Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
12/2010
12/02/2010DE102009022715A1 Component for aircraft, has reinforcement arranged in edge area such that edge area exhibits larger wall thickness than wall area, where wall area is attached to side that is turned away from component edge at edge area
12/02/2010CA2763531A1 Aircraft including supporting floor beams and bearings comprising a flexible material and connecting the floor beam to the mounting
12/02/2010CA2763113A1 Structural component and production method for a structural component
12/01/2010EP2256031A2 Stringer transition and method for producing the same
12/01/2010EP2256030A1 Aircraft assembly
12/01/2010EP2254789A1 Aircraft opening panel, especially an airplane cabin door
12/01/2010EP2254788A2 Method for producing a fibre composite component fibre composite component and a fibre composite fuselage component of an aircraft
12/01/2010EP2167376B1 Reduced dimension landing gear casing
12/01/2010EP2054296B1 Frame element, aircraft component assembly system and method of fitting a component in an aircraft
12/01/2010EP1960261B1 Aircraft with modular structure
12/01/2010CN201660123U Helicopter cockpit floor integrated and connected with frame beam
12/01/2010CN101903238A Aircraft structure including stiffener edge junctions
11/2010
11/30/2010CA2416809C Hybrid air vehicle
11/28/2010CA2700796A1 Stringer transition and method for producing composite parts using the same
11/25/2010WO2010106271A3 Under-flap stiffener for aircraft
11/25/2010WO2010100059A3 Connection system, and especially adapter module provided therefor
11/25/2010US20100294889 Device for joining torsion boxes of aircraft
11/25/2010US20100294888 Aircraft opening panel, especially an airplane cabin door
11/25/2010US20100294887 Pressurised aircraft door equipped with a vent flap
11/25/2010US20100294884 Attachment arrangement for a cargo compartment floor of an aircraft and aircraft with an attachment arrangement of this type
11/25/2010DE102009003278A1 Aircraft floor for use in aircraft, has multiple segments coupled one another in such manner that segments have translational degree of freedom against each other in direction of longitudinal axis of aircraft
11/24/2010EP2253539A2 Breather duct shielding
11/24/2010EP2253538A2 A gas turbine engine having a nacelle and a breather duct
11/24/2010EP2252505A1 Device for opening a passenger door in case of emergency
11/24/2010EP2252504A1 Fuselage structure for airplane
11/24/2010CN201647121U Inflatable flexible ailerons
11/24/2010CN201647120U V-shaped airplane
11/24/2010CN101896400A Split handle for aircraft door
11/24/2010CN101896399A Aircraft including stiffener edge junctions and method for producing one such aircraft
11/24/2010CN101896398A Method for the production of a fuselage airframe of an aircraft
11/24/2010CN101891016A Invisible autogyro
11/23/2010US7837808 Process for manufacturing structural components by machining plates
11/23/2010US7837148 Composite wing-body joint
11/23/2010US7837147 Systems and methods for reducing noise in aircraft fuselages and other structures
11/23/2010CA2537945C A resin infused transparent skin panel and method of making same
11/18/2010WO2010130687A2 Method for producing an aircraft fuselage and aircraft fuselage
11/18/2010WO2010104817A3 Method of applying an electric conductive layer to selected portions of a mounting frame
11/18/2010WO2010063627A4 Shell component for an aircraft or spacecraft
11/18/2010DE102009021369A1 Verfahren zur Herstellung eines Flugzeugrumpfes und Flugzeugrumpf A process for producing an aircraft fuselage and the fuselage
11/18/2010DE102009020896A1 Missile has base structure, which has energy absorption device serving tossed element and upsetting element, which is arranged in a crash effective range of tossed element
11/18/2010DE102009020891A1 Missile for use in e.g. aircraft, has cross brace dividing triangular cross section region into reinforcement region above cross brace and energy absorption region below cross brace
11/18/2010DE102008058451B4 Verfahren und System zur Notbelüftung einer Flugzeugkabine im Fall eines Lecks im Bereich eines Luftmischers Method and system for emergency ventilation of an aircraft cabin in the event of a leak in the region of an air mixer
11/18/2010CA2761654A1 A method for the manufacture of an aircraft fuselage, and an aircraft fuselage
11/17/2010EP1917185B1 Sound-absorbing element for transport means, in particular for aircraft
11/17/2010CN201633920U Aircraft bulkhead
11/17/2010CN201633919U Cabin door stay bar for airplane
11/17/2010CN201633918U Passenger-cargo mixed airplane passenger cabin
11/17/2010CN101885380A Asymmetrical design method for leading edge of hypersonic vehicle
11/16/2010US7832686 Combined displacement and swivel mechanism
11/16/2010CA2407406C Joint construction in a laminate of metal and plastic layers
11/11/2010WO2010129210A2 Supersonic flying wing
11/11/2010WO2010100057A3 Connecting device
11/11/2010WO2010099052A3 Distributing power in systems having a composite structure
11/11/2010US20100282918 Saucer shaped gyroscopically stabilized vertical take-off and landing aircraft
11/11/2010US20100282909 Elastomeric riblets
11/11/2010US20100282908 Methods for Reducing Laminar Flow Disturbances on Aerodynamic Surfaces and Articles having Self-Cleaning Aerodynamic Surfaces
11/11/2010US20100282907 Sealing system for the gap existing between the fuselage and the elevator of the orientable horizontal stabiliser of an aircraft, extended with an aerodynamic fairing for sealing of the opening existing between the fuselage and the orientable horizontal stabiliser
11/11/2010US20100282906 Multi-layer metal/shape memory polymer roll-up wing structures for fitment-constrained air vehicles
11/11/2010US20100282905 Splicing of omega-shaped stiffeners at a circumferential joint in an aircraft fuselage
11/11/2010US20100282904 Aircraft having a forward-facing section that deflects elastically under impact loads
11/11/2010US20100282903 Aircraft pressurized floor
11/11/2010US20100282900 System for Reducing Aerodynamic Noise at a Supplementary Wing of an Aircraft
11/11/2010DE102009020274A1 Verriegelung für eine Flugzeugtür Lock for an aircraft door
11/11/2010DE102009019434A1 Flugzeugtür und Verfahren zur Herstellung einer derartigen Flugzeugtür Aircraft door and method for manufacturing such aircraft door
11/11/2010DE102009002745A1 Fastening arrangement for cargo compartment floor of airplane, has multiple floor panels to form cargo compartment floor, transverse profile running transverse to longitudinal axis of airplane and multiple channels
11/10/2010EP2247496A1 Interconnection and aircraft or spacecraft having such an interconnection
11/10/2010CN101883717A Coupling element for connecting two longitudinal stiffening elements
11/09/2010US7828248 Aircraft walkway
11/09/2010US7828246 Wing with sectioned tubular members
11/09/2010CA2482247C Perforated skin structure for laminar-flow systems
11/04/2010US20100276545 Aerodynamic and Spatial Composite Flight Aircraft, and related Piloting Method
11/04/2010US20100276543 Aircraft door and a method for the manufacture of an aircraft door of this type
11/04/2010US20100276538 Cargo aircraft system
11/03/2010EP2244939A1 Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle
11/03/2010CN201619689U Tubular framed cabin edge connection structure
11/03/2010CN101875398A Multi-redundancy rotary motor-driven mechanism for driving airplane exhaust valve
11/03/2010CN101486265B Cumulative cutter shielding composite material for aerobus serving cabin door air emergency opening
11/03/2010CN101291846B Aircraft safety system
11/02/2010US7823835 Door pod assembly
11/02/2010US7823834 Door configured to close an opening inside an aircraft
11/02/2010US7823833 Window installation method and apparatus
11/02/2010US7823832 Injection-molded window panel and related methods
11/02/2010US7823830 Aircraft luggage compartment
11/02/2010US7823829 Equipment fastening device to enhance the crash safety of an aircraft
10/2010
10/28/2010WO2010123771A1 Composite laminate for a thermal and acoustic insulation blanket
10/28/2010WO2010122200A2 Metal fittings for engaging the vertical tailplane of an aircraft
10/28/2010US20100270430 Device and method for providing radiation occlusion and aero-thermal protection
10/28/2010US20100270429 Equipment element with retractable line
10/28/2010US20100270427 Bird collision prevention device for an aircraft
10/28/2010US20100270423 Planetary de-rotation system for a shaft fairing system
10/28/2010DE102009017977A1 Haltevorrichtung für innerhalb eines Flugzeugrumpfs verlegte Anbauteile Holding device for routed within an aircraft fuselage attachments
10/28/2010DE102006056442B4 Türschloss für Türen von Luftfahrzeugen, insbesondere von Hubschraubern Door lock for doors of aircraft, especially helicopters
10/28/2010CA2759753A1 Fittings for attaching the vertical tail stabilizer of an aircraft
10/28/2010CA2756817A1 Composite laminate for a thermal and acoustic insulation blanket
10/27/2010EP2243701A2 Impact-absorbing structure and method for producing the same
10/27/2010EP2242683A1 Unitary, self-stiffened, and pivoting composite panel, in particular for a mobile part of an aircraft
10/27/2010EP2242682A1 Method of connecting two fuselage sections with the formation of a transverse joint, and transverse joint connection
10/27/2010EP2019776B1 Aircraft comprising a device for reducing the induced drag
10/27/2010EP1762666B1 Composite beam with corrugated web
10/27/2010CN101873965A Splicing of omega-shaped stiffeners at a circumferential joint in an aircraft fuselage
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