| Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
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| 02/06/2013 | CN102910283A Loads interface, particularly a loads interface for a plug type aircraft door |
| 02/06/2013 | CN102910282A Loads interface, particularly a loads interface of an aircraft structure |
| 02/05/2013 | US8369069 Avionics equipment carrier system with quick-mount housing and quick-mount modules |
| 02/05/2013 | US8366050 Blended wing body cargo airplane |
| 02/05/2013 | US8366049 Hover delivery of cabin payload in tilt-rotor and tilt-wing aircraft |
| 02/05/2013 | US8366046 Aerospace articles made from quasi-isotropic chopped prepreg |
| 02/05/2013 | US8366045 Apparatus with damage indication feature |
| 02/05/2013 | US8366043 Structure, especially a fuselage structure of an aircraft or a spacecraft |
| 02/05/2013 | US8366042 Arrangement for installing electric cables in the floor region of an aircraft |
| 02/05/2013 | US8366041 Aircraft floor, use of said floor and aircraft section fitted with said floor |
| 02/05/2013 | US8365412 Core structure and method for producing a core structure |
| 01/31/2013 | WO2013015765A1 Aft-loading aircraft with-twin t-tail assembly |
| 01/31/2013 | WO2013015370A1 Laminate and thermal-insulation material using same |
| 01/31/2013 | WO2013013662A1 Light transmission control device and aircraft window furnished therewith, and a method for producing such a light transmission control device |
| 01/31/2013 | WO2012127038A3 Method for producing a structural component, and structural component |
| 01/31/2013 | US20130026296 Cockpit window of aircraft having electromagnetic shield, and aircraft |
| 01/31/2013 | US20130026295 Flow body with a base body and a leading edge |
| 01/31/2013 | US20130026292 Stiff panel for aircraft, comprising stiffeners with notched cores |
| 01/31/2013 | US20130026288 Aircraft Comprising At Least One Net For Reducing Aerodynamic Noise From A Structural Element Of Said Aircraft |
| 01/31/2013 | DE102010014265B4 Türrahmenanordnung mit einer Tür für einen Rumpf insbesondere für Luft- oder Raumfahrzeuge Door frame assembly with a door for a body in particular for air and space vehicles |
| 01/31/2013 | DE102007033868B4 Profil mit wenigstens einem Hohlprofilquerschnitt Profile with at least one hollow profile section |
| 01/31/2013 | DE102007015007B4 Türrahmenbauteil aus Titanguss und Rumpfstrukturteil Door frame component made of titanium alloy and hull structural part |
| 01/30/2013 | EP2551188A1 Stiffened panel for aircraft comprising stiffeners with indented webs |
| 01/30/2013 | EP2551187A1 Cap, fastened structure using same, and aircraft having said fastened structure |
| 01/30/2013 | CN202703886U Detachable airframe reinforcing frame |
| 01/30/2013 | CN202703885U Long purline butt connector with variable thickness |
| 01/30/2013 | CN202703884U Integration structure of missile airfoil rib and cabin longitudinal beam |
| 01/30/2013 | CN102905970A Rail system and method and system for mounting a component in an aircraft |
| 01/30/2013 | CN102897312A Protective shield against ice impacts on aircraft |
| 01/29/2013 | US8360362 Aircraft floor and method of assembly |
| 01/29/2013 | US8360357 Aircraft with a wing movable along the longitudinal axis of the fuselage |
| 01/29/2013 | US8360355 Wing-to-body fairing with spray-on foam and noise reduction method |
| 01/24/2013 | WO2013012505A1 Flexible truss frame and method of making the same |
| 01/24/2013 | US20130020440 Structure for joining torsion boxes in an aircraft using a triform fitting made from non-metallic composite materials |
| 01/24/2013 | US20130020439 Separating element for a platform cabin comprising a push rod mechanism for moving a leaf |
| 01/24/2013 | US20130020438 Flexible Truss Frame and Method of Making the Same |
| 01/24/2013 | US20130020434 Condensed Water Decreasing Insulation Package For Thermal And Acoustic Insulation Of A Vehicle Cabin |
| 01/24/2013 | DE102011108167A1 Window funnel for aircraft, has foam ring which is fastened on outer side of window funnel by adhesive layer, where foam ring is provided with section or groove in area that is not covered by adhesive layer |
| 01/24/2013 | DE102010005987B4 Verfahren zur Herstellung von Hohlkörpern mit bundförmigen Verstärkungen Process for the production of hollow bodies with collar-shaped reinforcements |
| 01/23/2013 | CN202686755U Anti-vibration structure of aircraft radome |
| 01/23/2013 | CN202686753U Cockpit cover door frame for helicopter |
| 01/23/2013 | CN202686752U Web-shaped airplane skylight framework |
| 01/23/2013 | CN202686751U Honeycomb sandwich structure covering |
| 01/23/2013 | CN202686750U Connection device for conjoined airplane |
| 01/23/2013 | CN102892670A Composite stringer end trim |
| 01/23/2013 | CN101875398B Multi-redundancy rotary motor-driven mechanism for driving airplane exhaust valve |
| 01/22/2013 | US8356773 Structural wing-fuselage component for connecting two wings to a fuselage section of an aircraft |
| 01/22/2013 | US8356772 Lightweight structure |
| 01/22/2013 | US8356771 Coupling for joining two frame segments |
| 01/22/2013 | CA2783706A1 Frangible joint mechanism for a platform partition, partition, set and associated methods |
| 01/22/2013 | CA2783595A1 Separation element for a platform cabin including a crank mechanism for moving an opening |
| 01/22/2013 | CA2783523A1 Separating element for platform cabin with a crankshaft drive arrangement for moving an out opening |
| 01/22/2013 | CA2598765C Method and apparatus for manufacturing composite structures |
| 01/17/2013 | WO2013009209A1 Device for attachment of doors of an aircraft |
| 01/17/2013 | WO2013007805A1 Intermediate retaining structure for systems to be installed on board an aircraft |
| 01/17/2013 | WO2013007456A1 Aircraft structure module and associated structure and aircraft |
| 01/17/2013 | WO2013007455A1 Cross-beam for supporting a structure of an aircraft and associated aircraft |
| 01/17/2013 | WO2012102640A3 Airframe for a highly maneuvrable multi-mode aircraft |
| 01/17/2013 | WO2012080217A3 Fastening arrangement and fastening fitting for fastening a component to a structural component of an aircraft or spacecraft |
| 01/17/2013 | US20130015294 Closing member for opening |
| 01/17/2013 | DE102009041670B4 Bremsrolle mit Schlingfeder Drag reel with coil spring |
| 01/16/2013 | CN102883949A Cap, fastened structure using same, and aircraft having said fastened structure |
| 01/16/2013 | CN102873880A Composite manufacturing method |
| 01/16/2013 | CN101678890B Shaped composite stringers and methods of making |
| 01/16/2013 | CN101668679B Wing-fuselage section of an aircraft |
| 01/16/2013 | CN101657352B Attachment arrangement for attaching a component to the fuselage of an aircraft, aircraft and method for constructing an attachment arrangement |
| 01/16/2013 | CN101194082B Ladder system, especially for vehicles |
| 01/15/2013 | US8353479 Arrangement of two fuselage sections of an aircraft and a connecting structure for connecting fuselage skins |
| 01/15/2013 | US8353478 Blended wing aircraft |
| 01/15/2013 | CA2557594C Self extinguishing composite primary structure |
| 01/10/2013 | WO2013004671A1 Method for locally strengthening a composite panel with fibrous reinforcement and panel obtained using such a method |
| 01/10/2013 | WO2013004553A2 Method and device for protecting composite primary structural elements from impacts |
| 01/10/2013 | US20130009008 Structural component with rib and cross member element |
| 01/10/2013 | US20130009007 Intermediate support structure for the cockpit of an aircraft |
| 01/10/2013 | US20130009002 Turboshaft engine supporting pylon covered with a porous material and turboshaft engine/pylon assembly |
| 01/10/2013 | DE10251580B4 Verfahren zum Herstellen eines Bauelementes aus faserverstärktem Kunststoff A method for producing a component of fiber reinforced plastic |
| 01/10/2013 | CA2838922A1 Method for locally strengthening a composite panel with fibrous reinforcement and panel obtained using such a method |
| 01/09/2013 | EP2370315B1 Planar component of an aircraft and method for producing the same |
| 01/09/2013 | EP2331318B1 Fiber composite component for energy absorption in the event of a crash for an aircraft or spacecraft, fuselage structural section of an aircraft or spacecraft, and aircraft or spacecraft |
| 01/09/2013 | EP2307272B1 Method for installing a dome-shaped pressure bulkhead in a rear section of an aircraft, and device for carrying out the method |
| 01/09/2013 | CN202657241U Unmanned helicopter fuselage frame |
| 01/09/2013 | CN102869569A Method for assembling window coaming on a fuselage, coaming to be used, and aircraft fuselage provided with such coaming |
| 01/09/2013 | CN102862673A Intermediate support structure for the cockpit of an aircraft |
| 01/09/2013 | CN102167155B Aircraft with turnable wings |
| 01/08/2013 | US8349986 Poly(ureaurethane)s, articles and coatings prepared therefrom and methods of making the same |
| 01/08/2013 | US8348194 Conveyor device intended in particular for luggage in an aircraft hold |
| 01/08/2013 | CA2702908C Aircraft structure including stiffener edge junctions |
| 01/08/2013 | CA2635832C Flight deck and airplane comprising such a flight deck |
| 01/06/2013 | CA2783081A1 Condensation drainage system for an aircraft |
| 01/03/2013 | WO2013003099A1 Flight vehicle fairing having vibration-damping blankets |
| 01/03/2013 | WO2013001224A1 Method of opening a protective dome, in particular a radome, and radome equipped with a pantograph for implementation thereof |
| 01/03/2013 | WO2013000447A1 Connection arrangement for connecting two profiled elements in an aerodynamically smooth manner, method for producing said connection arrangement, and device for carrying out the method |
| 01/03/2013 | WO2012152947A3 Gutter profile and aircraft |
| 01/03/2013 | US20130001361 Holder assembly for a secure line installation in structure openings of aircraft |
| 01/03/2013 | US20130001356 Reinforced aircraft fuselage |
| 01/03/2013 | DE102011107624A1 Verbindungsanordnung zur aerodynamisch glatten Verbindung zweier Profilelemente, Verfahren zu deren Fertigung und Vorrichtung zur Durchführung des Verfahrens Connecting assembly for aerodynamically smooth connection of two profile elements, processes for their manufacture and apparatus for carrying out the method |
| 01/03/2013 | CA2839809A1 Method of opening a protective dome, in particular a radome, and radome equipped with a pantograph for implementation thereof |
| 01/03/2013 | CA2834323A1 Flight vehicle fairing having vibration-damping blankets |
| 01/02/2013 | EP2541094A1 Vibration reduction device and vibration reduction method |
| 01/02/2013 | EP2540617A2 Safety swivel mechanism |