Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
04/2008
04/03/2008US20080078877 Window assembly and method for a mobile platform
04/03/2008US20080078876 Composite resin window frame constructions for airplanes
04/03/2008US20080078868 System and method for a power-assisted compartment
04/03/2008US20080078867 Air cargo power drive unit for detecting motion of an overlying cargo container
04/03/2008US20080078494 Window skin panel and method of making same
04/03/2008DE102006046080A1 Metallisches Flugzeugbauteil Metallic aircraft component
04/03/2008DE102006045635A1 Pre-hardened stringer tying method for e.g. spacecraft, involves tying stringers at structural component in pressure loaded manner, using foils, sealing unit and strips, and arranging stringers parallel to each other on component
04/03/2008DE102006045634A1 Method for bonding profile to second component comprises filling recesses in profile to give it rectangular cross-section, positioning it on component and covering with vacuum sheet, so that profile and component are pressed together
04/03/2008DE102006045633A1 Uncured stringer e.g. double T-shaped support, joining method, for e.g. aircraft, involves precuring/curing auxiliary material at specific temperature to form supporting units for web flanks, curing uncured stringer, and removing material
04/03/2008DE102006044093A1 Scheibenersatz zum Ausfüllen eines Fensterrahmens Disc replacement to fill out a window frame
04/03/2008DE102005015338B4 Seitenleitwerkanschluss Rudder port
04/02/2008EP1904367A2 Tunable acoustic absorption system for an aircraft cabin
04/02/2008EP1904366A2 Monolithic self-stiffened panels
04/01/2008US7350753 RF shielding for aircraft windows
03/2008
03/27/2008WO2008034992A1 Locking and unlocking system for the cockpit door of an aircraft and door with such a system
03/27/2008WO2008034988A1 Self-stabilised stiffener enabling element recovery
03/27/2008US20080073464 Passenger stairway for an aircraft and method for pulling in and out the passenger stairway
03/27/2008US20080073462 Force Assisting System
03/27/2008DE10205902B4 Riegelelement Locking element
03/27/2008DE102006055377A1 Fireproof bulkhead used in aircraft construction, comprises highly porous structure formed as reticulated metallic foam or as highly porous pimple or nub structure coated with intumescent lacquer
03/27/2008DE102006042748A1 Airframe structure i.e. pressure tunnel arrangement, for aircraft or spacecraft, has membrane arrangement forming receiving shaft that extends into hollow body section, and accessible from outside of section
03/27/2008DE102006041787A1 Multilayer interior fitting component, e.g. for side or overhead panelling in aircraft, comprises a transparent thermoplastic surface layer and a supporting layer of thermoplastic foam
03/27/2008DE102004037559B4 Montageschutzvorrichtung für ein Bauteil eines Flugzeugs Mounting protection device for a component of an aircraft
03/27/2008CA2663678A1 Locking and unlocking system for the cockpit door of an aircraft and door with such a system
03/27/2008CA2662849A1 Self-stabilised stiffener enabling element recovery
03/26/2008EP1902812A1 Metal aircraft structural member
03/26/2008EP1714867B1 Rotorcraft and supporting structure
03/25/2008US7347399 Aircraft partition designed to separate a cargo part from a cockpit or from a passenger compartment
03/20/2008WO2008033017A1 Skin panel for an aircraft fuselage
03/20/2008WO2008032040A1 Rib post
03/20/2008US20080067818 Bifurcated latching system
03/20/2008US20080067289 Splice plate for stringers and orbital joining device
03/20/2008US20080067288 Window replacement for filling a window frame
03/20/2008US20080067283 Methods and apparatus for reducing noise via a plasma fairing
03/20/2008DE102006031436A1 Strukturelement, Verfahren zur Herstellung eines derartigen Strukturelements und Flugzeug mit einem derartigen Strukturelement Structural element, method for producing such a structural member and aircraft with such a structural member
03/20/2008CA2663151A1 Rib post
03/19/2008EP1899149A1 Process for producing a substantially shell-shaped component
03/19/2008EP1500494B1 Composite material with improved damping characteristics and method of making same
03/19/2008EP1351855A4 Integrated and/or modular high-speed aircraft
03/19/2008CN101146711A Device and method for non-symmetrical mixed carbon-metal assembly
03/19/2008CN101146710A Integrated aircraft structural floor
03/18/2008US7344260 Stowable laser eye protection
03/18/2008US7344110 Aircraft with detachable passenger escape cabin
03/13/2008WO2008029049A1 Panel assembly and method of erecting a panel assembly
03/13/2008DE102006040383A1 Deflector trap for rainwater or de-icing fluid retracts into recess above fuselage entry door
03/13/2008DE102006040298A1 Lightweight construction for aircraft comprises bar elements connected to each other at the head region using connecting elements which extend from one bar element to another and are recessed between free regions
03/13/2008DE102006039292A1 Frame element for use in aircraft air-conditioning system, has longitudinal struts, each having air-inlet connection connected to air-conditioning unit, and air-outlet connection connected to cabin region
03/13/2008DE102006039291A1 Frame element for use in installation of storage bin in aircraft, has longitudinal parallel struts that extend parallel to ribs of aircraft structure, when frame element is mounted to aircraft structure
03/13/2008DE102006039290A1 Frame element for aircraft component assembly system, has connecting struts that are provided with recesses for receiving ribs of aircraft structure when frame element is attached to aircraft structure
03/13/2008DE102005039838B4 Transmissionsgesteuerte Fensterverglasung Transmission controlled window glazing
03/12/2008EP1897803A1 Holding element for fastening an equipment element to a supporting rail
03/12/2008EP1896322A1 Device for fixing a seat rail on a floor, and aircraft equipped with such a fixing device
03/06/2008WO2008025860A1 Tubular components for fuselages and methods and tools for producing same
03/06/2008WO2007072027A3 Aircraft fuselage heating
03/06/2008US20080054123 Operation mechanism for activating a deceleration device
03/06/2008US20080054122 Window Frame for Aircraft
03/05/2008EP1893479A2 Composite skin and stringer structures and methods for forming the same
03/05/2008EP1893478A1 Reinforcement beam as well as method and fiber laminate for manufacturing the reinforcement beam
03/05/2008EP1701882B1 Insulation arrangement for the internal insulation of a vehicle
03/05/2008EP1211174B1 Aircraft with a plurality of upper and lower cabins functioning as cargo compartments or passenger cabins and method of loading cargos for aircraft
03/05/2008CN101137541A Aircraft structural element provided with a cavity and drainage element
03/04/2008US7338013 Floor for aircraft
02/2008
02/28/2008WO2008022965A1 Aircraft with optimised utility volume and method for optimising the utility volume of an aircraft
02/28/2008WO2008022773A1 Frame element, aircraft component assembly system and method of fitting a component in an aircraft
02/28/2008WO2008022752A1 Frame element, aircraft air-conditioning system and method for the installation of a frame element in an aircraft
02/28/2008US20080048889 Aircraft Provided With A Cabin Differential Pressure Warning System
02/28/2008US20080048068 Window Frame For Aircraft
02/28/2008CA2661788A1 Aircraft with optimised utility volume and method for optimising the utility volume of an aircraft
02/28/2008CA2659836A1 Frame element, aircraft component assembly system and method of fitting a component in an aircraft
02/28/2008CA2659834A1 Frame element, aircraft air-conditioning system and method for the installation of a frame element in an aircraft
02/27/2008CN201026990Y Elevator car gate ladder
02/27/2008CN101132912A Layered, transparent thermoplastic for flammability resistance
02/27/2008CN100371216C System for loading and unloading unit loads into a cargo hold, in particular of an aircraft, and intermediate transport device or corresponding transport unit
02/26/2008US7334758 Attachment assembly for mounting a seat to the floor of a vehicle
02/21/2008WO2008000670A3 Pressure bulkhead for an aerospace fuselage
02/21/2008WO2007147885B1 Vacuum insulation panels for aircraft interiors
02/21/2008WO2007141268B1 Aircraft fuselage structure and method for producing it
02/21/2008US20080042012 Electrochromic window assembly
02/20/2008EP1889713A2 Method of joining composite honeycomb panel sections, and composite panels resulting therefrom
02/20/2008EP1888870A1 Ladder system, especially for vehicles
02/20/2008EP1888403A2 Rotor hub fairing system for a counter-rotating, coaxial rotor system
02/20/2008EP1888323A1 Method for manufacturing a reinforced shell for forming component parts for aircraft and shell for component parts for aircraft
02/20/2008CN201023652Y Airplane integral movement canopy framework
02/20/2008CN101128357A Monolithic composite panel with multicell box shape
02/19/2008US7331547 Device for facilitating the lowering of a landing gear by gravity
02/19/2008US7331545 Aircraft archway
02/19/2008US7331544 Deployable receptacle
02/14/2008US20080035793 Aircraft Door Arrangement With an Aircraft Door That Swings By 180
02/14/2008US20080035792 Deployable receptacle
02/14/2008DE102006035939A1 Verfahren zur Herstellung von Faserverbundbauteilen A process for the manufacture of fiber composite components
02/14/2008DE102006035847A1 Wing section producing method for e.g. aircraft, involves laying structural arrangement on laminating apparatus by tape-laying machine, and curing structural arrangement to form wing section
02/13/2008EP1697212B1 Dynamic cmg array and method
02/12/2008US7328771 Zero acoustic splice fan case liner
02/07/2008WO2008015362A1 Structural element of an aircraft
02/07/2008WO2008015360A1 Aircraft doorway
02/07/2008US20080029647 Reinforced cover for cut-outs in an aerodynamic contour
02/07/2008US20080029646 Device for Receiving Liquids in Aircraft and/or Releasing LiquidsTherfrom
02/07/2008US20080029644 Process for manufacturing composite material structures with collapsible tooling
02/07/2008DE202007016432U1 Befestigungsmittel zum Verbinden von Plattenhaltern mit einer Luftfahrzeugzelle, Plattenhalter mit einem solchen Befestigungsmittel und Luftfahrzeug mit einem solchen Plattenhalter Fastening means for joining insert holders with an air vehicle compartment plate holder with such a mounting means and aircraft with such a disc holder
02/07/2008CA2659821A1 Element de structure d'un aeronef
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