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)
03/2010
03/31/2010EP2167378A1 Differential pressure-controlled locking mechanism
03/31/2010EP2167377A1 Corrosion-resistant connection between a first component and a second component
03/31/2010EP2167376A1 Reduced dimension landing gear casing
03/31/2010CN201432797Y Inflatable fuselage
03/31/2010CN201432796Y Aircraft with safety protection device
03/31/2010CN101689211A Method for designing part made from composite material and having a curved surface
03/31/2010CN101687541A Aircraft structural element located at the interface between a wing and the fuselage
03/31/2010CN101687540A Compliant panel for aircraft
03/31/2010CN101687539A Method for coupling stiffening profile elements and structural component
03/31/2010CN101687538A Gap covering device
03/31/2010CN101687287A Method for producing a composite skin in the field of aeronautics and astronautics
03/30/2010US7686251 Rib support for wing panels
03/30/2010US7686250 Electronic display mount
03/30/2010US7686249 Integral frame member for an aircraft
03/30/2010US7686248 System and method for internal passive cooling of composite structures
03/30/2010US7686245 Rotary aircraft download alleviation apparatus and methods
03/30/2010CA2293076C Fan and compressor noise attenuation
03/25/2010WO2009134513A3 Aircraft flight termination system and method
03/25/2010WO2009124832A4 Aircraft having a force transmission element between a cabin structural element and a primary structure
03/25/2010US20100075090 improving the strength and stiffness, using polymeric matrix having low-density region including glass elements having a first packing density, and high-density region including glass elements having having a second packing density greater than the first packing density; window border
03/25/2010US20100072319 Landing gear casing provided with a box structure
03/25/2010DE102008062477B3 Fiber-reinforced composite component e.g. wing, manufacturing method for aircraft, involves removing body-shell component by blowing lifting pad, and controlling blowing of lifting pad by arithmetic unit
03/25/2010DE102008047001A1 Clamping beam, has pressure pipes for applying tensile pre-stress on outer layer parallel to beam longitudinal axis, and vertical frames connected together via single-axial force transmission element running within outer layer
03/25/2010DE102008042036A1 Stange zur Abstützung von Bauteilen innerhalb einer Rumpfzellenstruktur eines Flugzeugs Rod for support of components within a fuselage structure of an aircraft
03/25/2010DE102008041317A1 Anbindung einer Tragfläche an eine Rumpfzelle eines Flugzeugs Connecting a wing to fuselage airframe of an aircraft
03/24/2010EP2164754A2 Method for coupling stiffening profile elements and structural component
03/24/2010CN101678891A Reinforced panel
03/24/2010CN101678890A Shaped composite stringers and methods of making
03/24/2010CN101678889A Connecting device for connecting two curved ribs of an aircraft or spacecraft
03/24/2010CN101678888A Method of extending length of aircraft to increase interior space
03/24/2010CN100595107C Door for closing an opening inside an aircraft
03/24/2010CN100595106C Composite anti-crash structure with lateral restraint for aircraft
03/23/2010US7682682 Stiffener stop with staggered slopes and panel fitted with such a stop
03/23/2010US7681837 Method and apparatus for closing a swing tail on an aircraft
03/23/2010US7681836 Aircraft comprising a device for detection and/or measurement of atmospheric disturbances
03/23/2010US7681835 Single piece co-cure composite wing
03/23/2010US7681834 Composite missile nose cone
03/23/2010CA2313260C Acoustic liner and method of making an acoustic liner
03/18/2010WO2010028956A2 Rod for supporting components in a fuselage cell structure of an aircraft
03/18/2010WO2010004121A3 System for securing insulating mats and method of installing insulating mats in an aircraft fuselage
03/18/2010WO2009148670A3 Modularized airplane structures and methods
03/18/2010WO2009138546A3 Integrated aircraft structure in composite material
03/18/2010US20100065689 Load introducing element
03/18/2010US20100065688 Method and apparatus for reinforcing composite structures
03/18/2010US20100065687 Aircraft structure
03/18/2010US20100065686 Aircraft heated floor panel
03/18/2010US20100065685 Pressure bulkhead for an aerospace fuselage
03/18/2010US20100065681 Floor Structure in an Aircraft With Continuous Panels
03/18/2010US20100065680 Device with plane jets for reducing the noise generated by a jet aircraft
03/18/2010US20100064473 Attachment Bolt And Tensioned Support System Using Same
03/18/2010DE102008044461A1 Konstruktionsprinzip und Verfahren zum Aufbau von Klein-Luftfahrzeugen Design principle and method of construction of small aircraft
03/18/2010DE102005038857B4 Doppelschalig aufgebauter Mittelkasten Double Walled constructed center box
03/18/2010DE102004009967B4 Kabelhalter für ein Flugzeug, Kabelhalterkit und Flugzeug mit einem Kabelhalter Cable holder for an aircraft, and aircraft Kabelhalterkit with a cable holder
03/18/2010CA2735078A1 Rod for supporting components in a fuselage cell structure of an aircraft
03/17/2010EP2162350A1 Method of forming panels using an in-situ tape placement process and panels formed therefrom
03/17/2010CN101674978A Structural element of an aircraft fuselage
03/17/2010CN101674929A Composite structure comprising a stringer with a pad embedded in the recess of a panel and method of transmitting forces
03/17/2010CA2678321A1 Load introducing element
03/16/2010US7677499 Aircraft wing coupling arrangement
03/16/2010US7677498 Device and method for fastening an aircraft radome
03/16/2010US7677497 Hatch-actuating mechanism, particularly for an aircraft landing gear
03/16/2010US7677496 Stringer for an aircraft wing and a method of reinforcing thereof
03/16/2010US7677494 Boarding ramp device for aircraft
03/11/2010WO2010025860A2 Main body for aircraft
03/11/2010US20100064197 Random-access multi-directional cdma2000 turbo code interleaver
03/11/2010US20100059629 System and Method for Fabricating Composite Parts
03/11/2010US20100059628 Slide door device for aircraft
03/11/2010US20100059627 Aircraft with a Rear Fuselage Protection Shield
03/11/2010US20100059626 Fuselage arrangement for airplane
03/11/2010US20100059625 Front portion for an aircraft including a rest compartment for at least one pilot
03/11/2010DE102008045793A1 Rotary visible window for use on safety laminated glass pane of machine tool, has rotor and/or rotor window exchanged by removing fixing bolt, and magnet fastened to rotor by shifting magnet towards rotation axis into coil units
03/11/2010DE102008044759A1 Stütze für ein im Selective Laser Melting-Verfahren herstellbares Flugzeugstrukturbauteil Support for a manufacturable in selective laser melting process aircraft structural component
03/11/2010DE102008041788A1 Sandwichplatte mit integrierter Verstärkungsstruktur sowie Verfahren zu deren Herstellung Sandwich panel with integrated reinforcement structure as well as processes for their preparation
03/11/2010DE102008041172A1 Light-weight construction structure for an airplane, comprises components connectable by using a weld joining process, which is a friction stir welding process, a laser beam welding process and/or a fusion welding process
03/10/2010CN201419796Y Unmanned aircraft
03/10/2010CN201419795Y Unmanned aerial photography aircraft
03/10/2010CN101668679A Wing-fuselage section of an aircraft
03/10/2010CN101665152A Quick detachable combined cover cap capable of bearing stress
03/10/2010CN101665151A Local detachable architrave
03/09/2010US7674417 Method of manufacturing window having at least one of radio wave stealth property and electromagnetic wave shield property, and window material having at least one of radio wave stealth property and electromagnetic wave shield property
03/04/2010WO2010025376A1 Method of fabricating structures using composite modules and structures made thereby
03/04/2010WO2010024990A1 Composite tie rod and method for making the same
03/04/2010WO2010023059A2 Support for a aircraft structural component produced in a selective laser melting method
03/04/2010WO2010004159A3 Reinforced aircraft fuselage panel and method of manufacture.
03/04/2010WO2010004157A3 Aircraft fuselage element
03/04/2010US20100051753 Wall effects on vtol vehicles
03/04/2010US20100051748 Flush-mounted latching assembly and method of assembling same
03/04/2010US20100051747 Leaktight frame for a window and a mechanical assembly provided with such a frame
03/04/2010US20100051746 System and method for integrating handicapped accessible seats into aircraft interior configurations
03/04/2010US20100051743 Rear lower aerodynamic fairing for the attachment device of an aircraft engine
03/04/2010US20100051741 Unmanned air vehicle
03/04/2010US20100051167 Optimizing the shape of a composite structure
03/04/2010DE102008041173A1 Rumpfsektion mit integralem Druckschott sowie Rumpfschale mit einer derartigen Rumpfsektion Fuselage section with integral pressure bulkhead and hull with such a fuselage section
03/04/2010CA2735435A1 Method of fabricating structures using composite modules and structures made thereby
03/04/2010CA2732934A1 Support for an aircraft structural component produced in a selective laser melting method
03/03/2010EP2159154A1 Sealed window frame
03/03/2010EP2158125A2 Method and device for producing a fuselage cell of an airplane
03/03/2010CN101663197A Device for attaching a lift member to the fuselage of an aircraft
03/03/2010CN101663196A Fuselage of an aircraft or spacecraft and corresponding aircraft or spacecraft
03/02/2010US7669800 Reinforced cover for gaps in an aerodynamic contour
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