Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
11/2005
11/02/2005EP1578663A3 Perforated skin structure for laminar-flow systems
11/02/2005EP1286807B1 Apparatus for grinding/polishing a curved or flat wall element
11/01/2005US6959894 Impact resistant structure for the helicopter and energy absorber used for the same
10/2005
10/27/2005WO2005100802A1 Connecting element
10/27/2005WO2005100152A1 Fairing for an aircraft structure
10/27/2005US20050236524 Airfoil box and associated method
10/27/2005US20050236523 Internal arrangement of the walls of the fuselage of an aircraft
10/27/2005US20050236522 Device for heating lock elements in aircraft
10/27/2005US20050236521 Securing apparatus for a portable electronic unit
10/27/2005US20050235565 Device for actuating the doors of vehicles
10/27/2005CA2561787A1 Connecting element
10/27/2005CA2560978A1 Fairing for an aircraft structure
10/26/2005EP1588941A2 Heating device for locking elements in aircraft
10/26/2005EP1587734A1 Aircraft with forward opening inlay spoilers for yaw control
10/26/2005EP1349777B1 Composite beam with integrated break-off initiator and aircraft fuselage incorporating such beams
10/26/2005EP1311426B1 Composite material support structures with sinusoidal webs and method of fabricating same
10/26/2005EP1010615B1 A process for making a dismountable and/or fixed traction-compression joint to be applied to composite materials
10/25/2005US6957792 Lifting arrangement for aircraft fuselages
10/20/2005WO2005066526A3 Apparatus and method for sealing surfaces
10/20/2005US20050230550 Cockpit security door/restroom
10/20/2005US20050230548 Safety system and method for a serial passenger seat power bus
10/20/2005US20050230547 Aircraft drainmast assembly
10/20/2005US20050230546 Airflow control devices based on active materials
10/20/2005US20050230544 Arrangement for coating interior trim components in passenger aircraft while complying with relevant fire protection standards and at the same time improving thermal comfort
10/20/2005US20050230543 Power strip for seats
10/20/2005US20050230540 Integrated transport system for overhead stowage
10/20/2005US20050230538 Fuselage spar for aircraft and central sparbox provided with such a spar
10/20/2005US20050230535 Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea
10/20/2005US20050230521 Powerchute apparatus
10/19/2005EP1586501A1 Cabin liner coating
10/19/2005EP1585664A2 Single piece co-cure composite wing
10/19/2005CN1223490C Safety landing system of falling helicopter
10/13/2005WO2005095209A1 Support device for a galley
10/13/2005WO2005095206A1 Foam composite insulation for aircraft
10/13/2005WO2005095205A1 Adaptable payload enabling architecture
10/13/2005US20050224657 Force feedback refueling system for unmanned aircraft
10/13/2005US20050224656 Methods and systems for removing material from aircraft flight surfaces
10/13/2005US20050224655 Method for making a laminated structure and aircraft provided with such a structure
10/13/2005US20050224653 Cushioned grounding clamp
10/13/2005US20050224651 Apparatus for attachment of a unit to attachment devices in a vehicle
10/13/2005US20050224650 Adaptable payload processes
10/13/2005US20050224649 Catch device of cockpit door
10/13/2005US20050224648 Adaptable payload apparatus and methods
10/13/2005US20050224647 Insulating baffle for a floor shear truss
10/13/2005US20050224646 Overhead space access conversion monument and service area staircase and stowage system
10/13/2005US20050224645 Cargo deck
10/13/2005US20050224644 Support roller arrangement for use in an aircraft cargo hold
10/13/2005US20050224640 Methods for incorporating area rules surfaces in a supersonic aircraft
10/13/2005US20050224637 Self extinguishing composite primary structure
10/13/2005DE102004013966A1 Aktives Element zur Schwingungsreduktion von Bauteilen, insbesondere für Flugzeugkomponenten, sowie Verfahren zur aktiven Schwingungsreduktion An active element for vibration reduction of components, particularly for aircraft components, and methods for active vibration reduction
10/13/2005DE102004011182A1 Clamp support for holding and guiding electrical cable bundle, has wedge arranged at position between basic unit and structural component, when basic unit is clamped with structural component, to reflect dimension of structural component
10/12/2005EP1584896A1 Passive measurement of terrain parameters
10/12/2005EP1583690A2 Laminar flow wing for transonic cruise
10/06/2005WO2005093285A1 Active element for reducing the vibrations of components, in particular aircraft components and method for actively reducing vibrations
10/06/2005US20050218267 Method for determination of fuselage shape of supersonic aircraft, and fuselage front section shape
10/06/2005US20050218266 Avionic door lock system
10/06/2005US20050218265 An integrated transport system and method for overhead stowage and retrieval
10/06/2005DE102004016219B3 Cargo deck for cargo hold of aircraft has several mounting profiles which when viewed over width of cargo hold have identical spacings with identical components fitting accurately between them
10/06/2005DE102004013878A1 Vorrichtung zur Befestigung einer Einheit an Befestigungseinrichtungen eines Fahrzeugs Device for fastening of a unit to a vehicle attachment means
10/04/2005US6951322 Personal aircraft device
10/04/2005US6951321 Efficient cargo liner installation
10/04/2005US6951320 Lock mechanism for securing a door kinematics system and process of operating same
10/04/2005US6951319 Flexible hydraulic latch
10/04/2005US6951162 Penetration-and fire resistant fabric materials and structures
09/2005
09/29/2005WO2005090799A1 Signal activated fastener array
09/29/2005WO2005090798A1 Fastener networks
09/29/2005WO2005077755A9 Cargo-hold floor for aircraft
09/29/2005US20050216141 Apparatus and method for reducing induced drag on aircraft and other vehicles
09/29/2005US20050216139 Method and apparatus for facilitating information, security and transaction exchange in aviation
09/29/2005US20050216138 Airplane emergency navigational system
09/29/2005US20050211846 Stiffener stop with staggered slopes and panel fitted with such a stop
09/29/2005US20050211844 Seat rail for aircraft cabin and method of manufacturing such a rail
09/29/2005US20050211843 Method of assembling a single piece co-cured structure
09/29/2005US20050211841 Aircraft interior architecture
09/29/2005US20050211840 Adaptable payload enabling architecture
09/29/2005US20050211838 Foam composite insulation for aircraft
09/29/2005US20050211836 Payload to support track interface and fitting apparatus and methods
09/29/2005US20050211833 Non-protruding seat track apparatus and methods
09/29/2005US20050210820 Frame and method for fabricating the same
09/29/2005DE102004012262A1 Mounting plate e.g. for galley fitting in airplane, has arrangement having horizontal surface assigning thread with horizontal surface has recess where mounting plate covers thread for screwing into thread of arrangement
09/29/2005DE102004011183A1 Aircraft electrical cable mount, has two sections made of plastic, and connecting unit supporting plate-shaped unit, where both units are made up of more heat resistant or fire-resistant material
09/29/2005CA2560091A1 Fastener networks
09/29/2005CA2560090A1 Signal activated fastener array
09/28/2005EP1580858A2 Cable holder
09/28/2005EP1580122A2 Cargo deck
09/28/2005EP1580121A2 Cargo rollers and their use
09/28/2005EP1578663A2 Perforated skin structure for laminar-flow systems
09/28/2005EP1305209B1 Structural element for an aircraft, especially an aircraft door
09/28/2005CN1675391A Al-Cu-Mg-Si alloy and method for producing the same
09/27/2005US6948684 Composite beam with integrated rupture initiator and aircraft fuselage including such beams
09/22/2005US20050205716 Stealth craft
09/22/2005DE102004009967A1 Cable holder for aircraft, has separable cable holder module that is arranged on base element mounted on aircraft structure by inserting pins into corresponding recesses in structure
09/21/2005EP1578182A2 Fastening device for portable electronic unit
09/21/2005EP1577214A2 Catch device of a cockpit door
09/21/2005EP1577211A2 Aircraft unit fastening arrangement
09/21/2005EP1577084A1 Laminated plastic glazing for vehicles
09/21/2005EP1576248A2 Pressure responsive blowout latch with reservoir
09/20/2005US6946642 Optical window assembly for use in a supersonic platform
09/20/2005US6945727 Apparatuses and methods for joining structural members, such as composite structural members
09/20/2005US6945497 Cockpit door of aircraft
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