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Matches 401 - 450 out of 1,582

Document Document Title
WO/2010/007466A1
According to some embodiments, an airborne body extends horizontally along an axis between a first point and a second point. The body may be, for example, at least partially filled with a gas. Two or more vanes may be provided airborne w...  
WO/2010/006433A1
A wind powered generator is described that may take advantage of the strong wind present at higher altitudes above terrain than can feasibly be reached by traditional tower mounted wind generators. It makes use of a combination of lift s...  
WO/2010/003468A2
The invention relates to a segmented aircraft comprising gas cells which are filled with an energy medium, especially an aircraft which contains a gaseous energy medium that is approximately the same weight as air in interlinked gas cell...  
WO/2009/152604A1
A hybrid lift air vehicle for carrying and transporting a load, comprising an envelope having a generally ellipsoidal shape adapted to receive a volume of lighter-than-air gas, at least two variable thrust vertical thrusters in secure en...  
WO/2009/149727A1
The invention relates to a metering device for fine grained powder (1), in particular for medicinal powder (1) for pulmonary administration, and to a method for operating the metering device. The metering device comprises a powder pump a...  
WO/2009/145808A2
A planer hexagon curve extruded to a center point providing six isosceles triangle panels with the shortest edge being one of the six planer hexagon curves forms a buckyball hexagon extrusion that naturally provide pentagon extrusions. A...  
WO/2009/146084A2
A sliding-arm whirling wheel thruster includes first and second whirling wheels and a housing. The first whirling wheel is disposed about a first rotational axis, and the second whirling wheel about a second rotational axis parallel to t...  
WO/2009/137931A1
A method and system for geophysical surveying. An airship having a self-supporting gas envelope and propulsion units is provided with geophysical survey equipment, and geophysical data is collected while flying the airship. Also a method...  
WO/2009/112447A1
Elongated, cumbersome goods are transported using articulated trucks and unloaded using a crane. A method and an apparatus for transporting and use as crane for elongated, cumbersome loads over wide distances even under unfavorable infra...  
WO/2009/075600A1
The invention relates to airplanes lighter than air. The inventive airship comprises a gastight envelope and a longitudinal gastight deformable partition which is arranged inside the envelope and forms a main upper chamber filled with a ...  
WO/2009/076681A2
A planer hexagon curve extruded to a center point providing six isosceles triangle panels with the shortest edge being one of the six planer hexagon curves forms a buckyball hexagon extrusion that naturally provide pentagon extrusions. A...  
WO/2009/070402A1
An aerial load lifting system features a non-rigid or blimp-type dirigible providing a lighter-than-air envelope (10) that is placed within a structural shell (50). The system is designed so that the envelope provides essentially neutral...  
WO/2009/046554A1
A plurality of turbines (20) is disposed around a gear wheel (21). The mechanical power of the turbines generates the propulsion, and the thermal power generates the lift of the airship. On each of the output shafts of the turbines (20) ...  
WO/2009/033853A1
Elongated, bulky products are transported by means of a cable-guided lift body (1) connected to the load (15) by way of at least one mobile, controllable winch (13) via a hauling cable (18) and via a supporting cable (4; 7) and a rotatab...  
WO/2009/029367A2
An orientation system is disclosed for a lighter-than-air aircraft having a lower stage suspended from an envelope. The orientation system includes a swivel and a plurality of thrust generators. The swivel is affixed between the envelope...  
WO/2009/022889A1
The present invention concerns a new airship wherein are installed infrared cameras and radars for monitoring urban zones and conduits for gas or petroleum derivatives, for detection of leaks, and also for checking of the same; also for ...  
WO/2009/023114A2
A system for controlling yaw (7) associated with an airship may include one or more vertical control surfaces (25) associated with the airship, a first power source (541) and a second power source (542), each configured to provide a thru...  
WO/2008/134787A1
The invention relates to a method and device for extracting water from the moisture in the air surrounding the surface of the Earth by condensation from said air, wherein the cooling energy required therefor is taken from the colder laye...  
WO/2008/131916A2
The invention relates to a flexible multi-layer material that can be used in particular for an inflatable balloon casing, a blimp, an airbag, a sail, a flexible solar cell, or a flexible antenna. At least one layer (11, 13) is provided, ...  
WO/2008/133968A1
Apparatus and method for a continuous replenishing of the lift gas and maintaining the proper pressure and lift of a tethered medium altitude aerostat utilizing a novel feed tube running the entire length of the tether. A first end of th...  
WO/2008/118140A2
A method for performing east-west station keeping for a satellite in an inclined synchronous (16) orbit is described. The method includes averaging a value of a right ascension of the ascending node (34) for an inclination vector (140) a...  
WO/2008/110385A2
The invention relates to an airship comprising a balloon and several drives for displacing the airship. Said invention can be used by dirigibles that are also known as autonomous airships or blimps, as well as for Zeppelins. The aim of t...  
WO/2008/108655A1
An aircraft which is configured for vertically ascending and landing, comprises at least two wings (2a, 2b, 4a, 51, 4b, 52), a space (2c, 4c) for the generating during operation of climbing power, and an intermediate portion (3), the int...  
WO/2008/101390A1
A method and a special equipment converting wind energy at high altitude into kinetic energy on the ground are disclosed. Airoperated equipments flying to the high altitude obtain the wind energy at high altitude. While wind power at hig...  
WO2008059144B1
Secure device for transporting and storing gaseous hydrogen. The invention relates to a lighter-than-air balloon (aerostat) (1) filled with hydrogen and pulled with a cable (2) by a landborne vehicle (3), a boat (4), or another aerostat ...  
WO/2008/097136A1
The invention relates to lighter-than-air vehicles. The inventive aircraft comprises a rigid body with carrier gas-containing shells and propulsers arranged inside aerodynamic modules which are embodied in the form of aerodynamically sha...  
WO/2008/060717A2
A device for deploying an aerostat includes a cylindrical shaped container having an open end and a closed end and a center tube axially oriented in the container. A tapered disc is mounted for axial movement on the center tube, and it h...  
WO/2008/051175A2
A lighter than air semi-rigid air vehicle utilizing two or more spherical chambers with composite fairings in between to reduce drag. The vehicle also may utilize a reverse ballonet or conventional ballonet system for the lift gas contro...  
WO/2008/051638A2
One embodiment of the invention provides an airship having an outer tube formed in the shape of a toroid and defining a central opening, a first compartment positioned within the outer tube and containing a first gas, and a second compar...  
WO/2008/050322A2
The airborne guided shell (1) has an adapting kit (3) attached to a shell, where there is an elongated housing (4) that encapsulates the adapting kit (3). The adapting kit (3) includes driving flaps (5), the position of which can be chan...  
WO/2008/045582A2
By sharing tasks between the carrier vehicle (12) and the kill vehicles (14), the multiple kill vehicle interceptor (10) provides a missile defence system capable of intercepting and killing multiple targets. The control sensor (38) is p...  
WO/2008/025139A1
A hybrid lift air vehicle for lifting and transporting a payload to a delivery location, which comprises a helium or other lighter-than-air gas filled envelope mounted on an airframe. Variable and reversible vertical thrusters are positi...  
WO/2008/019812A1
The invention relates to an aerostat (1) which can be tethered by cables but can move in the direction in which the cables extend, with the aerostat (1) having a drive and, via its drive (14), a friction connection to at least one of the...  
WO/2007/138727A1
An airship-type aerial crane capable of inexpensively and safely transporting a cargo by simple operation in a wide range of field including collection of timbers in a mountainous area. The airship-type aerial crane has a body (1) filled...  
WO/2007/085807A1
A Wind energy conversion apparatus comprising a wind turbine supported by, or integral with, a lighter-than-air structure, the part of the turbine that rotates being rotated by the wind whilst at the same time absorbing substantially all...  
WO/2007/079788A1
The invention relates to an unmanned aircraft for telecommunicative or other scientific purposes, which s stationed in determined height, in particular in the stratosphere. The aircraft comprises a gas-filled balloon (11) carrying a plat...  
WO/2007/073361A1
The invention relates to the aircraft engine unit arrangement. The inventive tug aircraft comprises an engine unit provided with an aerodynamic propelling device for producing the tractive force of a transport device, the engine unite su...  
WO/2007/065649A2
The invention relates to an aerial transporter comprising rigid cell structures which are covered with light materials as a skin, composed of modules. The inventive aerial transporter represents some type of airship without a tail unit a...  
WO/2007/062440A1
The invention relates to an airship which can be unfolded and folded up automatically on the ground and during flight and which can be operated as an aircraft or as a reusable space shuttle, having a combined collapsible gas cell (400), ...  
WO/2007/045091A1
This invention relates to the field of buoyant aircraft and operation thereof, in particular, airships for lifting heavy and/or oversized loads. According to the present invention it would be advantageous to provide a airship that can li...  
WO/2007/041814A1
Flight control of an airship (2) is achieved by mounting on both ends of a traditionally shaped airship two engines with propellers (3, 12) with adjustable angle of attack, from positive to negative values. Behind each propeller a vertic...  
WO/2007/036038A1
This invention relates to the field of buoyant aircraft and operation thereof, in particular, airships with improved stability. The present invention is directed to non-rigid, non-spherical airships having an envelop contained within the...  
WO/2007/037932A2
An airship including a hull having a lenticular shape and a fairing attached to the hull to act as a stall strip and reduce the lift generated by the hull. The hull is symmetrical along a central horizontal plane and the fairing may be p...  
WO/2007/024965A2
An aerodynamic fairing system for an airship (10) having a substantially spherical balloon portion (12) includes an inflatable fairing that is attachable to the balloon portion (12) , and a fairing actuation mechanism that selectively in...  
WO/2007/021361A2
A system and method for moving an aerial vehicle along a flight path includes rotatable hubs mounted on opposite sides of the vehicle. Elongated airfoils are mounted on the hubs parallel to a common hub axis for rotation about the hub ax...  
WO/2007/016142A2
The present invention comprises an inflatable balloon of sufficient volume and buoyancy to allow a human pilot to float above the ground and to glide over the ground within an enclosed area. The balloon incorporates several safety featur...  
WO/2007/007353A1
The aircraft (10) comprises an elongated framework (26) provided with propelling means and direction-control planes. The framework is coupled to a pneumatic chamber (16) suited to be filled with lighter-than-air gas and comprising two tu...  
WO/2007/003206A1
The aim of the invention is to position an unmanned aircraft (1) that is used as a platform (10) for telecommunication or other scientific purposes at a predetermined altitude in the stratosphere. Said aim is achieved by an unmanned airc...  
WO/2007/001369A2
An aircraft including a ducted fan and an engine for driving the ducted fan includes a plurality of vanes movably mounted to the aircraft at a substantially rectangular exhaust end of the aircraft. Each of the plurality of vanes is subst...  
WO/2006/137880A2
Various embodiments of the invention relate generally to systems for providing active vertical control of an airship. More particularly, at least one embodiment of the invention relates to a system for actively controlling the aerostatic...  

Matches 401 - 450 out of 1,582