Patents
Sitemap › B64 - Aircraft; Aviation; Cosmonautics › B64C - Aeroplanes; Helicopters › B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
12/2008
12/04/2008WO2008145892A1 Device for attaching a lift member to the fuselage of an aircraft
12/04/2008WO2008128083A3 Overhead luggage bin for aircraft interior
12/04/2008US20080296433 Lightweight structural component in particular for aircraft and method for its production
12/04/2008US20080296432 Method of extending length of aircraft to increase interior space
12/04/2008US20080296431 Noise controlled turbine engine with aircraft engine adaptive noise control tubes
12/04/2008US20080296428 Air Freight Transport Method, Transport Aeroplane and Air Freight Transport System
12/04/2008US20080295334 Apparatus and methods for securing a first structural member and a second structural member to one another
12/04/2008DE10258105B4 Luftfahrzeug-Türanordnung Aircraft door arrangement
12/04/2008DE102008025148A1 Rückhaltevorrichtungssystem für das Laden von Luftfracht entlang der Mittellinie eines Frachtraumes eines Flugzeugs und Verfahren für dessen Verwendung Restraint system for loading of cargo along the center line of a cargo compartment of an aircraft, and method for its use
12/04/2008DE102007060030A1 Vorrichtung zur Halterung von Systemen A device for holding systems
12/04/2008CA2683596A1 Device for attaching a lift member to the fuselage of an aircraft
12/03/2008EP1998011A2 Vent for the lubricating oil system of a turbojet engine
12/03/2008EP1996458A1 Drainage device, aircraft, and method for letting out a fluid that is present between the exterior skin and the interior lining of an aircraft
12/03/2008EP1996457A1 Bolted joint
12/03/2008EP1996456A2 Bolted joint
12/02/2008CA2527105C Surface temperature control system
11/2008
11/27/2008WO2008143092A1 Aircraft assembly and method for manufacturing the same
11/27/2008WO2008054499A3 Composite wing-body joint
11/27/2008US20080290218 Plasma actuator system and method for use with a weapons bay on a high speed mobile platform
11/27/2008US20080290214 Shaped composite stringers and methods of making
11/27/2008DE102007063608A1 Verbund und Rumpfzellenabschnitt mit einem derartigen Verbund And composite fuselage section with such a composite
11/27/2008DE102007046478A1 Sheet laminate, particularly for use as skin plate for truncated cell of airplane, has multiple thin aluminum alloy sheets, which are laminated on one another
11/26/2008EP1912859B1 Window element for insertion in a window cutout in an outer skin of an aircraft
11/26/2008EP1492896B1 Al-zn-mg-cu alloys welded products with high mechanical properties, and aircraft structural elements
11/26/2008CN101312876A Landing gear casing provided with a dissociated structure
11/26/2008CN101312875A Landing gear casing provided with a box structure
11/25/2008CA2461079C Arrangement for fixing an insulating blanket and related method
11/20/2008WO2008141149A1 Aircraft door hinge assembly
11/20/2008WO2008141146A1 Vent door system with lever mechanism
11/20/2008WO2008139214A1 Reinforced panel
11/20/2008WO2008090084B1 Lining for an aircraft
11/20/2008US20080284619 Aircraft Doors
11/20/2008US20080283668 Composite material structure for aircraft fuselage and process for manufacturing it
11/20/2008US20080283666 Method and apparatus for attaching a wing to a body
11/20/2008US20080283665 Aircraft Ventral Fairing Partition Wall and Aircraft Equipped with a Ventral Fairing
11/20/2008US20080283664 Aircraft Fuselage Structure
11/20/2008US20080283662 Aircraft Interior Module
11/20/2008DE102005016654B4 Sandwichelement zur schallabsorbierenden Innenverkleidung von Verkehrsmitteln, insbesondere zur schallabsorbierenden Innenverkleidung von Luftfahrzeugen Sandwich panel for sound-absorbing interior lining of transport, particularly for sound absorbing interior trim of aircraft
11/20/2008CA2684551A1 Reinforced panel
11/19/2008EP1915290B1 Continuous fuselage connection
11/19/2008CN201151484Y Composite stressed-skin construction
11/19/2008CN101306722A Rib structure for torsion boxes of a wing or horizontal stabiliser of an aircraft
11/19/2008CN100434730C Connecting element
11/19/2008CN100434634C Contact stiffeners for structural skins
11/18/2008US7451950 Joint for connecting a longitudinal side to an upper side of components and flexible strip for use in such a joint
11/18/2008CA2459167C Composite material structure
11/13/2008WO2008135533A1 Connecting device for connecting two curved ribs of an aircraft or spacecraft
11/13/2008WO2008104714A3 Coating for acoustic treatment having a hot air icing processing function
11/13/2008WO2008097383A3 Unitary one-piece windshield
11/13/2008US20080277531 Hybrid Composite Panel Systems and Methods
11/13/2008US20080277530 Vent door system with lever mechanism
11/13/2008US20080277528 Payload support track interface and fitting
11/13/2008US20080277527 Attachment structure for affixing interior equipment components of an aircraft passenger cabin
11/13/2008US20080277526 Aircraft Cooling Duct
11/13/2008US20080277524 Methods and apparatus for aircraft
11/13/2008US20080277071 Method and apparatus for molding thermosetting composite material
11/13/2008DE102007021822A1 Sicherheitssystem gegen schädliche Druckwellen bei militärischen Einrichtungen wie Radarabdeckungen und Panzerungen Security system against harmful pressure waves to military facilities such as radar covers and armor
11/13/2008DE102007019821A1 Strukturelement eines Flugzeugrumpfs Structural element of an aircraft fuselage
11/13/2008DE102006020053B4 Metallisches, integrales Strukturbauteil Metallic, integral structural component
11/13/2008DE102004006648B4 Frachtraumboden für Luftfahrzeuge Cargo compartment floor for aircraft
11/13/2008CA2685188A1 Connecting device for connecting two curved ribs of an aircraft or spacecraft
11/13/2008CA2673611A1 Fire-barrier film laminate
11/12/2008EP1990552A1 Bolt and method for manufacturing bolt
11/12/2008EP1989108A2 Door pod assembly
11/12/2008EP1989101A2 Pressure activated latch
11/12/2008CN101304822A A multi-alloy monolithic extruded structural member and method of producing thereof
11/12/2008CN100431920C Window frame for aircraft
11/11/2008US7448652 Tubular metal fitting expandable in a wall opening and method of installation
11/11/2008US7448578 Aircraft with forward opening inlay spoilers for yaw control
11/11/2008US7448574 Aircraft archway architecture
11/06/2008WO2008132498A1 Composite structure comprising a stringer with a pad embedded in the recess of a panel and method of transmitting forces
11/06/2008WO2008132319A1 Method for making stiffeners of a composite material
11/06/2008WO2008132171A2 Structural element of an aircraft fuselage
11/06/2008WO2008132087A1 Wing-fuselage section of an aircraft
11/06/2008WO2008132050A1 Fibre metal laminate panel
11/06/2008WO2008131955A1 Door hinge and door arrangement
11/06/2008WO2008108826A3 Composite aircraft structures with hat stiffeners
11/06/2008WO2008085547A3 Aerodynamic integration of a payload container with a vertical take-off and landing aircraft
11/06/2008WO2007055813A3 Aerodynamic shroud having textured surface
11/06/2008US20080272615 Airflow control devices based on active materials
11/06/2008US20080272236 Space frame fuselage structure and related methods
11/06/2008DE102007021076A1 Inter-costal arrangement for aircraft or spacecraft, has cross-member movable between a first and a second position for relieving loading between struts
11/06/2008DE102007021075A1 Verbindungsanordnung zum Verbinden zweier gekrümmter Spanten eines Luft- oder Raumfahrzeugs Connecting arrangement for connecting two curved ribs of an aircraft or spacecraft
11/06/2008DE102007019305A1 Befestigungsanordnung zum Befestigen eines Bauteils an einem Flugzeugrumpf, Flugzeug und Verfahren zum Fertigen einer Befestigungsanordnung Fastening arrangement for fastening a component on an aircraft fuselage, the aircraft and method for fabricating a mounting assembly
11/06/2008CA2684076A1 Composite structure comprising a stringer with a pad embedded in the recess of a panel and method of transmitting forces
11/06/2008CA2682969A1 Structural element of an aircraft fuselage
11/06/2008CA2681854A1 Wing-fuselage section of an aircraft
11/06/2008CA2680369A1 Fibre metal laminate panel
11/05/2008EP1767343A4 Laminated composite material and a product made thereof
11/05/2008EP1763470B1 Commercial aircraft with a main deck and a lower deck
11/05/2008CN101300178A Baggage accommodation device
11/05/2008CN101300124A Stringpiece with bulb made of composite material
11/05/2008CN100430295C Insulation arrangement for the internal insulation of a vehicle
11/04/2008US7445180 Actuation system for tail section of aircraft
10/2008
10/30/2008WO2008129038A1 Attachment arrangement for attaching a component to the fuselage of an aircraft, aircraft and method for constructing an attachment arrangement
10/30/2008US20080265096 Aircraft door window
10/30/2008US20080265093 Integrated multispar torsion box of composite material
10/30/2008US20080265092 Methods and apparatus for an aircraft lavoratory
10/30/2008DE10212123B4 Frachtladesystem in einem Laderaum eines Flugzeugs Cargo loading system in a cargo compartment of an aircraft
10/30/2008DE102007019716A1 Faser-Metall-Laminat-Panel Fibre metal laminate panel
1 ... 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 ... 126