Patents
Patents for B64C 9 - Adjustable control surfaces or members, e.g. rudders (2,586)
12/2004
12/16/2004US20040251382 Aircraft high-lift system with overload protection
12/16/2004DE10326799B3 Vorrichtung zur Betätigung von Klappenelementen an den Tragflächen eines Flugzeuges A device for actuating flap elements on the wings of an aircraft
12/16/2004CA2514825A1 Aircraft with forward opening inlay spoilers for yaw control
12/15/2004EP1486416A1 Aircraft flap actuation device
12/14/2004US6830214 Rotary-wing aircraft
12/09/2004WO2004092520A3 Arrangement and associated system having an actuator and a tubular flap-drive member about the actuator
12/09/2004US20040245387 Method and system for controlling an aircraft control surface
12/09/2004US20040245386 Systems, apparatuses, and methods for moving aircraft control surfaces
12/09/2004US20040245379 Aircraft with topside only spoilers
12/07/2004US6827310 Apparatus and method for fin actuation in a portable missile
12/02/2004DE10328717B3 Operating device for control flap on rear edge of aircraft wing has pyramid transmission device connected on one side to wing structure and on other to flap
11/2004
11/18/2004DE10317258A1 Verstellmechanismus für einen formvariablen Flügel Adjustment mechanism for a shape-variable wing
11/10/2004EP1475305A2 Geared rotary actuators
11/04/2004US20040220014 Geared rotary actuators
11/03/2004EP1473223A1 Apparatus and methods for actuating rotatable members
11/03/2004EP1404573B1 Lift-flap mechanism
10/2004
10/28/2004WO2004092520A2 Arrangement and associated system having an actuator and a tubular flap-drive member about the actuator
10/28/2004WO2004092013A2 Winged spacecraft
10/20/2004EP1468909A1 Rotor blade and lift device with such a rotor blade
10/20/2004EP1467910A1 Joint for connecting a longitudinal side to an upper side of components and flexible strip for use in such a joint
10/20/2004EP1467909A1 Joint for connecting components together on opposite longitudinal sides in addition to a flexible strip used for said joint
10/20/2004EP1342556B1 Process for producing a fiber reinforced composite component
10/13/2004EP1100718B1 An aircraft fin and rudder
09/2004
09/22/2004EP1301835B1 Flight control module with integrated spoiler actuator control electronics
09/14/2004US6789769 Flexible airflow separator to reduce aerodynamic noise generated by a leading edge slat of an aircraft wing
09/02/2004US20040169110 Aerodynamic component for controlling a landing guide path of an aircraft
09/01/2004EP1452442A1 Aircraft lift augmentation system with overload protection
08/2004
08/12/2004WO2003039949A3 Wing with lift enhancement by internal air flow
08/12/2004US20040155146 Method of controlling a landing guide path of an aircraft
08/12/2004US20040155144 Aircraft spiralling mechanism - B
08/05/2004WO2004065209A1 Flow-mechanically effective surface for minimising induced resistance
08/05/2004DE10302514A1 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
08/04/2004EP1343687B1 An aircraft flap extension mechanism
07/2004
07/29/2004US20040145080 Method for fabricating wing
07/29/2004US20040144893 Aircraft with forward opening inlay spoilers for yaw control
07/28/2004EP1440880A1 Method and system for actuating aircraft control surfaces
07/27/2004US6766981 Control system for alleviating a gust load on an aircraft wing
07/22/2004US20040140394 Method and apparatus for installing and actuating movable airfoils, including canards
07/21/2004EP1438230A1 Carrying or guiding device for aircraft components
07/20/2004US6764047 Model airplane hinge construction
07/20/2004US6764044 Airplane spiralling mechanism
07/15/2004DE10308301B3 Aircraft landing flaps operating drive with overload protection provided by electrical load sensor at point of transmission of central drive energy to each individual flap body operating drive
06/2004
06/30/2004EP1226070B1 A hinge for movable control surfaces in an aircraft and a connecting piece to be used with such a hinge
06/24/2004US20040118969 Hydrogen powered aircraft
06/09/2004DE10257874B3 Paraglider or kite aerodynamic profile has slot at rear providing flow path between underside and upperside of profile
06/02/2004EP1198383B1 Actuator system for aerospace controls and functions
05/2004
05/27/2004US20040099765 Method and apparatus for actuating movable components, including canards, over multiple ranges
05/25/2004US6739550 Flight control surface control unit
05/21/2004WO2004007282A3 A rotary-wing aircraft having horizontal stabilizer
05/18/2004US6735842 Movable structural component for a thermomechanically stressed assembly as well as a process for producing the structural component
05/13/2004US20040089765 L-tail (featuring parabrakes)
05/13/2004DE10133920B4 Auftriebsklappen-Mechanismus Lift flap mechanism
05/12/2004EP1417124A1 System and method for controlling an aircraft
05/11/2004US6732974 Tiperon
05/04/2004US6729583 Device for articulating a flap to an aircraft aerodynamic surface
04/2004
04/29/2004US20040079839 Method and apparatus for rotatably supporting movable components, including canards
04/29/2004US20040079835 Control system for alleviating a gust load on an aircraft wing
04/28/2004EP1413782A1 Method and apparatus for rotatably supporting movable components, including canards
04/28/2004EP1413516A1 Method and apparatus for actuating movable components, including canards, over multiple ranges
04/22/2004DE19925560B4 Zusatzflügel für Hauptflügel von Flugzeugen Additional wings for the main wing aircraft
04/21/2004CA2444869A1 Method and apparatus for actuating movable components, including canards, over multiple ranges
04/20/2004US6722616 Method of lift control of aircraft and system therefor
04/15/2004WO2004031682A1 Braking device for a trajectory-correctable spin-stabilized artillery projectile
04/14/2004EP1407964A2 Slotted cruise trailing edge flap
04/08/2004WO2004008097A3 Apparatus for monitoring an aircraft flap and application of a dynamometric rod
04/08/2004US20040065783 Aircraft flap extension mechanism
04/07/2004EP1404573A1 Lift-flap mechanism
03/2004
03/23/2004US6708923 Aircraft spiralling mechanism
03/16/2004US6705570 Arrangement and associated system having an actuator and a tubular flap-drive member about the actuator
03/02/2004US6698688 Apparatus and methods for actuating rotatable members
02/2004
02/12/2004DE19819308B4 Flügelhinterkantenfeder Trailing edges spring
02/04/2004EP0951421B1 Method for controlling an aeroplane control surfaces to counter ground lateral drift
01/2004
01/29/2004DE10210517B3 Verfahren zur Herstellung eines Bauteiles in Faserverbundbauweise A method for producing a component of composite fiber material construction
01/28/2004CN2601211Y Aeroplane adopting double delta-wing two-side intaking side plate duck type pneumatic distribution
01/28/2004CN2601210Y Aeroplane adopting trapezoidal wing two-side intaking dust type pneumatic distrubution
01/28/2004CN2601209Y Aeroplane adopting belly intaking side plate type pneumatic distribution
01/27/2004US6682023 Contiguous variable camber device
01/22/2004WO2004008097A2 Apparatus for monitoring an aircraft flap and application of a dynamometric rod
01/22/2004WO2004007282A2 A rotary-wing aircraft having horizontal stabilizer
01/22/2004CA2493087A1 Rotary-wing aircraft
01/15/2004WO2004005132A1 Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
01/15/2004US20040007645 Rotary-wing aircraft
01/08/2004US20040004162 Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
12/2003
12/18/2003US20030230677 Device for articulating a flap to an aircraft aerodynamic surface
12/17/2003EP1371552A1 Articulation device for connecting a flap to an aircraft aerodynamic surface
12/11/2003US20030226936 Flexible airflow separator to reduce aerodynamic noise generated by a leading edge slat of an aircraft wing
12/04/2003DE10202439C1 Gelenk zur Verbindung von Bauteilen mit einander zugewandten Längsseiten sowie flexibles Band zur Verwendung für ein derartiges Gelenk Joint for connecting components with mutually facing longitudinal sides, as well as flexible tape for use for such a joint
11/2003
11/27/2003US20030218102 Microfabricated translational stages for control of aerodynamic loading
11/26/2003EP1212238B1 Improvements to convertible aircraft with tilting rotors
11/18/2003US6648433 Spiralling missile—B
11/11/2003US6644587 Spiralling missile—A
11/04/2003US6641089 Flap arrangement for varying the aerodynamic lift generated by an aerodynamic element of an aircraft
11/04/2003US6641086 System and method for controlling an aircraft
10/2003
10/29/2003EP1355930A2 A method for identification, isolation and production of antigens to a specific pathogen
10/23/2003US20030197097 Reconfiguration control system for an aircraft wing
10/02/2003DE10202440C1 Gelenk zur Verbindung einer Längsseite mit einer Oberseite von Bauteilen sowie flexibles Band zur Verwendung für ein derartiges Gelenk Joint for connecting a longitudinal side with an upper surface of component parts, flexible tape for use for such a joint
09/2003
09/30/2003US6626401 Aft fuselage control system for forward lifting elevator aircraft
09/25/2003US20030178738 Method for producing a fiber composite structural component
09/18/2003US20030173459 Lattice fin for missiles or other fluid-born bodies and method for producing same
09/17/2003EP1343687A1 An aircraft flap extension mechanism
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