| Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
|---|
| 07/06/2011 | EP2340991A2 Aircraft fuselage frame of composite material with stabilising ribs |
| 07/06/2011 | EP2340203A1 Airplane having engines partially encased in the fuselage |
| 07/06/2011 | EP2340201A1 Pyrotechnic egress system |
| 07/06/2011 | EP2340200A1 Systems and methods to provide optical enlargement of passenger interior cabin space |
| 07/06/2011 | EP2340162A1 Reinforced composite sandwich panel |
| 07/06/2011 | EP2019774B1 Sound-absorbing inner cladding of aircraft |
| 07/06/2011 | CN102114909A Leading edge impact and tiny cross passage cooling structure for hypersonic vehicle |
| 07/06/2011 | CN101466592B Aircraft fuselage structure and method for its production |
| 07/05/2011 | US7971827 Bird collision prevention device for an aircraft |
| 06/30/2011 | WO2011077030A1 Device and method for maintaining parallelism between the two glazings of an aircraft double glazing |
| 06/30/2011 | WO2011003844A3 Stringer |
| 06/30/2011 | WO2011001081A3 Frame for an opening provided in an aircraft fuselage |
| 06/30/2011 | US20110159248 Aircraft fuselage frame of composite material with stabilising ribs |
| 06/30/2011 | US20110159242 Aircraft fuselage frame in composite material with stabilized web |
| 06/30/2011 | US20110155854 Method for the manufacture of a fiber-reinforced component, device for implementing the method, and fiber-reinforced component |
| 06/30/2011 | US20110155852 Stiffening element for an aircraft and a surface structure with a stiffening element of this type |
| 06/30/2011 | US20110155851 Aircraft observation window |
| 06/30/2011 | US20110155850 Cross-beam and an aircraft with cross-beams of this type |
| 06/30/2011 | US20110155849 Resin infusion apparatus and system, layup system, and methods of using these |
| 06/30/2011 | US20110155847 Aft pylon fairing for an aircraft engine suspension system |
| 06/30/2011 | DE102009060706A1 Verfahren sowie Vorrichtung zur Herstellung einer Versteifungsstruktur für ein Flugzeugrumpfsegment sowie eine Versteifungsstruktur A method and apparatus for manufacturing a reinforcing structure for an aircraft fuselage segment and a reinforcing structure |
| 06/30/2011 | DE102009060693A1 Versteifungselement für ein Luftfahrzeug und Flächengebilde mit einem derartigen Versteifungselement Stiffening element for an aircraft and fabrics with such a stiffening element |
| 06/30/2011 | DE102009060606A1 Device for closing canopy of aircraft in military applications during aeronautical emergency situations, has canopy closing drive for removing canopy from aircraft after actuating release switch and releasing canopy holding device |
| 06/30/2011 | DE102009034416B4 Verfahren und Vorrichtung zur Systeminstallation sowie Frachtladesystem Method and apparatus for system installation and cargo loading system |
| 06/30/2011 | CA2784968A1 Device and method for maintaining parallelism between the two glazings of an aircraft double glazing |
| 06/30/2011 | CA2726594A1 Aircraft fuselage frame in composite material with stabilized web |
| 06/30/2011 | CA2726575A1 Aircraft fuselage frame of composite material with stabilising ribs |
| 06/29/2011 | EP2337736A2 Multifunctional cargo hold system |
| 06/29/2011 | CN201883790U Cabin door lock with automatic power failure protection function |
| 06/29/2011 | CN102112370A Protection panel and landing gear including same |
| 06/29/2011 | CN102108832A Window assembly with a motorized window shade mechanism |
| 06/29/2011 | CN101665152B Quick detachable combined cover cap capable of bearing stress |
| 06/29/2011 | CN101341067B Method for producing a fuselage cell of an aircraft |
| 06/28/2011 | US7970410 Method and apparatus for remote initiation of ARINC 615 downloads |
| 06/28/2011 | US7968170 Composite single pane window for an aircraft and method of making same |
| 06/28/2011 | US7967253 Antenna fairing and method |
| 06/28/2011 | US7967252 Fairing and airfoil apparatus and method |
| 06/28/2011 | US7967251 Truss network for aircraft floor attachment |
| 06/28/2011 | US7967250 Hybrid aircraft fuselage structural components and methods of making same |
| 06/28/2011 | US7967248 Rib element and composite flange for aircraft |
| 06/23/2011 | WO2011073315A1 Energy absorption structural element made of composite material |
| 06/23/2011 | US20110150594 Air Cargo Centerline Restraint System Having Restraints Mounted Over Floor Joists Outside the Wingbox Area for Lateral Support |
| 06/23/2011 | US20110147531 Portable onboard vehicular hoist systems |
| 06/23/2011 | US20110147530 Auxiliary fuel tank system |
| 06/23/2011 | US20110147525 Sealing of airflow between a wing and a fuselage |
| 06/23/2011 | US20110147523 Pipe coupling device for aircraft wing |
| 06/23/2011 | US20110147521 Method of constructing a fixed-wing aircraft |
| 06/22/2011 | EP2334547A1 Structural element for reinforcing a fuselage of an aircraft |
| 06/22/2011 | EP2334546A2 Panel assembly for an aircraft fuselage |
| 06/22/2011 | DE102009059720A1 Vorrichtung zur Herstellung einer aus Faserverbundwerkstoff bestehenden Rumpfschale für ein Luftfahrzeug An apparatus for producing a fiber composite material consisting of fuselage skin for an aircraft |
| 06/22/2011 | CN102105353A Structure of an aircraft aerofoil |
| 06/22/2011 | CN101648598B Novel inorganic thermal protection structure and manufacturing method thereof |
| 06/22/2011 | CN101466593B Pressure bulkhead for an aerospace fuselage |
| 06/22/2011 | CN101365625B Process and system for controlling the pressure in an aircraft cabin |
| 06/22/2011 | CN101346277B Locking device for fastening a container |
| 06/21/2011 | US7963483 Stiffening element carbon-glass layered foot section |
| 06/21/2011 | US7963482 Aircraft door |
| 06/21/2011 | CA2491186C Plate with means of fastening to a support and a sealing joint |
| 06/16/2011 | WO2011071939A2 Wing spar splice joint |
| 06/16/2011 | WO2010118448A3 Frame and method for producing such a frame |
| 06/16/2011 | US20110139940 Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle |
| 06/16/2011 | US20110139932 High pulloff capability hat stringer |
| 06/16/2011 | US20110139931 Fireproof bidirectional decompression panel |
| 06/16/2011 | US20110139927 Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment |
| 06/16/2011 | US20110139926 Landing gear with noise reduction apparatus |
| 06/16/2011 | DE102010005986A1 Method for manufacturing products, particularly cone- and truncated cone-shaped polar orthotropic hollow bodies by using endless fibers or fiber bundles, involves modifying winding angle after completion of winding of fiber layer |
| 06/16/2011 | DE102009058359A1 Krafteinleitungsbeschlag für Leichtbaukomponenten Of force fitting for lightweight components |
| 06/15/2011 | EP2331318A1 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 |
| 06/15/2011 | EP1871579B1 Use of a decorative panel based on wood, for aircraft interior design |
| 06/15/2011 | CN201864036U Vibration-attenuation noise-reduction mechanism |
| 06/15/2011 | CN102099246A Ramped stiffener and apparatus and method for forming the same |
| 06/15/2011 | CN102092474A Novel airplane |
| 06/15/2011 | CN101421157B Rotary wing vehicle |
| 06/14/2011 | US7959108 Control device for locking and unlocking and aircraft door and aircraft door that integrates such a device |
| 06/14/2011 | US7959107 Hinge device of a nacelle cowling of an aircraft engine on a supporting structure |
| 06/14/2011 | US7958801 Harmonic force generator for an active vibration control system |
| 06/09/2011 | WO2011068445A1 Dismountable helicopter |
| 06/09/2011 | WO2011066950A1 Aircraft fuselage component |
| 06/09/2011 | US20110133034 Aircraft nacelle incorporating a device for protecting an access flap for a locking system |
| 06/09/2011 | US20110133031 Cnt-tailored composite air-based structures |
| 06/09/2011 | US20110133027 Aircraft having a force transmission element between a cabin structural element and a primary structure |
| 06/09/2011 | US20110133026 Extended plug cold plate |
| 06/09/2011 | US20110133025 Acoustic attenuation panel for aircraft for engine nacelle |
| 06/09/2011 | US20110133021 Supersonic aircraft with shockwave canceling aerodynamic configuration |
| 06/09/2011 | US20110131986 Device for opening a passenger door in case of emergency |
| 06/09/2011 | DE102009057018A1 Aircraft fuselage structure has skin field, where diagonal stiffening elements are formed by skin-field polygons, and stiffening frames are designed for limiting fuselage section |
| 06/09/2011 | DE102009057012A1 Door surrounding arrangement for aircraft fuselage structure, has door surrounding structure integrally or partially integrally designed and including connecting surface, which is connectable with support surface of fuselage skin |
| 06/09/2011 | DE102009057010A1 Door panel arrangement for fuselage structure of aircraft, has door panel including rear structure with door frame, which limits door cutout for receiving aircraft door, where center section of cutout is arranged between fuselage frames |
| 06/09/2011 | DE102009056999A1 Grid-like reinforcement structure for reinforcing skin field of fuselage of aircraft, has rigid parts merged in intersection regions, and load transfer element arranged in intersection region and in active connection with parts |
| 06/09/2011 | DE102009056998A1 Reinforcement structure for sheet material for skin field of fuselage of aircraft, has stringers merged in intersection regions and defining closed meshes with different sizes, and ribs led above stringers and intersection regions |
| 06/09/2011 | DE102009056997A1 Stiffening structure, particularly for aircraft fuselage, has three-dimensional struts arranged on skin field, where struts are made of fiber-reinforced composite material |
| 06/09/2011 | DE102009056996A1 Stiffening structure for reinforcing planar structure, particularly skin field of fuselage of aircraft, comprises variety of struts with different geometries, where one strut has linear geometry |
| 06/09/2011 | DE102009056995A1 Longitudinal welded joint for two fuselage sections, particularly for airplane, comprises overlapping joint formed by two fuselage sections, where opposite braces are connected with each other |
| 06/09/2011 | DE102009056994A1 Butt joint for longitudinal welding and/or mating of two fuselage sections of aircraft, has butt strap including elevations within region of stiffeners, where elevations extend in longitudinal direction of stiffeners |
| 06/09/2011 | DE102009056978A1 Vorrichtung und Verfahren zur Herstellung einer aus einem Faserverbundwerkstoff bestehenden Rumpfschale für ein Luftfahrzeug Apparatus and method for producing a made of a fiber composite material for an aircraft fuselage shell |
| 06/09/2011 | DE102009056593A1 Installation system for connecting lines and cabin components to primary structure of aircraft, has mounting unit including adjustable reception element receiving one of two attachment elements |
| 06/09/2011 | DE102009056533A1 Flugzeugrumpfbauteil Fuselage component |
| 06/09/2011 | DE102009047340A1 Verfahren zum Bilden eines Strukturbauteils eines Luft- oder Raumfahrzeuges und Umformvorrichtung A method of forming a structural component of an aircraft or spacecraft and reshaping |
| 06/09/2011 | DE102009047040A1 Cabin for use in space vehicle, has core structure exhibiting trigger area, where structural strength of core structure is smaller than outside of trigger area in thickness direction of sandwich structure |
| 06/08/2011 | EP2328804A1 Fuselage structure for the combined fastening of an insulation mattress and devices, and aircraft including such a structure |