| Document |
Document Title |
|
WO/2005/039956 |
A vehicle includes a chassis and a plurality of wheel assemblies articulated with the chassis, each of the plurality of wheel assemblies comprising a rotatable wheel spaced away from the chassis, and further comprising an articulated sus...
|
|
WO/2005/035362 |
For a transport of a cargo within the earth atmosphere and into the space and back there is designed a cargo transport means provided with transfer means for movement up to the height of about 80 km above the earth surface and transporta...
|
|
WO/2005/032939 |
The invention relates to a flying object, referred to as the Autherith flying object (AFO), said AFO being characterised by the cited novel system of construction. The AFO can take off and land vertically above the ground and water (fig....
|
|
WO/2005/030578 |
An aircraft arrangement for Mini or Micro UAV comprising a fore wing (14) and an aft wing (12) in tandem closed-coupled arrangement. The aft wing (12) has side panels (18) and control surfaces (19), and tapered planform with positive swe...
|
|
WO/2005/025983 |
Fixed wing micro aerial vehicle characterized in that it comprises an allowing platform (1) composed by two low aspect ratio semi-wings (2) with substantially trapezoidal planform, equipped with elevons (4) along their trailing edge and ...
|
|
WO/2005/025986 |
The invention provides a control station (5) for use an surveillance aircraft. Controls for each surveillance accessory (lights, cameras etc) are lead to a station having a single VDU (8) and a single hand control (10). The VDU (10) and ...
|
|
WO/2005/023642 |
A portable unmanned air vehicle and launcher system is provided that includes a foldable unmanned air vehicle having a pressure tube; a launch gas reservoir for holding launch gas; a launch tube operatively connected to the launch gas re...
|
|
WO/2005/023644 |
An impeller (16) driven ring wing (12) aircraft (10) whose lifting forces are augmented by the release of jets of air (113) from Coanda slots (42) disposed around the exterior edge (32) of t-he ring wing (12). These jets of air (113) ent...
|
|
WO/2005/023645 |
A wing (1) including a lift augmentation device, comprising a main wing body (3) and a displaceable auxiliary body (5) defining a lift augmenting configuration and a non-augmenting configuration and moveable to intermediate configuration...
|
|
WO/2005/023643 |
An aircraft (10) with swept back wings (16, 18) and spoilers (30,32) inlaid into the top surface (36) near the tips of the wings. The aircraft also includes an elevator (34) formed in the center back portion of the aircraft, which is als...
|
|
WO/2005/019029 |
A rotary aircraft (rotorcraft) in which the entire aircraft rotates about its center of mass as it flies, and in which the center of mass is located external to the aircraft in the generally triangular region formed by the aircraft's sin...
|
|
WO/2005/019028 |
A small unmanned aircraft, comprising a flying wing type main wing (1) formed in a camber wing type having a generally flat lower surface and convergent in tapered shape toward wing tips, having wing leading edges with sweep-back angles,...
|
|
WO/2005/016753 |
Methods and apparatuses for cable launching airborne devices (e.g., unmanned aircraft) are disclosed. In one embodiment, an apparatus includes an elongated structure, e.g., a tower, boom or derrick. At least one flexible elongated member...
|
|
WO/2005/016746 |
The disc flying object is a new form of aircraft for flying through atmosphere or space. The armour (1) and the body (2) have a form of the disc, i.e. the form of ellipse observed from directions of x and y-axis and the form of circle ob...
|
|
WO/2005/014390 |
Methods and apparatuses for assembling, launching, recovering, disassembling, capturing, and storing unmanned aircraft (140) and other flight devices or projectiles are described. In one embodiment, the aircraft (140) can be assembled fr...
|
|
WO/2005/007508 |
An aircraft which comprises means providing air circulation and directing said circulation along a housing. Different operational stages of the aircraft such as take off and level flight are achieved by using the same functionally interc...
|
|
WO/2005/002965 |
A mobile object being a vehicle of any type includes a plurality of force generators and a plurality of engines. Each force generator (42) is a propulsion mechanism that converts directly a rotational energy of an engine (44) into a self...
|
|
WO/2005/000671 |
A novel design and construction method for an inflatable, rigidizable wing for a terrestrial or planetary flying vehicle. The wing is caused to deploy from an initially packed condition and to assume its functional shape by means of an i...
|
|
WO/2004/113165 |
The inventive small-dimension helicopter comprises a body, rotor blade system, power engine, and a transmission. Said rotor blade system is embodied in the form of a space frame whose axis coincides with the axis of the engine shaft and ...
|
|
WO/2004/113166 |
The invention relates to a gyropter having coaxial contrarotating rotating aerofoils, in particular, one having two crown rotors (2,1) that rotate in opposite directions about a pod (6) either provided in the form of a drone or of a mann...
|
|
WO/2004/112929 |
A apparatus for assisting in flying, walking or swimming having wings, legs or fins attached to a drive mechanism in which the end of the wings, legs or fins are simultaneously oscillated and moved linearly generating lift or walk and sw...
|
|
WO/2004/113163 |
The purpose of this invention is to provide an ultra-miniature aircraft which is able to perform 'Vertical Take-off and Landing (VTOL)' and maintaining altitude when the vehicle is moving or when the horizontal velocity of a vehicle is a...
|
|
WO/2004/108527 |
A resonant wingbeat tuning circuit automatically tunes the frequency of an actuating input to the resonant frequency of a flexible wing structure. Through the use of feedback control, the circuit produces the maximum flapping amplitude o...
|
|
WO/2004/108524 |
In one embodiment, a method for controlling an aircraft (10) comprises providing an attitude error (214) as a first input into a neural controller (202) and an attitude rate (216) as a second input into the neural controller (202). The a...
|
|
WO/2004/108526 |
An aircraft (50) comprises first (68) and second (70) wings positioned on opposite sides of a longitudinal axis, a first forward opening control surface (52) attached to an upper surface of the first wing (68), and a second forward openi...
|
|
WO/2004/106156 |
A heavier-than-air air vehicle (1), particularly a long endurance, solar powered, unmanned aerial vehicle (UAV) intended for 'perpetual' flight within the stratosphere, is carried to its operational altitude suspended on a tether (14) fr...
|
|
WO/2004/103889 |
A drive assembly for a wing of a micromechanical flying insect. The drive assembly comprises a honey comb structure. A method for flying a micromechanical flying insect comprising moving a wing with a drive assembly having a stiffness to...
|
|
WO/2004/100289 |
A neutral buoyant airship, such as a blimp, contains a lifting body which allows the airship to remain neutrally buoyant in air and fuel cell located in the airship. A method of generating power in the neutrally buoyant airship, comprisi...
|
|
WO/2004/098992 |
The invention relates to an aircraft comprising: a lift-generating fuselage (1), the largest span (11) of said fuselage being in the third fifth (15) or the four fifth (17) of the total length thereof, and the outline of the fuselage pro...
|
|
WO/2004/094227 |
The present invention relates to an apparatus for reducing drag of an aircraft utilized in combination with an aircraft surface (12), where the local airflow has an upward momentum due to the free air stream being deflected upward by the...
|
|
WO/2004/092013 |
A rocket-powered spacecraft with a wing (17) havint hinged portions (21, 22) which can be elevated about a hinge line (23). Tail booms (24, 25) extend rearwardly from the outer ends of the aft wing portions, and rudders (29) are mounted ...
|
|
WO/2004/082854 |
The invention relates to transportation, in particular to transport objects using a magnet and air cushion. The inventive locomotion method for a transport object (TO) consists in levitating above an elevated road (AR) and in moving ther...
|
|
WO/2004/078588 |
The invention relates to an advantageous design of aircraft, such as passenger or cargo transport aircraft. The invention also relates to a system for loading and unloading aircraft of this type at airports. The invention additionally re...
|
|
WO/2004/074063 |
The invention relates to aircraft engineering, in particular to aircraft using the screen effect. The sense of said invention lies in the following: the inventive air cushion amphibian airfoil boat is characterised in that it consists of...
|
|
WO/2004/074680 |
A power generator assembly incorporates a series of four blades (1) of vane-like form. Each blade (1) is mounted on a shaft (2) in a support structure incorporating an integral cog wheel (3). Each of the four cog wheels (3) are linked by...
|
|
WO/2004/074093 |
Swept-wing box-type aircraft comprising a fuselage (1) and a lifting system formed by two substantially horizontal wings (2, 3), one of which has a positive sweep angle, while the other one has a negative sweep angle, lying on planes spa...
|
|
WO/2004/065208 |
A VTOL aircraft with magnetic linear induction powered impeller rotors (21b). The craft may have many configurations of multiple or single rotors. Directional control is included through the use of vanes or thrust tilting of the rotors.
|
|
WO/2004/063008 |
A modular automated air transport system comprising an unmanned autonomous aircraft having a selectively detachable control systems portion and a structural air frame portion, wherein the structural air frame portion contains an interior...
|
|
WO/2004/060743 |
A micro air vehicle (10) having a bendable wing (12) enabling the micro air vehicle to fly. The bendable wing (12) may be bent downwards so that the wingspan may be reduced for storing the micro air vehicle. The bendable wing (12) may be...
|
|
WO/2004/054875 |
The invention relates to an aircraft comprising a fuselage (1) and at least two essentially hollow cylindrical lifting bodies (2, 3, 4, 5) which are applied to the fuselage (1) and comprise a plurality of rotor blades (8) which extend ov...
|
|
WO/2004/043783 |
An electric-energy lifting panel levitates a user secured to the electric-energy lifting panel. The electric-energy lifting panel (104) includes a first capacitive plate (106) and a second capacitive plate (108) having different geometri...
|
|
WO/2004/043781 |
A jet-powered tri-mode aircraft (100) comprising a fuselage (102), a rotor blade (104) with gas flow exit nozzles, a turbofan engine producing an exhaust gas flow, a cruise nozzle for regulating and outputting gas flow, canard wings (124...
|
|
WO/2004/042495 |
A modular combat command and control system is disclosed having a concrete layer and a plurality of abstracted layers. Various components can be interchangeably associated with the abstracted layers to form different applications, such a...
|
|
WO/2004/042495 |
A modular combat command and control system is disclosed having a concrete layer and a plurality of abstracted layers. Various components can be interchangeably associated with the abstracted layers to form different applications, such a...
|
|
WO/2004/030783 |
Disclosed is a flying device comprising at least one flying unit (10) that can accommodate one or fewer persons, is able to take off in a vertical direction, and is used for flying freely within at least one hall (100), the limitations (...
|
|
WO/2004/018158 |
A system of self-organizing mobile robotic agents (MRAs) (6) in a multi robotic system (MRS) (2). MRAs cooperate, learn and interact with the environment. The system uses various AI technologies including genetic algorithms, genetic prog...
|
|
WO/2004/016504 |
A single pilot aircraft that can be carried and bound to a pilot, comprises a turbojet engine, two propulsion air-outlet nozzles which are arranged on either side of the turbojet engine and which can be adjusted to change the direction o...
|
|
WO/2004/003680 |
A system is described for remote sensing surveillance by configuring groups of automated mobile robotic vehicles (MRVs). The collection of MRVs have sensors that feed information to a central network node. As the MRVs interact with the e...
|
|
WO/2004/002822 |
The inventive method for producing a lifting force consists in forming a binary cyclone with the aid of thermal currents of at least one gas-jet device which are directed over the top surface of an object situated in the atmosphere of th...
|
|
WO/2004/002821 |
A ducted air power plant, comprising a motor driven fan (7) situated in a duct (4), the fan (7) having an air intake side and in operation providing a high pressure air stream in the duct, and the fan being located adjacent air splitter ...
|
