Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
12/2005
12/27/2005US6980104 Aircraft with security alarm system
12/27/2005US6979377 Method for producing components from fiber-reinforced composite ceramic and methods for using the components
12/22/2005WO2005121596A1 High-damping absorbing coating
12/22/2005WO2005047102A3 Systems and methods for configuring aircraft to meet performance goals and shock wave disturbance constraints
12/22/2005US20050280897 Stowable laser eye protection
12/22/2005US20050279887 Aircraft partition designed to separate a cargo part from a cockpit or from a passenger compartment
12/22/2005US20050279886 Jittie Blocker / Shield
12/22/2005DE102004026835A1 Verbundstoffbauteil und Verfahren zu seiner Herstellung Composite member, and process for its preparation
12/22/2005DE102004025381A1 Manufacturing window frame for installation in exterior shell of aircraft involves providing semifinished part composed of multiple, individual substructures
12/22/2005DE102004025380A1 Window frame for aircraft, is made from resin reinforced with unidirectionally-arranged fiber bundles
12/22/2005DE102004025378A1 Window frame for aircraft, is made from resin reinforced with unidirectionally-arranged fiber bundles
12/22/2005DE102004025377A1 Window frame for aircraft has vertical flange perpendicularly arranged between outer flange and inner flange such that flanges are made of fiber-reinforced resin
12/22/2005DE102004025376A1 Window frame for aircraft has vertical flange perpendicularly arranged between outer flange and inner flange such that flanges are made of fiber-reinforced thermoplastic material
12/22/2005DE102004025375A1 Window frame for aircraft, includes holder units set equidistant to each other at outer flange, and having pins extending perpendicular from base plate and mutually engaged with downholder clips
12/21/2005EP1607655A1 Impact energy absorber
12/21/2005EP1607576A2 Airfoil cooling passageway turn and manufacturing method therefore
12/21/2005EP1154900B1 Composite laminates
12/21/2005CN2747160Y Cabin able to keep pilot in horizontal posture
12/20/2005US6976658 Cockpit door of aircraft
12/20/2005US6976654 Vertical takeoff and landing aircraft
12/20/2005CA2398218C Emergency vision apparatus
12/15/2005WO2005118391A1 Air freight transport method, transport aeroplane and air freight transport system
12/15/2005WO2005049422A3 Aircraft
12/15/2005US20050278085 System and method with adaptive angle-of-attack autopilot
12/15/2005US20050276698 Cooling passageway turn
12/14/2005EP1311768B1 Apparatus and method for joining dissimilar materials to form a structural support member
12/08/2005WO2005115841A1 Window frame for aircraft
12/08/2005WO2005115840A1 Window frame for aircraft
12/08/2005WO2005115839A1 Window frame for aircraft
12/08/2005WO2005115838A1 Window frame for aircraft
12/08/2005WO2005115837A1 Window frame for aircraft
12/08/2005WO2005115836A1 Window frame for aircraft
12/08/2005WO2005115728A1 Method for making window frame
12/08/2005WO2005056383A3 A resin infused transparent skin panel and method of making same
12/08/2005US20050273259 Passive measurement of terrain parameters
12/08/2005US20050272483 Electronic device
12/08/2005US20050269452 Vehicle safety
12/08/2005US20050269451 Flight passenger seat with an integrated spring element
12/08/2005CA2565495A1 Window frame for aircraft
12/08/2005CA2564781A1 Window frame for aircraft
12/08/2005CA2564417A1 Window frame for aircraft
12/08/2005CA2564173A1 Window frame for aircraft
12/08/2005CA2564167A1 Window frame for aircraft
12/08/2005CA2563574A1 Method for making window frame
12/08/2005CA2563441A1 Window frame for aircraft
12/07/2005EP1601572A1 Device for the fixing of air cargo netting to air cargo palettes
12/07/2005CN2744599Y Heat protection device for pneumatic heating heated-surface of superhigh speed aircraft
12/06/2005US6971689 Flush handle assembly
12/06/2005US6971608 Integrated transport system and method for overhead stowage and retrieval
12/06/2005CA2107809C Double configuration emergency exit for land evacuation and following alighting on water of an aircraft cabin
12/01/2005WO2005113333A2 Load bearing window
12/01/2005WO2005068289A3 Fuselage
12/01/2005US20050265038 Laminate material component and method for its production
12/01/2005US20050263950 Process and device for localized gripping and holding of a thin, flexible panel, in particular having a complex shape
12/01/2005US20050263645 Structural panels for use in aircraft fuselages and other structures
12/01/2005US20050263254 Window shade positioning apparatus and method
12/01/2005DE10116224B4 Verfahren und Vorrichtung zur Verstellung einer türseitigen Sicherungseinrichtung einer Flugzeugtür Method and apparatus for adjusting a door-side safety device of an aircraft door
11/2005
11/30/2005EP1600316A1 Window shade positioning apparatus
11/30/2005EP1600246A1 Titanium-Aluminium-component
11/30/2005EP1417535B1 Switchable electrochromic devices
11/29/2005US6970773 Apparatus and method for reducing induced drag on aircraft and other vehicles
11/29/2005US6969029 Methods and systems for removing material from aircraft flight surfaces
11/24/2005WO2005111529A2 System and method with adaptive angle-of-attack autopilot
11/24/2005WO2005110843A2 Architectural archway for an aircraft
11/24/2005WO2005110842A2 Airfoil box and associated method
11/24/2005US20050260051 Process and device for machining by windowing of non-deformable thin panels
11/24/2005US20050258309 Efficient cargo liner installation
11/24/2005DE10327404B4 Mechanismus zum Öffnen bzw. Schließen einer Passagiertür eines Flugzeuges Mechanism for opening and closing a passenger door of an aircraft
11/24/2005DE102005019194A1 Flugzeug-Frachtladelogistiksystem Aircraft cargo loading logistics system
11/24/2005DE102004021513A1 Suspension clamping holder e.g. for support structure, has free carrier, support and clamping valve with free carrier laterally at upper end of support and perpendicularly formed with support having back with carrier extension
11/24/2005DE102004018736A1 Verbindungselement Connecting element
11/24/2005DE10116216B4 Vorrichtung zum Bewegen einer an einem Tragarm schwenkbar gelagerten Flugzeugtür An apparatus for moving a pivotably mounted on a support arm aircraft door
11/23/2005EP1598270A2 Aircraft passenger seat with integrated spring element
11/23/2005EP1492701B1 Aircraft window case that can be artificially illuminated in an indirect manner
11/22/2005US6966525 In-flight refueling system, alignment system, and method for automatic alignment and engagement of an in-flight refueling boom
11/17/2005US20050253019 Method and apparatus for tempering gaseous and/or liquid media in transportation vehicles, particularly in aircraft
11/17/2005US20050253016 Structural mode shape alignment
11/17/2005DE10301445B4 Leichtbau-Strukturbauteil insbesondere für Flugzeuge und Verfahren zu seiner Herstellung Lightweight structural element, in particular for aircraft and process for its preparation
11/17/2005DE102005019280A1 Maschinenlesbare Kennungen nutzendes Flugzeug-Frachtladelogistiksystem Machine-readable identifiers-use aircraft cargo loading logistics system
11/17/2005DE102004018737B3 Coating for the inner lining sections of a passenger aircraft, comprises applying a transparent layer and a further layer structure to the section
11/17/2005DE102004013875A1 Vorrichtung zur Befestigung einer portablen elektronischen Einheit Device for fastening a portable electronic device
11/17/2005DE10012001B4 Strukturteil mit einer an seiner Innenseite angeordneten und abgedichteten Verriegelungseinrichtung Structural part arranged with one on its inside and sealed locking device
11/16/2005EP1596075A1 Three-dimensionally adjustable mounting device
11/16/2005CN1227437C Quick release and fastening cover
11/10/2005US20050251298 Automatic generation of telemetry flight software, accompanying specifications, and decode files
11/10/2005US20050248191 Composite protection for revealing damage to a core in a vehicle such as an aircraft
11/10/2005US20050247823 Injection-molded polycarbonate door
11/10/2005US20050247822 Load bearing window
11/10/2005US20050247818 Stiffened structures and associated methods
11/10/2005DE202005014077U1 Load-limiting securing arrangement for ceiling mounting of equipment in aircraft has mounting rails each having side attached to support structure, with side able to deform while keeping equipment attached to support structure
11/09/2005EP1351807B1 Forming structural assemblies with 3-d woven joint pre-forms
11/03/2005US20050246132 Aircraft cargo loading logistics system
11/03/2005US20050246074 System and method to enhance attitude estimation for transfer orbit maneuver
11/03/2005US20050246073 Multiple stayout zones for ground-based bright object exclusion
11/03/2005US20050246072 Method and apparatus for real-time star exclusion from a database
11/03/2005US20050246057 Aircraft cargo loading logistics system using machine readable identifiers
11/03/2005US20050242240 Aircraft with a detachable passenger escape cabin
11/03/2005US20050242237 Vtol aircraft external load drag reduction system
11/03/2005DE102004018579A1 Verkleidung für eine Struktur eines Flugzeugs Cladding for a structure of an aircraft
11/02/2005EP1591357A1 Aircraft fuselage panels interior fitting
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