloy member of aerospace instrument
08/24/2006US20060188355 Apparatus for attaching a hitch to a vehicle
08/24/2006US20060186271 Loading device for the at least partially automated loading and unloading of a cargo hold on transport equipment as well as a conveying system
08/24/2006US20060186270 Door for aircraft, and aircraft provided with such a door
08/24/2006DE102005007308A1 Ball mat for transport of freight containers in cargo hold of aircraft has cover and base plate which are connected to each other by ball element support and distance pots
08/24/2006DE102005007058A1 Arrangement of pipe connectors for components in airplane passenger cabin, has pipe connector element which is provided for intake of several pipe connectors
08/24/2006DE10020825B4 Verfahren und Vorrichtung zum Schliessen einer Tür eines Flugzeuges Method and apparatus for closing a door of an aircraft
08/24/2006CA2597266A1 Surface treatment method of titanium alloy member for aerospace equipment
08/23/2006EP1467909B1 Joint for connecting components together on opposite longitudinal sides in addition to a flexible strip used for said joint
08/22/2006US7093805 System and methods for integrating a payload with a launch vehicle
08/22/2006US7093798 Transformable airplane
08/22/2006US7093797 Adaptable payload apparatus and methods
08/22/2006US7093470 Methods of making integrally stiffened axial load carrying skin panels for primary aircraft structure and fuel tank structures
08/17/2006US20060182650 Al-Zn-Mg-Cu alloys and products with high mechanical characteristics and structural members suitable for aeronautical construction made thereof
08/17/2006US20060180706 Method for seizing an object
08/17/2006US20060180705 Brazed structural assembly and associated system and method for manufacture
08/17/2006US20060180704 Mandrel segment loader
08/17/2006DE102005003518A1 Windschott zum Einsatz in Flugzeugen Wind deflector for use in aircraft
08/16/2006CN1819947A Single piece co-cure composite wing
08/15/2006US7090168 Catenary girt arrangement for emergency evacuation slides
08/15/2006US7090112 Method and sealant for joints
08/10/2006WO2006083314A2 Insulation process
08/10/2006WO2006057575A3 Lifting-type aeroplane fuselage
08/10/2006DE102005002546A1 Frame clamping device for longitudinal assembly of fuselage has connecting means for connecting device at first frame and fixing means is provided for force fitting and friction engaging fixing of first and second shell of fuselage
08/10/2006CA2842211A1 Cargo aircraft
08/10/2006CA2589813A1 Cargo aircraft
08/10/2006CA2572587A1 Insulation process
08/09/2006EP1687590A1 Perspective vertical situation display system and method
08/09/2006EP1196325B1 Monolithic structure with redundant load paths
08/09/2006CN1816476A Aircraft comprising a lift-generating fuselage
08/08/2006US7087317 Composite laminated aluminum-glass fiber sandwich panels
08/08/2006US7086815 Lashing device for tying a load in a transport conveyance
08/08/2006US7086629 Severance of polycarbonates and polycarbonate laminates with linear shaped charge
08/03/2006US20060169838 Method of enhancing the movement of dangerous goods
08/03/2006US20060169400 Methods for manufacturing composite aircraft, parts and a family of composite aircraft
08/02/2006EP1686056A2 Reinforced cover for openings in an aerodynamic contour
08/02/2006EP1685024A2 Aircraft
08/02/2006EP1685023A2 Architectural archway for an aircraft
08/02/2006EP1438473A4 Pressure sensing dead bolt
08/02/2006CN1812911A Perforated skin structure for laminar-flow systems
08/01/2006US7083437 Aircraft seat electrical quick disconnect
08/01/2006US7083147 Modularized insulation, systems, apparatus, and methods
07/2006
07/27/2006WO2006078651A1 Control surface assemblies with torque tube base
07/27/2006WO2006077111A1 Pressure-difference warning system
07/27/2006WO2006012716A3 A device for fastening passenger seats on a seat track break in an aircraft
07/27/2006US20060163432 Multi-servicing and retractable bridge for an operational ground support system
07/27/2006DE102005003297A1 Horizontal and vertical tails connecting barrel shaped fuselage rear section for e.g. transport plane, has horizontal tail section with end frames firmly connected with each other by torsion boxes and longitudinally reinforced braces
07/27/2006DE102005003296A1 Rear fuselage section for airfreighter, has vertical tail segment with end frames having reinforcement bars that are connected with nodal points of frames by space bars which are bent in course
07/27/2006DE102005003154A1 Cellular shaped box for aircraft`s fitting e.g. medical space, has upper part which contains cell cover whose height is adjusted, where upper part is pressed with elastic units on respective sealing to achieve full vertical height
07/27/2006DE102005002370A1 Strukturelement für ein Flugzeug Structural element for an aircraft
07/27/2006DE102004058013B3 Aircraft wing structure manufacturing method, involves forming elevating projections at surface of substrate layer, and forming one projection into integral profile-like reinforcing unit e.g. stringer, by deformation using one cylinder
07/25/2006US7080807 Window frame/seal assembly and method of forming the same
07/25/2006US7080806 Overhead space access conversion monument and service area staircase and stowage system
07/25/2006US7080805 Stiffened structures and associated methods
07/25/2006US7080441 Composite fuselage machine and method of automated composite lay up
07/20/2006US20060157621 Hatch-actuating mechanism, particularly for an aircraft landing gear
07/20/2006US20060157620 Baggage compartment in passenger transport system
07/20/2006US20060157613 Supersonic aircraft with active lift distribution control for reducing sonic boom
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