Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
09/2005
09/18/2005CA2461286A1 Frame and method for fabricating the same
09/15/2005WO2005085065A1 Static port skin applique apparatus and method
09/15/2005WO2005084156A2 Hydrogen powered aircraft
09/15/2005WO2005084152A2 Aircraft fuselage
09/15/2005WO2005065920A3 Method of making a window skin panel
09/15/2005WO2003089295A3 Perforated skin structure for laminar-flow systems
09/15/2005DE10330341B4 Metallischer Schichtwerkstoff, verstärkt mit langen Basaltfasern sowie dessen Erzeugnisse Metallic layer material, reinforced with long fibers of basalt and its products
09/15/2005DE102004020662B3 Emergency exit door locking unit heating device for aircraft, has sliding plate with recess to receive heating foil that is sandwiched between fabric mats, and hermetically sealed, where plate and recess are filled with fluid ceramic
09/15/2005DE102004009020A1 Strengthening frame for aircraft fuselage hatch or door surround has spars with cruciform cross section
09/15/2005CA2557946A1 Aircraft fuselage
09/13/2005US6943336 Optical window assembly for use in supersonic platform
09/13/2005US6942178 Mach weighted area ruling for supersonic vehicles
09/09/2005WO2005083647A1 Improvements in aircraft doors
09/09/2005CA2557512A1 Improvements in aircraft doors
09/08/2005US20050197748 Vehicle data services
09/08/2005US20050196121 Cable holder
09/08/2005DE202005010293U1 Force initiation element on struts of fiber composite material for applications in air travel consists of thermoplastic synthetic material reinforced by short or discontinuous long fibers
09/08/2005DE102004007018A1 Aircraft comprises a fuselage and/or inner elements consisting of a tear resistant material in the form of double-walled structures incorporating airtight inflatable chambers
09/08/2005DE102004006648A1 Frachtraumboden für Luftfahrzeuge Cargo compartment floor for aircraft
09/07/2005EP1571079A1 Fuselage longeron for an aircraft and a central wing box with such a longeron
09/07/2005EP1569846A1 Door which is intended to be positioned between the cockpit and the cabin of an aircraft
09/07/2005EP1569845A1 Aircraft door arrangement
09/07/2005EP1140625B1 Environment control system for aircraft having interior condensation problem reduction, cabin air quality improvement, fire suppression and fire venting functions
09/07/2005CN1665673A Method of assembling a single piece co-cured structure
09/06/2005US6938854 Integrated and/or modular high-speed aircraft
09/06/2005US6938448 Shaped metal panels and forming same by shot peening
09/06/2005US6938376 Door reinforcement system
09/04/2005CA2498251A1 Longeron for aircraft and centre-wing section equipped with such a longeron
09/01/2005US20050192398 high curvature; a PVB bleaching compound; having a low concentration of plasticizer; interlayer has a yellowness index (YID) color of less than about 12
09/01/2005DE102004003773A1 Luftfahrzeughüllenelement und Verfahren zur Aufnahme einer Anzahl von Bildern Aircraft shell element and method for recording a number of images
08/2005
08/31/2005EP1569058A1 Windowing machining method and system for non-developable thin panels
08/31/2005EP1567774A1 Assembly of sealed components
08/30/2005US6935594 co-cured nonmetallic composite part for use in environments having elevated temperatures comprising plurality of layers of nonmetallic materials, layers including material for structural support, second material formed from ceramics; missiles
08/30/2005CA2266663C Vibration isolation insert for aircraft floor panels and the like
08/25/2005WO2005077755A1 Cargo-hold floor for aircraft
08/25/2005US20050183376 Space truss structure surface slab assembly
08/25/2005US20050183260 Device for assembly of several elements by riveting and procedure for assembly of panels especially for aircraft fuselages by means of said device
08/25/2005DE10393136T5 Al-Cu-Mg-Si Legierung und Verfahren zur Herstellung derselben Al-Cu-Mg-Si alloy and process for producing same
08/25/2005DE102004057289A1 Isolationsaufbau zur Innenisolierung eines Luftfahrzeuges Insulation structure for the internal insulation of an aircraft
08/24/2005EP1566334A1 Stiffener end with staggered slopes and panel with such stiffener end
08/24/2005EP1565374A2 Forward restraint apparatus for restraining a load in an aerial delivery system
08/24/2005EP1289735B1 Conformable locating aperture system and method for alignment of members
08/24/2005EP1163151B1 Modular air intake duct for aircraft
08/24/2005CN1659080A Switchable electrochromic devices for use in aircraft transparency windows
08/23/2005US6932621 Connector interface pad for structurally integrated wiring
08/23/2005CA2208435C Hollow, integral asymmetrical metal structure such as an aircraft wing slat trailing edge and method of manufacture
08/18/2005US20050182528 Perspective vertical situation display system and method
08/18/2005US20050181203 First and second polymeric films covering aluminum foil include nylon, poly ether ether ketone (PEEK), polysulfonate, polyesters polyimide, polyolefins, polyurethane, halopolymers; protective coatings for aircraft skin; protection against lightning strikes and/or mitigation of P-static charging
08/18/2005US20050178924 Perforated skin structure for laminar-flow systems
08/18/2005US20050178914 Aircraft fuselage element and method of taking a number of pictures
08/18/2005US20050178912 Transformable airplane
08/18/2005US20050178907 Avionic door lock system
08/18/2005US20050178884 Flight device with a lift-generating fuselage
08/18/2005US20050178883 Helicopter tail rotor pylon
08/18/2005US20050178601 Control device for moving a vehicle closure element
08/18/2005DE102004035170B3 Process for manufacturing a cylindrical sheet metal part provided with ribs and stringers, especially an airplane fuselage, comprises attaching ribs in raised stringer/rib connector regions elastically deforming the shell part
08/17/2005EP1564141A1 Aircraft seat rail and its production method
08/17/2005EP1564135A1 Process and machine for machining flexible pannels with compensation of the machining thrust by a support means
08/17/2005EP1563958A1 Method and device for holding a thin and flexible pannel with a plurality of vacuum cups
08/16/2005US6929216 Method and apparatus for installing and actuating movable airfoils, including canards
08/11/2005WO2005073082A1 Reinforcing elements in the rear section of an aircraft
08/11/2005WO2005056383A9 A resin infused transparent skin panel and method of making same
08/11/2005US20050175406 Joint for connecting a longitudinal side to an upper side of components and flexible strip for use in such a joint
08/11/2005US20050175399 Joint for connecting components together on opposite longitudinal sides in addition to a flexible strip used for said joint
08/11/2005DE102005003436A1 Aircraft drainage mast assembly for used drinking water has heating isolation bush that presses the inner outlet heating arrangement radially inwards and the outer outlet heating arrangement radially outwards
08/10/2005CN1652923A Fluid transport assemblies with flame retardant properties
08/10/2005CN1214172C Collapsible panel and method for controlled callapsing thereof and vehicle thereof
08/10/2005CA2496770A1 Method and device for the mechanical machining of flexible panels, especially of complex shape
08/09/2005US6926481 Mounting apparatus for a transportation system
08/09/2005US6926235 Runway-independent omni-role modularity enhancement (ROME) vehicle
08/09/2005US6926231 Vertical takeoff and landing aircraft
08/09/2005US6925756 Apparatus for controlling the ingress and egress to and from an operator's compartment
08/04/2005WO2005035359A3 Attachement apparatus for injection-molded frameless canopies
08/04/2005US20050171653 Satellite coverage region detection
08/04/2005US20050170083 Method of manufacturing window having at least one of radio wave stealth property and electromagnetic wave shield property, and window material having at least one of radio wave stealth property and electromagnetic wave shield property
08/04/2005US20050169728 Fastening assemblies and components thereof
08/04/2005US20050169726 Expandable collet anchor system and method
08/04/2005DE10361655A1 Vorrichtung und Verfahren zur Fußbodenheizung in einem Flugzeug Apparatus and method for underfloor heating in an airplane
08/04/2005DE10361391A1 Connection connects a rudder unit having spars to the fuselage ribs of an airplane to form a power flow between the spars and the ribs
08/04/2005DE102004009017B3 Decompression device for two sDEarate regions of aircraft has locking device with release element in control cavity
08/04/2005DE102004001083A1 Insulation structure for commercial aircraft, has insulation core embedded in an insulation package which is enveloped by a burn-through safe film whose surface region serves to obstruct a fire
08/04/2005DE102004001081A1 Insulating structure for interior of vehicle e.g. aircraft, has insulation package, which is implemented homogeneously by using burn-through safe insulation made of burn-through safe insulation material
08/04/2005DE102004001080A1 Anordnung zur Innenverkleidung einer Passagierkabine eines Flugzeuges Arrangement for the inner lining of a passenger cabin of an airplane
08/03/2005EP1558492A1 Emergency door actuator system
08/03/2005EP1440883B1 Aircraft security system
08/03/2005EP0773881B1 Yaw control and stabilization system for helicopters
08/02/2005US6923606 Medical evacuation patient support pallet
08/02/2005US6923404 Apparatus and methods for variable sweep body conformal wing with application to projectiles, missiles, and unmanned air vehicles
08/02/2005US6923403 Tailed flying wing aircraft
08/02/2005CA2266317C Vibration isolation insert for aircraft floor panels and the like
07/2005
07/28/2005WO2005068291A1 Insulation arrangement for the internal insulation of a vehicle
07/28/2005WO2005068290A1 Insulation package arrangement for insulating the interior of an aircraft fuselage
07/28/2005WO2005068289A2 Fuselage
07/28/2005WO2005068288A1 Panel arrangement for an interior lining of a passenger cabin in an aircraft
07/28/2005WO2005068258A2 Insulation structure for the internal insulation of a vehicle
07/28/2005WO2005002961A3 Methods for manufacturing composite aircraft, parts and a family of composite aircraft
07/28/2005US20050163414 Rib structural system and method of manufacturing the rib structural system
07/28/2005DE10360484A1 Flugzeugtor Aircraft door
07/28/2005DE102004001078A1 Aircraft fuselage outer skin is a composite sandwich structure of carbon fiber, glass fiber, ceramic fibers, aluminium or titanium alloys
07/28/2005DE102004001049A1 Arrangement for internal insulation of an aircraft fuselage, for retardation of flame propagation into the cabin interior, comprises insulation packages which are covered by a foil with fire resistant properties
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