Patents for B64C 5 - Stabilising surfaces (949) |
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12/29/2005 | WO2005044661A3 Supersonic aircraft with aerodynamic control |
12/29/2005 | DE10313290B4 Strömungsmechanisch wirksame Fläche eines sich in einem Fluid bewegenden Geräts, insbesondere eines Fluggeräts, insbesondere Tragfläche oder Ruderfläche eines Fluggeräts Fluidically effective area of a moving fluid in a device, in particular an aircraft, in particular wing or control surface of an aircraft |
12/27/2005 | US6978970 Aircraft with foldable tail assembly |
12/07/2005 | EP1602575A2 Supporting or guiding element |
12/01/2005 | WO2005044660A3 Wing gull integration for nacelle clearance, compact landing gear stowage, and sonic boom reduction |
12/01/2005 | US20050262682 Method and apparatus employing eccentric bushing |
12/01/2005 | DE102004019496A1 Wings for aircraft, has bearing areas that are divided into primary and secondary wings that are usually attached to respective sides of fuselage, where wings are connected to each other and manufactured in lengthwise manner |
11/22/2005 | US6966526 Dragless flight control system for flying objects |
11/03/2005 | WO2005103505A1 Method and apparatus employing eccentric bushing |
11/03/2005 | US20050242236 Aircraft with foldable tail assembly |
11/03/2005 | DE102004018579A1 Verkleidung für eine Struktur eines Flugzeugs Cladding for a structure of an aircraft |
10/27/2005 | WO2005100152A1 Fairing for an aircraft structure |
10/27/2005 | US20050236520 Flying amphibious SUV |
10/27/2005 | US20050236514 Dragless flight control system for flying objects |
10/27/2005 | CA2560978A1 Fairing for an aircraft structure |
10/26/2005 | EP1587734A1 Aircraft with forward opening inlay spoilers for yaw control |
10/25/2005 | US6957792 Lifting arrangement for aircraft fuselages |
10/20/2005 | US20050230546 Airflow control devices based on active materials |
10/13/2005 | WO2005075765A3 Locking device with solenoid release pin |
10/06/2005 | US20050218262 Process for improving the landing of an aircraft |
09/29/2005 | US20050211823 Helicopter |
09/27/2005 | US6948685 Locking device with solenoid release pin |
08/31/2005 | EP1568604A1 Helicopter |
08/27/2005 | CA2497252A1 Helicopter |
08/18/2005 | WO2005075765A2 Locking device with solenoid release pin |
08/18/2005 | US20050178899 Process for reducing the aerodynamic loads applied to the elevators of an aircraft during takeoff |
08/18/2005 | US20050178898 Method and apparatus for controlling an airplane |
08/18/2005 | US20050178883 Helicopter tail rotor pylon |
08/16/2005 | US6929216 Method and apparatus for installing and actuating movable airfoils, including canards |
08/16/2005 | US6928715 Method for producing lattice fin for missiles or other fluid-born bodies |
08/10/2005 | EP1562091A1 Method for improving the landing of an aircraft |
08/09/2005 | US6928400 Method for designing a deployment mechanism |
08/04/2005 | DE10361391A1 Connection connects a rudder unit having spars to the fuselage ribs of an airplane to form a power flow between the spars and the ribs |
08/02/2005 | US6923404 Apparatus and methods for variable sweep body conformal wing with application to projectiles, missiles, and unmanned air vehicles |
07/26/2005 | US6921052 Dragless flight control system for flying objects |
07/26/2005 | US6921045 Supersonic aircraft with channel relief control |
07/14/2005 | WO2005062743A2 Supersonic aircraft with aerodynamic tail structure |
07/14/2005 | WO2005023643A3 Aircraft with topside only spoilers |
07/14/2005 | US20050151018 Rudder unit connection |
06/22/2005 | EP1544101A1 Method for ameliorating the maneuverability of an aircraft during pitch up |
06/22/2005 | EP1544100A1 Method for reducing the aerodynamic forces on an elevator of an aircraft during takeoff |
06/09/2005 | US20050121946 Airflow control devices based on active materials |
06/09/2005 | US20050121240 Airflow control devices based on active materials |
06/09/2005 | US20050120538 Lattice fin for missiles or other fluid-born bodies and method for producing same |
06/02/2005 | US20050116116 Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance |
06/02/2005 | US20050116113 Dragless flight control system for flying objects |
06/02/2005 | US20050116087 Aircraft converts drag to lift |
06/02/2005 | US20050116085 Aircraft spiralling mechanism - c |
05/25/2005 | DE10346189B3 Car which converts to aeroplane has wings which swivel from longitudinal position along car to flying position at right angles to it, tail unit having side flaps forming cover for ends of wings in longitudinal position |
05/24/2005 | US6896221 Vertical takeoff and landing aircraft |
05/19/2005 | WO2005044660A2 Wing gull integration for nacelle clearance, compact landing gear stowage, and sonic boom reduction |
05/19/2005 | US20050103929 Supersonic aircraft with channel relief control |
05/19/2005 | US20050103926 Locking device with solenoid release pin |
05/17/2005 | US6892982 Aircraft with forward opening inlay spoilers for yaw control |
05/06/2005 | WO2005044661A2 Supersonic aircraft with aerodynamic control |
05/04/2005 | CN2696693Y Direction controller for traffic tool with propeller |
05/03/2005 | US6886778 Efficient wing tip devices and methods for incorporating such devices into existing wing designs |
03/31/2005 | US20050067525 Aircraft thickness/camber control device for low sonic boom |
03/24/2005 | WO2005025983A1 Fixed wing micro aerial vehicle |
03/17/2005 | WO2005023643A2 Aircraft with topside only spoilers |
03/17/2005 | US20050056731 Fiber matrix for a geometric morphing wing |
03/17/2005 | CA2528405A1 Aircraft with topside only spoilers |
03/03/2005 | US20050045764 Canard position and dihedral for boom reduction and pitch/directional control |
02/22/2005 | US6857599 Highly swept canard with low sweep wing supersonic aircraft configuration |
02/08/2005 | US6851646 Method and apparatus for actuating movable components, including canards, over multiple ranges |
02/03/2005 | DE19610870B4 Vorrichtung zur Strömungsführung A flashback guide |
01/25/2005 | US6845937 Survivable and reusable launch vehicle |
01/18/2005 | US6843450 Method and apparatus for rotatably supporting movable components, including canards |
01/18/2005 | US6843447 Vertical take-off and landing aircraft |
01/05/2005 | EP1493660A1 Efficient wing tip devices and methods for incorporating such devices into existing wing designs |
12/30/2004 | US20040262451 Efficient wing tip devices and methods for incorporating such devices into existing wing designs |
12/16/2004 | WO2004108526A1 Aircraft with forward opening inlay spoilers for yaw control |
12/16/2004 | CA2514825A1 Aircraft with forward opening inlay spoilers for yaw control |
12/14/2004 | US6830214 Rotary-wing aircraft |
12/09/2004 | US20040245379 Aircraft with topside only spoilers |
12/09/2004 | US20040245377 Helicopter |
12/09/2004 | US20040245374 Vertical take-off and landing aircraft |
12/07/2004 | US6827314 Aircraft with active control of the warping of its wings |
11/30/2004 | US6824092 Aircraft tail configuration for sonic boom reduction |
11/24/2004 | EP1479605A2 Helicopter |
11/18/2004 | DE202004014384U1 Wing and control surface arrangement for aircraft has each wing tip in form of folding flap, each with at least one control surface acting as rudder |
11/10/2004 | EP0993588A4 Gps guided munition |
11/03/2004 | EP1473223A1 Apparatus and methods for actuating rotatable members |
10/21/2004 | DE10313290A1 Wing structure for aircraft, has outer wing that swivels relative to inner wing when it hits certain counter force to reduce high fluid mechanical loads affecting aircraft wing |
10/13/2004 | EP1100718B1 An aircraft fin and rudder |
10/06/2004 | CN2646044Y Pneumatic layout structure of pilotless aircraft |
09/28/2004 | US6796532 Surface plasma discharge for controlling forebody vortex asymmetry |
09/22/2004 | CN2642674Y Hull type amphibious super-light airplane with two seats arranged longitudinally |
09/07/2004 | US6786450 Rapidly-convertible roadable aircraft |
09/02/2004 | US20040169485 Vehicle direction control with a crosswise fan |
08/19/2004 | US20040159227 Apparatus and method for restraining and releasing a control surface |
08/12/2004 | US20040155157 Winglet |
08/12/2004 | US20040155144 Aircraft spiralling mechanism - B |
08/05/2004 | WO2004065209A1 Flow-mechanically effective surface for minimising induced resistance |
08/05/2004 | DE10302514A1 Strömungsmechanisch wirksame Fläche eines sich in einem Fluid bewegenden Geräts, insbesondere eines Fluggeräts, insbesondere Tragfläche eines Fluggeräts Fluidically effective area of a moving fluid in a device, in particular an aircraft, in particular wing of an aircraft |
08/04/2004 | EP1442976A1 Airfoil member comprising an inflatable geometric morphing device with embedded fiber matrix |
07/29/2004 | US20040144893 Aircraft with forward opening inlay spoilers for yaw control |
07/22/2004 | US20040140395 Highly swept canard with low sweep wing supersonic aircraft configuration |
07/22/2004 | US20040140394 Method and apparatus for installing and actuating movable airfoils, including canards |
07/20/2004 | US6764044 Airplane spiralling mechanism |