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Match Document Document Title
US20100295303 Tethered system for power generation  
A system for power generation comprises a wing, a turbine, a tether, and a tether tension sensor. The wing is for generating lift. The turbine is coupled to the wing and is used for generating...
US20120211598 Variable Pitch Airfoils  
An apparatus may comprise an inflatable control surface for an aircraft and an end of the inflatable control surface configured for attachment to a fuselage of the aircraft. The end of the...
US20150108271 Differential Throttling Control Enhancement  
A system for enhancing movement of a multi-engine flight vehicle about either of pitch or yaw axes. The engines are oriented relative the centerline of the flight vehicle and a portion of the...
US20110029165 METHOD FOR DETERMINING THE SPEED AT WHICH AN AIRCRAFT BREAKS FREE OF THE GROUND EFFECT  
According to the invention, during take-off, the aircraft (AC) is given the tail strike attitude (θts) and the ailerons (6G, 6D) arc deflected fully downwards.
US20090306840 VISION-BASED AUTOMATED LANDING SYSTEM FOR UNMANNED AERIAL VEHICLES  
The invention relates generally to the control and landing of unmanned aerial vehicles. More specifically, the invention relates to systems, methods, devices, and computer readable media for...
US20070235584 Unmanned air vehicle interoperability agent  
A method of coordinating communications between a plurality of Unmanned Air Vehicles (UAVs) operating in connection with differing communication languages. A common language is provided which...
US20140343752 DEEP STALL AIRCRAFT LANDING  
An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an...
US20080142644 Flight apparatus having movable motors  
A flight control system for use in flight apparatus wherein the motors are capable of movement in more than one plane with respect to the support member in response to movement of the control...
US20130240667 Aircraft comprising fairings for correcting its dissymmetry or lateral asymmetry  
An aircraft having an asymmetry or a lateral geometric dissymmetry and comprising at least one pair of wings to each of which are fixed at least one fairing, each fairing comprising a surface...
US20080283660 Aircraft Braking System  
A method of braked pivot turning an aircraft, the aircraft comprising a fuselage and a landing gear assembly located to one side thereof. The landing gear comprises a bogie with wheels mounted...
US20110042508 CONTROLLED TAKE-OFF AND FLIGHT SYSTEM USING THRUST DIFFERENTIALS  
A manned/unmanned aerial vehicle adapted for vertical takeoff and landing using the same set of engines for takeoff and landing as well as for forward flight. An aerial vehicle which is adapted to...
US20120241556 APPARATUS FOR ADJUSTING A SURFACE OF AN AIRCRAFT MODEL, SURFACE UNIT, AIRCRAFT MODEL, AND USE OF AN AIRCRAFT MODEL  
An apparatus for adjusting a surface of an aircraft model includes, but is not limited to a first linear adjustment unit with a first retaining body that is movable along a first axis, a second...
US20120119017 Aircraft Wing Extension and Nozzle System  
A system and method to control flight of an aircraft. The aircraft having an engine with a rotatably nozzle assembly configured to create forward propulsion and yaw control of the aircraft. The...
US20140231578 STABILIZED UAV PLATFORM WITH FUSED IR AND VISIBLE IMAGERY  
Embodiments of the present invention relate to an unmanned aerial vehicle (UAV) and a method of use. The UAV may comprise a UAV platform designed around a sensor system. The UAV platform may...
US20080001028 Aircraft control system  
A span-loaded, highly flexible flying wing, having horizontal control surfaces mounted aft of the wing on extended beams to form local pitch-control devices. Each of five spanwise wing segments of...
US20130175390 MODULAR MINIATURE UNMANNED AIRCRAFT WITH VECTORED-THRUST CONTROL  
An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion...
US20090312891 Conversion system fault management system for tiltrotor aircraft  
The difference between a first position of a first pylon of a tiltrotor aircraft and a second position of a second pylon of the aircraft is prevented from becoming too large. An actuator position...
US20050242234 Lifters, methods of flight control and maneuver load alleviation  
The present invention provides a flight control system and method for various models of aircraft, including thin-winged, long range, transonic and low supersonic aircraft, and may be beneficial on...
US20070180394 Method of system for verifying entry of manually adjustable data in a multi-parameter aircraft instrument display  
A method and system for providing an easily recognizable visual feedback to a user in a multi-parameter aircraft instrument display, such as a flat panel display, of manually induced variations in...
US20060167598 Avionic system and ground station for aircraft out of route management and alarm communications  
An avionic system and ground station for aircraft out of route management and alarm communications composed of an avionic device, which is fitted onboard the aircraft, with a memory unit for...
US20090004004 Rotorcraft  
There is described a rotary wing aircraft comprising a fuselage (5), a main rotor (3) rotatable e in a main rotor plane relative to the fuselage for supporting the aircraft in flight, and a...
US20090140095 ELECTRIC POWERED ROTARY-WING AIRCRAFT  
A rotary-wing aircraft with an electric motor mounted along an axis of rotation to drive a rotor system about the axis of rotation.
US20090200431 AIRCRAFT WING TIP HAVING A VARIABLE INCIDENCE ANGLE  
An embodiment of an aircraft wing includes a main wing section and a variable incidence wing tip. The main wing section is adapted to connect to an aircraft fuselage at a first angle of incidence....
US20120056040 Electric VTOL Aircraft  
An electric and hybrid Vertical-Take Off and Landing (“VTOL”) aircraft is disclosed comprising a plurality of small Electric Ducted Fans (“EDFs”) of various sizes and orientations. The thrust of...
US20100170982 Aircraft without pilot (for commercial and military use)  
My innovated aircraft doesn't need pilots to fly in the designated airport; rather, it needs air worthy aircraft and airport's communication/navigation systems. By responding with the...
US20070252035 Unmanned vehicle  
A UAV or watercraft includes a navigation system that is configured to identify and make use of convective energy in a fluid medium through which it travels. The energy is used to provide movement...
US20070023570 System and method for remote control of interdiction aircraft  
An aircraft attack interdiction system using an unmanned interdiction aircraft piloted using a remote control system. In-flight refueling system, weapons launcher systems and intelligence...
US20100096490 Remote engine/electric helicopter industrial plat form  
The invention is an unmanned flying helicopter aircraft platform (“aircraft platform”) that can be powered by either interchangeable electric motors or by fuel powered internal combustion engines....
US20130231106 SYSTEMS AND APPLICATIONS OF LIGHTER-THAN-AIR (LTA) PLATFORMS  
Innovative new methods in connection with lighter-than-air (LTA) free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally...
US20090218442 TRAILING EDGE AIRCRAFT STRUCTURE WITH OVERHANGING COVER  
An aircraft structure comprising: a rear spar; and a composite cover attached to the rear spar and having an overhanging portion extending to its rear. The overhanging portion of the cover...
US20120175459 GUIDANCE CONTROL FOR SPINNING OR ROLLING VEHICLE  
A projectile, air vehicle or submersible craft with a spinning or rolling fuselage, rotating on its axis, has a collar which can be positioned relative to a longitudinal axis of the projectile...
US20100187369 DUCTED FAN UAV CONTROL ALTERNATIVES  
A ducted fan air-vehicle having alternative methods of control is described. The ducted fan air-vehicle includes an air duct, a fan, a center body, a plurality of control vanes. Each control vanes...
US20100252690 AIRCRAFT  
An unmanned aerial vehicle (UAV) in the form of a “tail sitter” flying wing adapted for vertical take off and landing and transitions between flight as a helicopter and wing-borne flight. The...
US20110210200 CONTROL SURFACE ASSEMBLIES WITH TORQUE TUBE BASE  
Control surface assemblies have a torque tube base. In one embodiment, a method includes moving an aerospace vehicle through a medium; and moving at least a portion of a control surface assembly...
US20090179109 System and method for adjusting control surfaces for wind tunnel models  
A system and a method for adjusting and locking a control surface that is movably arranged on a wind-tunnel aircraft model and comprises a drive arrangement for driving the control surface, and a...
US20100230546 CONTROL SYSTEM AND CONTROL METHOD FOR AIRBORNE FLIGHT  
A control system and method for control of a cyclical flying system which uses lift segments, which may be airfoils, which rotate around a central hub, similar to the mechanics of an autogyro. The...
US20140182695 Method of Using Microjet Actuators For The Control Of Flow Separation And Distortion  
A system for controlling unwanted flow separation. One or more microjets are placed to feed auxiliary fluid into a region of suspected flow separation on a surface. If the separation is...
US20120145834 Aircraft Attitude Control Configuration  
Control surfaces in an aircraft attitude control configuration provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes...
US20140312168 Control Surface for Creating Variable Camber Along a Wing  
An apparatus and method for controlling a shape of an outer surface of a control surface. In one illustrative embodiment, an apparatus comprises a control surface and a shaping system associated...
US20130292511 DIELECTRIC BARRIER DISCHARGE FLIGHT CONTROL SYSTEM THROUGH MODULATED BOUNDARY LAYER TRANSITION  
An aerodynamic control system incorporates multiple Dielectric Barrier Discharge (DBD) flow control actuators adjacent a surface of an airborne vehicle in a path of laminar boundary layer flow...
US20090127378 METHODS AND APPARATUS FOR DEPLOYING CONTROL SURFACES SEQUENTIALLY  
Methods and apparatus for deploying control surfaces generally comprise a fin deployment system for projectiles. The fin deployment system is used to control the timing of the control surface...
US20110174920 FLIGHT CONTROL SYSTEM ESPECIALLY SUITED FOR VTOL VEHICLES  
Flight control systems have plural control subsystems with redundancies organized so as to provide continued but degraded control power over critical aircraft flight operating parameters even if...
US20170037910 TORQUE TUBE ASSEMBLIES FOR USE WITH AIRCRAFT HIGH LIFT DEVICES  
Example torque tube assemblies for use with aircraft high lift devices are described herein. An example apparatus includes a spline coupling having a first yoke, a sliding splined shaft having a...
US20160311547 METHOD AND A DEVICE FOR STOPPING A TURBOSHAFT ENGINE IN NOMINAL OPERATION  
A method of stopping a turboshaft engine in flight. During a power reduction step, a current power of the engine for stopping is reduced to reach zero power, and a current speed of rotation of the...
US20160185466 SYSTEM AND METHOD FOR ENHANCING DISTRIBUTION LOGISTICS AND INCREASING SURVEILLANCE RANGES WITH UNMANNED AERIAL VEHICLES AND A DOCK NETWORK  
A system and method for enhancing distribution logistics and surveillance ranges with unmanned aerial vehicles (UAV) and at least one dock in a dock network. The UAV remains in communication with...
US20160185449 FLUID-VECTORING SYSTEM  
A jet aircraft includes an aircraft integrated, fluid vectoring, exhaust nozzle system. Implementation of this disclosure may eliminate or reduce the size of the aircraft vertical stabilizer and...
US20160179097 Unmanned Aerial Vehicle and a Method for Landing the Same  
Various embodiments provide a method for landing an unmanned aerial vehicle (UAV) in the presence of a wind. The method comprises: performing a first flare-maneuver whilst the UAV is flying. The...
US20160163206 Deep Stall Aircraft Landing  
An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an...
US20160137286 SHAPE-VARIABLE GAP COVERING BETWEEN CONTROL SURFACES AND ADJACENT STRUCTURAL COMPONENTS ON AIRCRAFTS  
A transition piece, which can be mounted in a recess, and which can form a continuous surface from a structural component of an airplane to a control surface, which is connected to the structural...
US20160059958 Controlling Rotary Wing Aircraft  
A rotary wing aircraft can include a central body and at least three rotors, each rotor connected to the central body by a swashplate. A system for controlling the flight of an aircraft with a...

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