Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
10/2010
10/26/2010US7819363 Mobile cargo loader with a thermal curtain enclosure
10/26/2010US7819360 Window frame for aircraft
10/26/2010US7819359 Aircraft firewall
10/26/2010US7819221 Lightweight acoustic damping treatment
10/26/2010CA2577029C Compression-molded parts having an embedded conductive layer and method for making same
10/21/2010WO2010121058A2 Lightning protection sheet with patterned discriminator
10/21/2010WO2010121044A2 Lightning protection sheet with patterned conductor
10/21/2010WO2010120426A1 Metal-coated fabrics for fiber-metal laminates
10/21/2010WO2010119023A2 Method for optimising the life cycle of measurement data based on the retroaction during assembling processes whilst being produced
10/21/2010WO2010118987A2 Holding device
10/21/2010WO2010118970A1 Method and device for pre-assembling fittings for an aircraft fuselage
10/21/2010WO2010118448A2 Frame and method for producing such a frame
10/21/2010US20100266424 Inflation aspirator with collapsible barrel
10/21/2010US20100264273 Fuselage structure for an aircraft fuselage in composite material and aircraft equipped with such a fuselage structure
10/21/2010US20100264272 Aircraft structure including stiffener edge junctions
10/21/2010US20100264271 Fittings for attaching the vertical tail stabilizer of an aircraft
10/21/2010US20100264267 Fixing rail for attaching loading devices to the loading deck of an aircraft
10/21/2010US20100264266 Metal-coated fabrics for fiber-metal laminates
10/21/2010US20100264264 Method for producing an aircraft with reduced envrionmental impact and the aircraft thus obtained
10/21/2010US20100264261 Aircraft drag management structure
10/21/2010DE102010003903A1 Außenhautpaneel für einen Flugzeugrumpf For an aircraft fuselage skin panel
10/21/2010DE102009017644A1 Vorrichtung zur Verhinderung des Durchtritts von Gasen und/oder Fluiden aus einem Flügelkasten in eine Rumpfzelle eines Flugzeugs A device for preventing the passage of gases and / or fluids from a wing box in a fuselage cell of an aircraft
10/21/2010DE102009016769A1 Rumpfbugtor Rumpfbugtor
10/21/2010DE102009002404A1 Bending mount for forming base plate of cargo-hold floor of aircraft, comprises multiple profiles made of carbon-fiber reinforced plastic arranged next to each other
10/21/2010CA2758798A1 Lightning protection sheet with patterned discriminator
10/21/2010CA2758741A1 Frame and method for producing such a frame
10/20/2010EP2240364A2 Floor system for a fuselage section of an aircraft
10/20/2010EP2240363A1 Load-supporting and damage-tolerant laminated aircraft window
10/20/2010CN101868406A Method for manufacturing and attachment of wing fairings
10/20/2010CN101868405A Coupling device for joining fuselage sections, combination of a coupling device and at least one fuselage section, and method for producing said coupling device
10/19/2010US7815147 Reinforced cover for cut-outs in an aerodynamic contour
10/19/2010CA2584352C Aircraft windshield defogging/deicing system and method of use thereof
10/19/2010CA2364347C Sandwich acoustic panel
10/14/2010WO2010116168A2 Coupling assembly
10/14/2010WO2010115876A1 Center fuselage bellows
10/14/2010US20100258676 Aircraft including stiffener edge junctions and method for producing one such aircraft
10/14/2010US20100258675 Drag-Optimised Ram-Air Duct And Process For Controlling A Mass Flow Of Ambient Air Or Cooling Air Through A Ram-Air Duct
10/14/2010US20100258673 Pressure bulkhead made of composite material for an aircraft
10/14/2010CA2755879A1 Coupling assembly
10/14/2010CA2755462A1 Center fuselage bellows
10/13/2010EP2239195A1 Center fuselage bellows
10/13/2010EP2238022A2 Optimized aircraft manhole
10/13/2010EP2238021A2 Connecting arrangement for joining two stiffening elements having different cross-sectional profiles for an aircraft or spacecraft, and shell component
10/13/2010CN101861269A Interconnection device connecting an aircraft internal structure component to the fuselage of this aircraft
10/13/2010CN101856999A Element for sealing or strengthening of cavity and method for introducing penetration element in such an element
10/12/2010US7810758 Arrangement for coupling a coupling pivot for a trimmable horizontal stabiliser to the tail fuselage of an aircraft
10/12/2010US7810756 Composite internal beam for reinforcing the structure of an aircraft
10/12/2010CA2397191C Structural assembly of a part of an aircraft, in particular a rotary wing aircraft including such a structural assembly
10/12/2010CA2371335C Procedure for de-icing a jet engine air inlet cowl and device for applying the said procedure
10/07/2010WO2010113523A1 Lightning-resistant fastener, cap, and method of mounting lightning-resistant fastener
10/07/2010WO2010112742A2 Rear section of an aircraft including an engine mounting structure swingably mounted on the fuselage
10/07/2010WO2010112648A1 Integration of an aircraft fairing
10/07/2010WO2010112644A1 Structure for assembly of the pressure bulkhead of an aircraft
10/07/2010WO2010112527A2 Fuselage segment, and method for the production of a fuselage segment
10/07/2010WO2010112270A1 Aircraft comprising an insulation system for thermal and acoustic insulation
10/07/2010WO2010026524A3 Apparatus and system for providing surveillance of an area or a space
10/07/2010US20100252684 Fuselage cell structure of an airplane for the simplified installation and attachment of fasteners for fastening conduits
10/07/2010US20100252683 Conjoining of a cross beam to a structure part
10/07/2010US20100252682 Fuselage nose door
10/07/2010US20100252681 Internally stiffened composite panels and methods for their manufacture
10/07/2010US20100252679 Emergency exit hatch for exiting a cabin module in an emergency and entering the same
10/07/2010US20100252677 Aeroplane with improved acoustic comfort
10/07/2010DE102009015858A1 Verbindung eines Querträgers mit einem Strukturbauteil Compound of a cross member with a structural component
10/07/2010DE102009015856A1 Rumpfsegment und Verfahren zur Herstellung des Rumpfsegments Fuselage segment and method for producing the hull segment
10/07/2010DE102009015590A1 Luftfahrzeug mit einem Isolierungssystem zur Wärme- und Schallisolierung Aircraft with an insulation system for thermal and sound insulation
10/07/2010DE102009014933A1 Verfahren zum Toleranzausgleich zwischen zwei Bauteilen und Werkzeug zur Durchführung des Verfahrens A method for tolerance compensation between two components and tooling for performing the method
10/07/2010DE102007011621B4 Vorrichtung, insbesondere Samerstange, zur Aussteifung einer Rumpfzellenstruktur eines Luftfahrzeugs und/oder zur Befestigung eines Bauteils Device, especially Samer rod for stiffening a fuselage structure of an aircraft and / or for fastening a component
10/07/2010CA2757143A1 Fuselage segment and method for manufacturing the fuselage segement
10/07/2010CA2756345A1 Rear section of an aircraft including an engine mounting structure swingably mounted on the fuselage
10/07/2010CA2755705A1 Lightning-resistant fastener, cap, and method of mounting lightning-resistant fastener
10/07/2010CA2755378A1 Aircraft with an insulation system for thermal and acoustic insulation
10/06/2010EP2236730A2 Blind assembly, in particular for an aircraft window, including means for maintaining the tension thereof
10/06/2010EP2236729A2 Blind assembly with two screens, in particular for an aircraft window
10/06/2010EP2236412A2 Aircraft insulation systems and methods
10/06/2010EP2236411A1 Locking device for an aircraft door
10/06/2010EP2234875A1 Acoustically attenuated fuselage for aircraft
10/06/2010EP2234874A1 Pressurised aircraft carrier with open air exposure flap
10/06/2010CN201597751U 飞机舱盖玻璃边缘软连接结构 Aircraft hatch glass edge flexible connecting structure
10/06/2010CN101855132A Aircraft assembly
10/06/2010CN101850842A Aircraft insulation systems and methods
10/06/2010CN101850841A Aerial organic glass window and manufacturing method thereof
10/06/2010CN101462594B Aerocraft capable of concealing laterally and method for manufacturing the same
10/06/2010CN101222999B Method for connection of at least two pieces of sheet material, particularly at least two metal sheets for a lightweight structure as well a joining and lightweight structure
10/05/2010US7806368 Aerial sensor pod deployment system
10/05/2010CA2473891C Joint for connecting components together on opposite longitudinal sides in addition to a flexible strip used for said joint
09/2010
09/30/2010WO2010110964A1 Integrated aircraft floor with longitudinal beams
09/30/2010WO2010109046A1 Joint arrangement of structural elements of a composite material
09/30/2010WO2010108842A1 Aeroplane structure comprising air guiding shafts built into structural elements
09/30/2010WO2010063627A3 Shell component for an aircraft or spacecraft
09/30/2010WO2010060908A3 Planar component of an aircraft and method for producing the same
09/30/2010WO2010046276A4 Multifunctional cargo hold system
09/30/2010US20100247903 Part of composite material having a wedge between two zones
09/30/2010US20100247848 Sandwich element for sound-absorbing inner cladding of transport means, especially for sound-absorbing inner cladding of aircraft fuselage cells
09/30/2010US20100243814 Emergency Evacuation System, in Particular for a Tailless Aeroplane
09/30/2010US20100243810 Integrative structure for aircraft fairing
09/30/2010US20100243809 Opening plug and method of installing the same
09/30/2010US20100243807 Aircraft insulation systems and methods
09/30/2010US20100243806 Aircraft pressure bulkhead assembly structure
09/30/2010US20100243805 Structural Element of an Aircraft Fuselage
09/30/2010US20100243804 Joint arrangement for composite-material structural members
1 ... 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 ... 126