Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
03/2001
03/01/2001DE19961734C1 Freight storage system for aircraft has pneumatically-operated roller drive units and/or locking units for handled freight container or pallets
02/2001
02/27/2001US6194074 Metal plates separated at joint by sealant
02/27/2001US6193032 Piezoceramic vibration control device and tuning control thereof
02/20/2001US6189833 Aircraft sliding door system
02/20/2001US6189832 Permanently connected remote latch mechanism
02/13/2001US6186717 Electrical terminal blind grounding stud fastener system
02/13/2001US6186444 Sliding pocket door for aircraft use capable of nondestructive blow-out and easy access
02/13/2001US6186211 Window assembly with a motorized window shade mechanism
02/07/2001EP1074653A2 High performance insulations and methods of manufacturing the same
02/07/2001EP1073822A1 Window shade assembly with a motorized window shade mechanism
02/07/2001EP1073582A1 Gallery retainer
02/06/2001US6182787 Rigid sandwich panel acoustic treatment
01/2001
01/24/2001CN1061102C Beryllium-containing alloys of aluminium and semi-solid processing of such alloys
01/23/2001US6177189 Appliqu{acute over (e)}s providing corrosion protection
01/18/2001WO2001004001A2 Monolithic structure with redundant load paths
01/18/2001WO2001003916A1 Fireproofing insulating material adapted for aeronautical insulation
01/18/2001DE19929471C1 Verfahren und Vorrichtung zur Herstellung eines dreidimensionalen Großbauteiles Method and apparatus for producing a three-dimensional large component
01/17/2001EP1068130A1 Adhesively bonded joints in carbon fibre composite structures
01/17/2001EP0773881A4 Yaw control and stabilization system for helicopters
01/10/2001EP1066195A1 Permanently connected remote latch mechanism
01/10/2001EP1066194A1 Propulsion system for an aircraft
01/09/2001US6170781 Door edge gap and radar signature mitigation door seal
01/09/2001US6170780 Twin engine aircraft
01/04/2001WO2001000488A1 Laminar flow control system and suction panel for use therewith
01/04/2001DE19955397C1 Holder on an aircraft stringer for tools and appliances has grooved recess for stringer and with spring-tensioned locking element movable perpendicular until locking face adjoins rounded side of stringer
01/04/2001CA2370647A1 Laminar flow control system and suction panel for use therewith
01/02/2001US6168114 Aircraft door assembly
01/02/2001US6168112 Double pane window for an aircraft cabin
12/2000
12/28/2000WO2000078547A1 Fire barrier panel
12/27/2000EP1063166A1 Method and apparatus for the manufacture of a three-dimensional large sized structure
12/26/2000US6164590 Variable body helicopter with tandem lifting rotors
12/21/2000WO2000076841A1 Improvements to aircraft landing gear compartment doors
12/14/2000WO2000075012A1 Improved fire-blocking insulation blanket and method for attaching same
12/12/2000US6158692 Main deck cargo door electric lock system
12/12/2000US6158690 Cabin interior panel system for reducing noise transmission in an aircraft
12/12/2000CA2123393C Structure having an aerodynamic surface for an aircraft
12/07/2000WO2000072990A1 Metallic shell component
12/07/2000CA2336074A1 Metallic shell component
12/05/2000US6155450 Composite shell shaped as a body of revolution
12/05/2000CA2073058C Treatment of metals for coating or activation
11/2000
11/30/2000DE19923441C1 Tür eines Luftfahrzeuges Door of an aircraft
11/28/2000US6151755 Front-mounted hinge
11/28/2000CA2019802C An acoustic liner
11/23/2000WO2000032388A3 Burn through resistant systems for transportation, especially aircraft
11/23/2000DE10007373C1 Sandwich component manufacture for aerospace products involves injecting resin mixture onto core covered with dry reinforcement, gelling and then finally closing tool
11/22/2000EP1053934A2 Aircraft door
11/22/2000EP1053803A2 Core for use in casting alloy structures
11/22/2000EP1053175A1 Double-walled panel
11/22/2000EP1053174A1 Dual function structures
11/16/2000WO2000068074A1 Grooved profile for diverting liquid
11/15/2000EP1052169A2 Aircraft fuselage floor structure
11/09/2000WO2000066426A1 Multiple glazed insulating unit, especially for an aircraft window, with electromagnetic armour
11/07/2000US6142419 Landing gear assembly for a model helicopter
11/07/2000CA2145099C Fuselage burn-through blocking material
11/02/2000WO2000065241A1 Electrical terminal blind grounding stud
11/02/2000EP1048562A2 Emergency exit system
11/02/2000DE19918736A1 Plattenbauteil, insbesondere für eine Fußbodenplatte in einem Flugzeug Plate member, in particular for a floor panel in an aircraft
10/2000
10/31/2000US6139232 YZ- latch for tying freight to a loading floor
10/31/2000US6138949 Main rotor pylon support structure
10/29/2000CA2307384A1 Emergency exit system
10/26/2000WO2000063070A1 Method of sealing a panel to an aircraft structure
10/25/2000EP1046576A2 Panel unit, particularly for an aircraft floor panel
10/24/2000US6135238 Extended reaction acoustic liner for jet engines and the like
10/19/2000WO2000061957A1 Structural blind bolt
10/19/2000CA2366103A1 Structural blind bolt
10/18/2000CN1270551A Method for making parts in composite material with thermoplastic matrix
10/12/2000WO2000059754A1 Method of shortening down times during the loading and unloading of a transport vehicle, and transport system
10/10/2000US6129312 Aircraft decompression vent assembly
10/05/2000DE19914939A1 Loading and unloading time shortening method for different vehicles uses exchangeable cabins sent ahead separately so that they are ready for changing when vehicle arrives
10/03/2000US6126114 Door for aircraft, particularly for helicopter, with interconnected movements of upper and lower leaves
10/03/2000US6126113 Helicopter removable drive train platform
10/03/2000US6125984 Ball mat
09/2000
09/28/2000WO2000056602A1 Modular air intake duct for aircraft
09/28/2000WO2000056541A1 Composite material with a reinforced connecting area
09/27/2000CN2398200Y Airplane with double-deck connect seat passage type safety steam pocket
09/26/2000US6123295 Fuel tank for lifting body re-entry vehicle
09/26/2000US6123171 Acoustic panels having plural damping layers
09/19/2000US6120070 Lockable panel latch
09/13/2000EP1034579A1 Method for producing a radar reflection diminishing structural component
09/12/2000US6116542 Door system for a passenger aircraft
09/12/2000US6116389 Apparatus and method for confinement and damping of vibration energy
09/05/2000US6114050 Hybrid laminate includes a central reinforcing core layer having bonded to each of its sides a layup that includes layers of titanium alloy foil with layers of a composite of fiber-filled organic resin between the foil layers
08/2000
08/31/2000WO2000050723A1 Window shade assembly with a motorized window shade mechanism
08/30/2000EP1031617A1 Component for interior decoration of aircraft, and method of manufacturing the same
08/30/2000EP1030807A1 Pressure frame designed in particular for an aircraft
08/30/2000CN2393821Y Frame of helicotoper cabin
08/29/2000US6110327 Primer for promoting adhesion of electroconductive metal oxide to plastic substrates
08/29/2000US6109563 Plug door operating mechanism
08/22/2000US6105902 Aircraft fuselage and method of forming same
08/17/2000WO2000048206A1 Materials and composites activable into a state of enhanced conductivity
08/17/2000WO2000047397A1 Fibre reinforced composites and method of making same
08/17/2000CA2362254A1 Materials and composites activable into a state of enhanced conductivity
08/16/2000EP0935556B1 Emergency egress system for aircraft
08/08/2000US6098927 Multi-purpose aircraft
08/08/2000US6098922 Lifting-fuselage/wing aircraft having low induced drag
08/08/2000US6098267 Method for forming surface structures from a single-sided mold
08/03/2000WO2000045001A1 Continuous wave composite viscoelastic elements and structures
08/01/2000US6097553 Window structure with non-radial mounting support having graded thermal expansion
07/2000
07/27/2000DE19922295C1 Underfloor structure of fuselage cell for helicopter is connected with floor and outer fuselage shell, comprising interconnected longitudinal and crossbearers
07/27/2000DE19901286A1 Structural component, especially for aircraft construction, has one-piece inner body with recesses and/or openings to form installation spaces, and cover element connected to inner body and closing off recess or opening