| Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
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| 07/16/2009 | US20090179111 Interior panel attachment system |
| 07/16/2009 | US20090179110 Extended Decompression Flap Arrangement |
| 07/16/2009 | DE102007061804A1 Connecting elements for connecting two components in aircraft, particularly airplane, have actuator, which is controlled by electrical signal, where connecting elements compensate temperature-induced elongation of component |
| 07/15/2009 | EP2077962A1 Combined thermal protection and surface temperature control system |
| 07/15/2009 | EP2077942A1 Stiffened casing for an aircraft or spacecraft with a laminate stringer of high rigidity and corresponding laminate stringer |
| 07/15/2009 | CN101481013A Power installation for emergency opening of service door during passenger plane trial flight |
| 07/15/2009 | CN101481012A Safeguard structure of passenger plane service module for exploding and cutting covering during aerial emergency pressure relief |
| 07/14/2009 | US7561947 Dynamic CMG array and method |
| 07/14/2009 | CA2484180C Magnetic indexer for high accuracy hole drilling |
| 07/14/2009 | CA2362235C Fibre reinforced composites and method of making same |
| 07/09/2009 | WO2009084411A1 Heat-insulating sound-absorbing material with high heat resistance |
| 07/09/2009 | WO2009083575A2 Optimized aircraft manhole |
| 07/09/2009 | WO2009083262A2 Wing-fuselage structural component for the connection of two airfoils and a fuselage section on an aircraft |
| 07/09/2009 | WO2009062712A4 Coupling element for interconnecting two longitudinal reinforcing elements |
| 07/09/2009 | US20090176426 electrically insulant, compressible impermeable cloth formed by impregnating an electrically insulant woven fiber with a sealant, and curing; airframe structures may be assembled by positioning the cloth between a substructure and an outer skin on substructure, and assembling outer skin to substructure |
| 07/09/2009 | US20090173828 Fastener |
| 07/09/2009 | US20090173827 Method and apparatus for monitoring the integrity of components and structures |
| 07/09/2009 | US20090173826 Trapezoidal panel pin joint allowing free deflection between fuselage and wing |
| 07/09/2009 | US20090173825 Aircraft door with oversizing |
| 07/09/2009 | US20090173824 Closure system for a support structure |
| 07/09/2009 | US20090173823 Method and component for determining load on a latch assembly |
| 07/09/2009 | DE102007061253A1 Flugzeugrumpfelement Fuselage element |
| 07/09/2009 | CA2711105A1 Structural wing-fuselage component for connecting two wings to a fuselage section on an aircraft |
| 07/08/2009 | EP2076430A2 Aircraft fuselage made from longitudinal panels and method of producing such a fuselage |
| 07/08/2009 | EP1957216B1 Method of superplastic forming of titanium assemblies and aircraft structure manufactured thereby |
| 07/07/2009 | US7556462 Cargo deck |
| 07/07/2009 | US7556220 Seal for sealing a component opening in a component |
| 07/07/2009 | US7555873 Self-locating feature for a pi-joint assembly |
| 07/02/2009 | WO2009081020A1 Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle |
| 07/02/2009 | WO2009080385A1 Safety cabin |
| 07/02/2009 | US20090166475 Apparatus for the pivotal fastening of an active surface, in particular a spoiler on a wind tunnel model of an aircraft |
| 07/02/2009 | US20090166474 Baggage Accommodation Device |
| 07/02/2009 | US20090166473 Optimized aircraft manhole |
| 07/02/2009 | US20090166472 Floor plate for covering a floor framework in an aircraft |
| 07/02/2009 | US20090166471 Fuselage Structure and Method for the Production of a Fuselage Structure |
| 07/02/2009 | DE202008017047U1 Cockpitbeschattung für Tiefdeckersportflugzeuge und Segelflieger Cockpit shading for low wing sport aircraft and gliders |
| 07/02/2009 | DE102008025389A1 Verfahren zum Isolieren einer Flugzeugkabinenwand bzw. zum Abkühlen oder Aufwärmen von Flugzeugkabinenluft und dazu geeignete Flugzeugkabinenwand A method for isolating an aircraft cabin wall or cooling or warming of aircraft cabin air and to appropriate aircraft cabin wall |
| 07/02/2009 | DE102007061433A1 Verbesserte Dekompressionseinrichtung mit einem einstellbaren Auslösedruck Improved decompression with an adjustable trigger pressure |
| 07/02/2009 | DE102007061429A1 Hull structure for aircraft, has structural components connected with outer skin, and inner lining forming supporting structure with outer skin and structural components, where stringers and frames are formed as hollow sections |
| 07/02/2009 | DE102007061425A1 Holder for fixing e.g. electrical line, in fuselage cell structure of aircraft, has upper part connected with lower part enclosing head region of ring pants for fixing holder, where upper part and/or lower part includes functional element |
| 07/02/2009 | DE102007061423A1 Sicherheitskabine Safety Enclosure |
| 07/02/2009 | CA2709331A1 Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle |
| 07/02/2009 | CA2707985A1 Safety cabin |
| 07/01/2009 | EP2074024A1 Self-supporting interior cabin structure with integrated installation elements |
| 07/01/2009 | CN101472794A Assembling principle for aerial vehicle airframe |
| 06/30/2009 | US7553533 High-damping absorbing coating |
| 06/30/2009 | US7552896 Aircraft window assembly |
| 06/30/2009 | CA2419444C Apparatus and method for joining dissimilar materials to form a structural support member |
| 06/25/2009 | WO2009056729A3 Curved parts made of composite with stiffeners |
| 06/25/2009 | US20090159750 Holder for fixing components, in particular lines, inside an aircraft without using holes |
| 06/25/2009 | US20090159749 Connector element for connecting two component parts |
| 06/25/2009 | US20090159748 Decompression Device With Adjustable Release Pressure |
| 06/25/2009 | US20090159747 Aircraft Fuselage Element |
| 06/25/2009 | US20090159746 Hull structure |
| 06/25/2009 | US20090159745 Aircraft stringer clip and related methods |
| 06/25/2009 | US20090159744 System box for accommodating aircraft systems |
| 06/24/2009 | CN201261545Y Once solidified and molded fuselage ring and covering |
| 06/24/2009 | CN101466595A Composite wing-body joint |
| 06/24/2009 | CN101466594A Tail structure for an aircraft or spacecraft |
| 06/24/2009 | CN101466593A Pressure bulkhead for an aerospace fuselage |
| 06/24/2009 | CN101466592A Aircraft fuselage structure and method for its production |
| 06/24/2009 | CN100503861C High-damage tolerant aluminium alloy product in particular for aerospace applications |
| 06/23/2009 | CA2343622C Device for pressure tapping and procedure for setting it on fuselage panel of an aircraft |
| 06/18/2009 | WO2009074669A1 Acoustically attenuated fuselage for aircraft |
| 06/18/2009 | WO2009056643A3 Structure, especially a fuselage structure of an aircraft or a spacecraft |
| 06/18/2009 | WO2009053645A3 Splicing of omega-shaped stiffeners at a circumferential joint in an aircraft fuselage |
| 06/18/2009 | WO2009053040A4 Aircraft component mounting system |
| 06/18/2009 | WO2009051875A3 Aircraft door and method for using the same |
| 06/18/2009 | WO2009042549A3 Method for manufacturing and attachment of wing fairings |
| 06/18/2009 | US20090155014 Expandable collet anchor system and method |
| 06/18/2009 | US20090152400 Acoustically attenuated fuselage for aircraft |
| 06/18/2009 | US20090152399 Line system arrangement in an aircraft or spacecraft having a fuselage |
| 06/18/2009 | US20090152398 Device for limiting the deflection of a door arranged in a fuselage cell of an aircraft |
| 06/18/2009 | US20090152397 Selective release latch |
| 06/18/2009 | US20090152395 Absorbent structure for attenuating noise particular by a rotor-generator noise, and a rotor duct including such a structure |
| 06/18/2009 | US20090152392 Parametric geometry model for a blended wing body |
| 06/18/2009 | DE202008015039U1 Hubschrauber variabler Konfiguration und Container-Betrieb mit PU-System Helicopter variable configuration and container-operation with PU system |
| 06/18/2009 | DE102007060668A1 Sandwichpaneel zur Schallabsorption Sandwich panel for sound absorption |
| 06/18/2009 | DE102007060662A1 Sandwichpaneel zur Schallabsorption Sandwich panel for sound absorption |
| 06/18/2009 | DE102007060029A1 Verfahren und Vorrichtung zur Herstellung röhrenförmiger Strukturbauteile Method and apparatus for producing tubular structural components |
| 06/18/2009 | CA2709235A1 Acoustically attenuated fuselage for aircraft |
| 06/17/2009 | EP2070974A2 Metal impregnated composites and methods of making |
| 06/17/2009 | EP2070816A2 Methods and apparatus for an integrated aerodynamic panel |
| 06/17/2009 | EP2070815A2 Ducted fan vehicles particularly useful as VTOL aircraft |
| 06/17/2009 | EP2070688A2 Aircraft structures bonded with adhesive including magnetostrictive material |
| 06/17/2009 | EP2069198A1 A door for opening and closing a door aperture in an aircraft |
| 06/17/2009 | EP2069130A2 Improved composite resin window frame construction for airplanes and method of producing the same |
| 06/17/2009 | EP1694560A4 Area ruling for supersonic vehicles |
| 06/17/2009 | CN101460358A Fuselage structure and method for the production of a fuselage structure |
| 06/16/2009 | US7546979 Trapezoidal panel pin joint allowing free deflection between fuselage and wing |
| 06/16/2009 | US7546864 Stiffening means for structural components, method of manufacturing and apparatus therefor |
| 06/16/2009 | US7546756 Method for processing a metal slab or billet, and product produced using said method |
| 06/16/2009 | CA2402848C K-spar configuration for bonded wing construction |
| 06/11/2009 | WO2009050358A3 Aircraft structure including stiffener edge junctions |
| 06/11/2009 | WO2009050357A3 Aircraft including stiffener edge junctions and method for producing one such aircraft |
| 06/11/2009 | WO2008102278A9 Multi deck aircraft |
| 06/11/2009 | WO2005096770A3 Novel method to secure airline and other carrier travel |
| 06/11/2009 | US20090146009 Actuating Device |
| 06/11/2009 | US20090146008 Door Frame Compartment of Cast Titanium and Structural Fuselage Part |
| 06/11/2009 | US20090146007 Methods and Systems for Attaching Aircraft Wings to Fuselages |