Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
07/2010
07/22/2010WO2010060824A4 Structural component of an aircraft or spacecraft and a fuselage component arrangement of an aircraft or spacecraft
07/22/2010US20100181435 Door assembly for laminar flow control system
07/22/2010US20100181429 Device for moving objects, intended in particular for luggage in a hold of an aircraft
07/22/2010US20100181428 Profile Comprising at Least One Hollow Profile Section
07/22/2010US20100181427 Curved element, wing, control surface and stabilizer for aircraft
07/22/2010US20100181426 Aircraft Fuselage Structure and Method for Producing it
07/22/2010US20100181420 Coating for acoustic treatment that integrates the function of hot-air treatment of frost
07/22/2010DE102007029337B4 Korrosionsfeste Verbindung zwischen einem ersten Bauteil und einem zweiten Bauteil Corrosion-resistant connection between a first component and a second component
07/22/2010DE102006039292B4 Rahmenelement, Flugzeugklimatisierungssystem sowie Verfahren zur Montage eines Rahmenelements in einem Flugzeug Frame member, aircraft air conditioning system and method for mounting of a frame member in an aircraft
07/22/2010DE102005007308B4 Kugelmatte zum Transport von Frachtbehältern Ball mat for the transportation of freight containers
07/21/2010EP2007622B1 Aircraft floor, use of said floor and aircraft section fitted with said floor
07/21/2010CN201530472U Force bearing rapid combined mouth cover
07/20/2010CA2467135C Composite material with improved damping characteristics and method of making same
07/20/2010CA2452787C Profiled wing unit of an aircraft
07/15/2010WO2010080536A2 Monomolecular carbon-based film for forming lubricious surface on aircraft parts
07/15/2010WO2010079282A1 Longitudinal joint for aircraft fuselage panels made of composite materials
07/15/2010US20100178454 Equipment and method for obtaining profile sections made from composite material and profile section obtained by means of said method
07/15/2010US20100176250 Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft
07/15/2010US20100176241 Aircraft front portion including a concave bulkhead separating a non-pressurized radome area and a pressurized area
07/15/2010DE102009004811A1 Device for locking passenger door against body structure of aircraft, has threaded pins cooperating with threaded bushes of edge frames such that movement of frame releases form-fit locking or opening of door over breadth of door joint
07/15/2010DE102005021078B4 Frachtladesystem Cargo loading system
07/14/2010EP2205484A2 Methods for fuel-efficient transportation of cargo by aircraft
07/14/2010EP1748925B1 Window frame for aircraft
07/14/2010CN101778986A Locking device
07/14/2010CN101778760A Composite laminate structure
07/13/2010US7753312 Lightweight structure especially for an aircraft and method for making such a structure
07/08/2010WO2010077508A2 A method of and system for maintaining operating performance of a transparency
07/08/2010WO2010077507A2 Transparency having sensors
07/08/2010WO2010028956A3 Rod for supporting components in a fuselage cell structure of an aircraft
07/08/2010US20100174426 Airplane emergency navigational system
07/08/2010US20100170997 Aircraft with optimised utility volume and method for optimising the utility volume of an aircraft
07/08/2010US20100170996 Weldable high-strength aluminum alloys
07/08/2010US20100170995 Support structure for a wing
07/08/2010US20100170994 Elastic aircraft joint fairing
07/08/2010US20100170992 Conveyor device intended in particular for luggage in an aircraft hold
07/08/2010US20100170989 Elongate composite structural members and improvements therein
07/08/2010US20100170988 Section of aircraft fuselage in composite material with a constant interior profile
07/08/2010US20100170987 Central section of aircraft with ventral or belly fairing capable of movement
07/08/2010US20100170986 Aircraft structural element located at the interface between a wing and the fuselage
07/08/2010US20100170985 Composite panel stiffener
07/08/2010US20100170984 Engine assembly for aircraft with sliding nancelle
07/08/2010DE102007063159A1 Flügel-Rumpf-Strukturbauteil zur Verbindung von zwei Tragflügeln und einer Rumpfsektion an einem Flugzeug Wing-fuselage component for connecting two wings and a fuselage section of an aircraft
07/07/2010EP2203308A2 Flexible laminate sheet materials
07/07/2010CN101772451A Self supporting cellular thermal acoustic insulation
07/06/2010US7748661 Aircraft structure and a fastener for use therewith
07/01/2010WO2010072952A1 Composite l-shaped fitting and method and mould for the production thereof
07/01/2010WO2010007415A4 Ramped stiffener and apparatus and method for forming the same
07/01/2010US20100163676 Aircraft with windshield glass plates interchangeable between different types
07/01/2010US20100163675 Transparency having sensors
07/01/2010US20100163670 Deltoid main wing aerodynamic configurations
07/01/2010US20100163669 Super aircraft structrue
07/01/2010DE202010004404U1 Fensterverdunkelungsvorrichtung Window shading device
07/01/2010DE102009014528A1 Elektromechanische Blockiereinrichtung, insbesondere für die Tür eines Flugzeuges Electromechanical locking device, in particular for the door of an aircraft
07/01/2010DE102008064122A1 Türmechanismus für eine Flugzeugbordküche Door mechanism for an aircraft galley
07/01/2010DE102008062703A1 Flugzeugkabinenpaneel zur Schallabsorption Flugzeugkabinenpaneel for sound absorption
07/01/2010DE102008062701A1 Flugzeugkabinenpaneel mit Kerntaschen zur Schallabsorption Flugzeugkabinenpaneel core with pockets for sound absorption
07/01/2010DE102008043023A1 Device for supporting door in pressure-tight fuselage compartment of passenger aircraft, has thrust bearing comprising thrust bearing surface sectionally lying at counter bearing surface in closed condition of door
07/01/2010DE102007041387B4 Bremsvorrichtung für bewegliches Teil in einem Luftfahrzeug Braking device for moving part in an aircraft
07/01/2010DE102004049893B4 Fugenabdeckung in Flugzeugen Covering joints in aircraft
06/2010
06/30/2010EP2200898A1 Structural component and fuselage of an aircraft or spacecraft
06/30/2010EP2200897A1 Method for the production of a fuselage airframe of an aircraft
06/30/2010CN101765538A Reduced dimension landing gear casing
06/30/2010CN101765499A A window shade and a multi-layered article, and methods of making the same
06/30/2010CN101758922A Retractable captive flight support for external hanging equipment
06/29/2010US7746037 Power supply for an electric window dimming device
06/29/2010US7744035 Door for compartment of the baggage-compartment type
06/29/2010US7744034 Translating flap drive door
06/29/2010US7744033 Aircraft luggage handling system
06/29/2010US7743884 Sandwich panel for sound absorption
06/24/2010WO2010070184A1 Structure of the load-introduction area in the fuselage rear section of an aircraft
06/24/2010WO2010070182A2 Horizontal stabilising surface of an aircraft
06/24/2010WO2010070071A1 Aircraft cabin panel for sound reduction
06/24/2010WO2010069831A1 Multilayer board for sound insulation
06/24/2010WO2010043516A4 Structural element for reinforcing a fuselage of an aircraft
06/24/2010WO2010020632A3 Connection of a wing to a fuselage of an airplane
06/24/2010WO2009153033A4 Aircraft conduit monitoring system and method
06/24/2010US20100155537 Energy-absorbing structural composite element
06/24/2010US20100155533 Composite forward pressure bulkhead
06/24/2010US20100155532 Structure of the load introduction zone in the rear end of an aircraft
06/24/2010US20100155529 Landing gear with noise reduction fairing
06/24/2010US20100155527 Monomolecular carbon-based film for forming lubricious surface on aircraft parts
06/24/2010US20100155524 Monomolecular carbon-based film for forming lubricious surface on aircraft parts
06/24/2010DE102008063923A1 Mehrschichtplatte zur Schalldämmung Multilayer board for sound insulation
06/24/2010DE102007029762B4 Verfahren zur Verbindung eines trockenen Faserbands mit einem trockenen Faserstrang A method for connecting a dry fiber tape with a dry fiber strand
06/24/2010CA2747690A1 Structure of the load introduction zone in the rear end of an aircraft
06/24/2010CA2747689A1 Aircraft horizontal stabilizer surface
06/24/2010CA2746333A1 Aircraft cabin panel for sound reduction
06/23/2010EP2197739A1 Fuselage structure for aircraft fuselage made of composite material and aircraft equipped with such fuselage structure
06/23/2010CN101746499A Miniaturized large-load low-altitude low-speed unmanned plane
06/23/2010CN101481013B Power installation for emergency opening of service door during passenger plane trial flight
06/22/2010US7740932 Hybrid fiberglass composite structures and methods of forming the same
06/22/2010US7740201 Device and method for floor heating in an aircraft
06/17/2010WO2010067001A1 Modular floor section for aircraft
06/17/2010WO2010065999A1 A controllable buoyancy system
06/17/2010US20100148009 Connecting arrangement comprising a coupling element and two curved ribs of an aircraft or spacecraft
06/17/2010US20100148008 Rib-fitting
06/17/2010US20100148007 Cover for an aircraft structure
06/17/2010US20100148005 Curved beam of fiber composite material
06/17/2010US20100148004 Stiffened casing for an aircraft or spacecraft with a laminate stringer of high rigidity and corresponding laminate stringer
06/17/2010US20100148003 Structuring construction for an aircraft fuselage
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