Abstract: A laminate material for lighter-than-air vehicles includes at least one monofilament yarn layer, a high modulus film layer adjacent to said at least one monofilament layer and optionally including reinforcing fiber or inorganic filler, and a metallized coating adjacent to said high modulus film layer.

Abstract: An unmanned, lighter-than-air airship includes three omnidirectional thrust generating units. One unit is mounted at the fore-end of the airship to generate thrust in a plane that is perpendicular to the longitudinal axis of the airship. This unit controls pitch and yaw movements of the airship. The other two units are mounted on the airship equidistant from the first unit, and are located in a same midships plane that is perpendicular to the longitudinal axis. These two units generate thrust vectors that control roll movements of the airship and provide propulsion for the airship.

Abstract: An elevated sailing apparatus that extracts traction power from the wind. It operates without the heeling moment (typical of conventional sailboats), which constrains the design and limits the power that can be used. A wing or sail is attached beneath a streamlined blimp with aerodynamic stabilizers that keep both the blimp and the wing (or sail) directed into the wind. The blimp is directed into the wind for minimum drag. The wing (or sail) is directed into the wind for a desired angle of attack. The apparatus is tilted so that a combination of dynamic lift and lateral propulsive force is generated in addition to the static lift generated by the blimp. A single tether transfers these aerodynamic forces to a boat or other vehicle. Conventional electronically operated automatic and remote control systems can be used to adjust the tilt and to tack the apparatus.

Abstract: An aerodynamic fairing system for an airship having a substantially spherical balloon portion includes an inflatable fairing that is attachable to the balloon portion, and a fairing actuation mechanism that selectively inflates and deploys the fairing after lift-off, and deflates and retracts the fairing before landing. The actuation mechanism includes an inflation/deflation mechanism and a deployment/retraction mechanism that cooperate to deploy and inflate the fairing, and to deflate and retract the fairing. The fairing includes a substantially conical, inflatable tail section tapering from a wide forward end to a narrow aft end, and a collapsible annular collar connecting the forward end of the tail section to the balloon portion. The inflation/deflation mechanism includes a fan system in the tail section, and the deployment/retraction mechanism includes a plurality of cables attached between the tail section and a plurality of winches mounted on the balloon portion.

Abstract: A hovering wind turbine (1) whose blades (2) lie on the surface of an imaginary horizontal cylinder and have their pitch angle changing as a function of the rotational angle, allowing them to gather wind energy mainly in the upwind and downwind sectors of the cylindrical path and to use a fraction of the gathered energy to create lift by deflecting air downwards, mainly in the upper and lower sectors of the cylindrical path. The remainder of the gathered wind energy is used to drive a pair of on board electrical power generators (9), and anchoring tethers (13) carry electrical current to a land of offshore site. The turbine (1) is tied to a blimp (11) that is purposely located in its wind shade and keeps it airborne during periods of light or no wind.

Abstract: In one aspect, a hybrid airship including an outer shell, a plurality of helium filled gas envelopes, and an all-electric propulsion system may have the shape of a delta-wing. In some embodiments, the hybrid airship may be launched using buoyancy lift alone and aerodynamic lift may be provided by the all-electric propulsion system. In one aspect, a photovoltaic array and a high energy density power storage system may be combined to power the propulsion system making the propulsion system regenerative. The delta-wing shape can provide a surface area large enough to accommodate very large circular or elliptical transmission devices. By continuously recharging the power storage system, the hybrid airship in accordance with some embodiments can stay aloft at an operational altitude of at least about 85,000 ft for months or even years. The hybrid airship may function as an airborne military communications relay platform.

Abstract: An apparatus and associated method for launching and recovering a lighter-than-air aircraft are provided. The aircraft includes an envelope that is substantially filled before launch with a lift gas and a second gas. The lift gas and second gas are substantially separated in the envelope by a boundary layer of mixed gas, formed by the lift and second gases. The aircraft is supported by one or more masts as the lift gas is injected to achieve the required buoyancy for launch. The aircraft is then released and rises, for example, in an inclined orientation. As the aircraft climbs, the lift gas expands in the envelope, and the second gas is vented therefrom. During horizontal descent, air can be pumped into the envelope to maintain the envelope in a substantially filled configuration. The air and lift gas can be mixed to avoid sloshing and pooling.

Abstract: An elevated sailing apparatus that includes one or more wings, tethered to a conveyance, and suspended from beneath a streamlined, lighter-than-air blimp. The wings generate both propulsive and lifting forces from the wind. The propulsive force is used to propel a conveyance. The lifting force prevents the apparatus from being pushed into the water by the propulsive force. The wings use stabilizers to orient them to the oncoming wind and control surfaces to adjust the angle of orientation. A ballast weight provides a vertical reference relative to the blimp, so that the propulsive and lifting forces can be controlled independently. A remote control system allows the degree of lifting force and propulsive force to be controlled from the conveyance. Thus the pilot may tack the apparatus and control its altitude. The use of a streamlined blimp and high aspect-ratio wings allows this elevated sailing apparatus to achieve the low drag-angle necessary for high-speed sailing.

Abstract: A lighter-than-air ship using hydrogen or other gas as a lift gas with at least one hydrogen fuel cell aboard. The fuel cell can draw hydrogen fuel from the lift gas reservoir to produce electricity both for the ship's use and optionally for propulsion. The waste product of the fuel cell is water which can be used for the needs of a crew on the ship. The hydrogen lift gas chamber, which can be compartmentalized for lift control, can be surrounded by a safety jacket filled with an inert gas and contain optional hydrogen and/or oxygen sensors.

Abstract: A vertical lift aircraft comprises a cabin mounted to an enclosed rotary wing which provides vertical lift for the aircraft. The rotary wing includes an annular housing and a main rotor blade rotatable within a space circumscribed by the housing. The main rotor blade is rotatable about a rotation axis that is tilted forwardly from a vertical axis of the aircraft. A horizontal directional control for the aircraft includes a plurality of control slides disposed at spaced locations along the housing and being movable inwardly and outwardly in a radial direction between a neutral position in which the control slides are retracted from the downdraft area and an operational position in which the control slides are extended into the downdraft area. Selective deployment of one or more control slides in the operational position effects horizontal directional turning of the aircraft in the direction of the one or more deployed control slides.

Abstract: An aircraft includes at least one airfoil having a leading edge and a trailing edge. A number of pulse detonation engines are distributed along one of the leading and trailing edges of the airfoil and are positioned beneath the airfoil. Each pulse detonation engine is adapted for impulsively detonating a fuel/oxidizer mixture to generate a thrust force and to apply the thrust force to the aircraft. At least one of the pulse detonation engines is movably configured for altering a direction of the thrust force relative to the airfoil.

Abstract: A variable-lift device using a helium to fly. The device comprises a balloon (1) composed of an outer flexible envelope (3) supported by a rigid structure. The rigid structure comprises a plurality of hollow toruses (4) of inside volume that acts as a tank for storing helium under pressure.

Abstract: A means to use the natural forces of nature when correctly understood and applied to move personnel and objects from Earth's surface to outer space using a conduit with valves, access air locks, support & stabilizing means, to redirect and throttle naturally occurring forces. A magnetic field may also be used. The magnetic field may be applied parallel or longitudinal to the conduit. “Outer space lake substance” Redirecting Means may be utilized with the conduit in order to assist in moving a vessel with personnel or objects to or from outer space.

Abstract: An autonomous stratospheric airship comprising a hull which contains an equipment bay, forward and aft ballonets, forward and aft air management sub-systems, a propulsion system, and a control system is described. The airship also comprises a regenerative solar energy power and storage sub-system which allows powered daytime and nighttime operations. Further, the control system of the airship enables autonomous operation between selected waypoints or along a specified line of sight. The solar arrays utilized by the airship are internally mounted and gimballed so as to provide maximum collection efficiency and not impede the aerodynamic profile of the airship. A greatly simplified and slightly less controllable version of the airship, which makes use of alternative solar array control and ballast management systems, while carrying the equipment bay on the exterior of the hull, is also disclosed.

Abstract: A winged hybrid airship (dynastat) combining the advantages of lighter-than-air (LTA) and heavier-than-air (HTA) aircrafts is disclosed. By combining the dynamic lift of low drag, high aspect ration airfoils (e.g., length over chord >10) with the static lift of low drag, laminar-airflow airships, a platform is formed which is capable of prolonged high altitude flight, maintaining station over a given point on the earth, carrying a payload of communications, reconnaissance or meteorological equipment. Solar collection cells and microwave antennas allow for recharging of on board batteries/fuel cells for powering both the airship and on board avionics computers and reconnaissance or meteorological equipment. An alternate embodiment, having strengthened structural members, is able to provide low altitude heavy cargo lift in remote regions regions or cross country transport of goods.

Abstract: An aircraft includes an aircraft body that retains gas that is lighter than air and rotates about a vertical axis, and a cargo carrier attached to the body so that the carrier does not rotate with the body. The aircraft includes one or more propulsion devices that cause the aircraft body to rotate and to move laterally through air. The propulsion devices use gas retained in the aircraft body as fuel. One or more wings may extend from the body, which control the vertical motion of the aircraft during travel. A computerized navigation system is provided with the aircraft to permit the aircraft to be preprogrammed to travel a desired travel path, or to permit the aircraft to be remote controlled. The electronic components of the aircraft are powered by one or more power supplies, which may also act as ballast weights to raise the center of gravity of the aircraft as it spins, and to maintain tension on the aircraft body as fuel is consumed.

Abstract: A lighter-than-air craft, which may be a freely floating balloon or may be an airship with its own propulsion, has an envelope which is filled with at least a substantial proportion of steam to provide buoyancy. Liquid water which accumulates at a low point of the interior of the envelope is passed out from the envelope and is discharged into the atmosphere, and stored ballast is also discharged into the atmosphere. The ballast discharge mass rate may be brought to be approximately equal to the water discharge mass rate, either manually or automatically; and the ballast discharge mass rate may be manually varied within a certain range around the water discharge mass rate. The ballast may be water. A drain valve may be provided for draining off liquid water as it condenses upon the inside of the envelope while preventing gas from escaping or entering, and a boiler may be provided for reboiling the drained off water into steam which is supplied back into the envelope.

Abstract: A hybrid air vehicle having a gas-filled contoured flattened hull including a pair of longitudinally extending side lobes defining, on the underside of the hull, a longitudinally extending central recess, a payload module received in the central recess and air cushion landing gear units on the underside of said side lobes of the hull. The landing gear units are spaced apart on either side of the payload module. The hybrid air vehicle has characteristics of an airplane, a lighter-than-air airship and a hovercraft.

Abstract: An apparatus for inflating and deploying an aerostat having a nose section and a tail section includes a cylindrical container for housing the deflated portion of the aerostat. The cylindrical container is formed with an open end and defines a longitudinal axis. A feed hose extends from a gas source, through the container to a hose end that projects axially from the open end of the container. The deflated aerostat is initially folded to juxtapose the nose and tail of the aerostat. Next, the nose of the aerostat is attached to the feed hose end and the remaining portion of the aerostat is folded and inserted into the container. As the tail section is inflated outside of the container, aerostat cloth is drawn from the container. A mechanism is provided to control the release of cloth from the container and maintain pressure in the inflating aerostat within a predetermined range.

Abstract: An autonomous stratospheric airship comprising a hull which contains an equipment bay, forward and aft ballonets, forward and aft air management sub-systems, a propulsion system, and a control system is described. The airship also comprises a regenerative solar energy power and storage sub-system which allows powered daytime and nighttime operations. Further, the control system of the airship enables autonomous operation between selected waypoints or along a specified line of sight. The solar arrays utilized by the airship are internally mounted and gimballed so as to provide maximum collection efficiency and not impede the aerodynamic profile of the airship. A greatly simplified and slightly less controllable version of the airship, which makes use of alternative solar array control and ballast management systems, while carrying the equipment bay on the exterior of the hull, is also disclosed.

Abstract: A device to provide control of the trajectory of a lighter than air vehicle, such as a balloon, is provided. A lifting device, such as a wing on end, is suspended on a tether well below the balloon to take advantage of the natural variation in winds at different altitudes. The wing can generate a horizontal lift force that can be directed over a wide range of angles. This force is transmitted to the balloon by the tether. Due to this force, the balloon's path is altered depending on the relative sizes of the balloon and the wing. A relatively small amount of power is needed to control the system, possibly with a rudder. As the energy of the wind provides most of the force, the wind's energy does most of the work. The balloon is able to avoid hazards, to reach desired targets, to select convenient landing zones, and to provide other operational advantages.

Abstract: An autonomous stratospheric airship comprising a hull which contains an equipment bay, forward and aft ballonets, forward and aft air management sub-systems, a propulsion system, and a control system is described. The airship also comprises a regenerative solar energy power and storage sub-system which allows powered daytime and nighttime operations. Further, the control system of the airship enables autonomous operation between selected waypoints or along a specified line of sight. The solar arrays utilized by the airship are internally mounted within the bull and gimballed so as to provide maximum collection efficiency and not impede the aerodynamic profile of the airship. A greatly simplified and slightly less controllable version of the airship, which makes use of alternative solar array control and ballast management systems, while carrying the equipment bay on the exterior of the hull, is also disclosed.

Abstract: An spacecraft/airship, which uses buoyancy and thrusters to ascend into space with lifting gas as propellant or fuel for thrusters, which may be conventional thrusters or electric turbojets or ion thrusters. The airship aspect has gas retaining structures that can regulate the density of the gasses within. The spacecraft aspect provides for mounting thrusters, control, power, services, and interior space for missions of the spacecraft/airship.

Abstract: An autonomous stratospheric airship comprising a hull which contains an equipment bay, forward and aft ballonets, forward and aft air management sub-systems, a propulsion system, and a control system is described. The airship also comprises a regenerative solar energy power and storage sub-system which allows powered daytime and nighttime operations. Further, the control system of the airship enables autonomous operation between selected waypoints or along a specified line of sight. The solar arrays utilized by the airship are internally mounted and gimballed so as to provide maximum collection efficiency and not impede the aerodynamic profile of the airship. A greatly simplified and slightly less controllable version of the airship, which makes use of alternative solar array control and ballast management systems, while carrying the equipment bay on the exterior of the hull, is also disclosed.

Abstract: In a cruise airship whose hull (S) has the form of an ellipsoid, this ellipsoid has three axes of different lengths at right angles to one another, whereby a longitudinal axis (L), which is horizontally oriented in the position for travel, a transverse axis (Q), which is horizontally oriented in the position for travel and at right angle to the longitudinal axis (L), and a vertical axis (H), which is vertically oriented in the position for travel, possess the longest, middle and shortest length respectively.

Abstract: A power generation, transmission and distribution system for an aerostat using a tether, includes a ground-based power delivery system for generating a multi-phase power signal having a frequency at least greater than 400 Hz, an aerostat-based power distribution system for receiving the multi-phase power signal, and a tether for delivering the multi-phase power signal from the ground-based power delivery system to the aerostat-based power distribution system. The base power system generates a 3, 6, or 12 phase base power signal having a nominal frequency signal received by a rectifier to generate a high voltage DC output. A converter/inverter receives the high voltage DC output and generates the multi-phase power signal transmitted by the tether. A transformer aboard the aerostat steps down the multi-phase power signal and a rectifier processes the stepped-down multi-phase power signal into a DC power delivery signal.

Abstract: The cableway consists of a captive balloon (1) carrying a gondola (2) to which two transport cables (3, 4) and a mooring cable (5) are attached. The two transport cables (3, 4) bearing a cabin (10, 11) for carrying passengers end at a ground station (7) which is rotatable on a circular rail (9) around a vertical axis (8). The transport cables (3, 4), both in the gondola (2) and in the ground station, run on and off drums. The ground station (7) can be actively tracked with reference to the site of the captive balloon (1). The mooring cable (5), secured to the gondola (2), runs on a drum in the ground station (7) and is equipped with beacons (13). The captive balloon (1) can be released to any desired height, the unused length of the transport cables (3, 4) remaining on the drums in the ground station (7). The cabins (10, 11) are coupled in shuttle operation or move separately driven by motors provided in the gondola (2).

Abstract: An apparatus and method for floating such apparatus in the air, such apparatus having at least one cell containing air and a fluid. The fluid in one embodiment is heated to create steam which, in turn, makes the cell lighter than the surrounding air, thereby providing lift to the apparatus.

Abstract: An airship/spacecraft, which, in a preferred embodiment, uses its lifting gas as fuel for thrusters, which may be of the turbo-type or rocket type, or both, to achieve transition to space flight. The airship aspect has gas retaining structures that can withstand internal and external pressure and can change in volume and shape. The spacecraft aspect provides control, power, services, and interior space for missions of the airship/spacecraft.

Abstract: An inflatable airship of predetermined volume is filled with gas to lift a predetermined weight to a predetermined high altitude. An elevator module is releasably secured to a gondola attached to the airship. A cable of a length at least equal to the deployment altitude of the airship has a first end attached to the elevator module and a second end attached to a winch mounted on the gondola. The airship is raised with the elevator module anchored to the ground and the cable is unwound from the winch as the airship rises. Once the desired operating altitude is reached, the winch is reversed to wind the cable onto the winch and raise the elevator module to the gondola.

Abstract: A method and apparatus for controlling the flight direction of a blimp. The blimp includes an elongate fuselage for containing a lighter-than-air gas, a movable rudder located toward a tail end of the fuselage, and at least one propeller mounted on a side of the fuselage. The propeller is attached to the blimp by a connection that provides two axes of movement. The propeller connection can be rotated or pivoted (1) about a first axis which is a horizontal axis that is perpendicular to a direction of the longitudinal axis of the elongate fuselage, and/or (2) about a second axis which is a vertical axis that is perpendicular to the direction of the longitudinal axis of the fuselage.

Abstract: An airborne monitoring system for measuring conditions in the lower atmospheric boundary layer of a tropical cyclone or other concerted atmospheric systems. The system flies on the wind. In the case of a tropical cyclone it flies over the sea, into the eye and tracks the storm, transmitting meteorological data and receiving commands from a remote base station. The system includes a hybrid lifting body tethered from a line contacting the surface of the sea. It is maintained in aerodynamic and hydrodynamic balance at a substantially constant altitude.

Abstract: A helium purification system for use with lighter-that-air airships has a catalytic purification stage for removing oxygen from the lift gas, and if desired, a nitrogen removal stage. Impure lift gas is passed through the catalytic purification stage which includes catalytic means for reacting hydrogen and contaminating oxygen entrained in the lift gas to form water and liberate heat energy. The catalytic reaction of oxygen and hydrogen increases the lift capacity of the airship both by removing oxygen from the lift gas which can then be replaced with additional lift gas and by heating the lift gas. The lifht weight catalytic purifier requiring no external power makes practical an on-board lift gas purifier to scavenge oxygen from the lift gas as soon as it enters the aerostat whose only cost of operation is that of the hydrogen consumed.

Abstract: What has been created is a new form of an equipment/kite that carry weight in mid-air regardless of fuel and/or wind, which converts the wind energy into mechanical energy by acting as a sail in a multi-level formation, which is in the form of a large flat air balloon 1/2 acre to more than 5 acres wide that floats in the air concave downward against the wind, which functions as a large kite in the presence of wind--soaring upward instead of being blown down which may be constructed into a multi-level balloon kite from ground to the highest altitude of wind to carry several rotary blade windmills on each kite or top pull transportation on land or on water or on aerial cable railway; to carry electric wire conductors up into the clouds to collect electricity from the clouds; to carry lamps, advertisements, and observatory instruments to high altitudes; to serve as sail for large type of windmills in a configuration similar to the United Sail Windmill under U.S. Pat. No.

Abstract: A multi stage high-altitude data acquisition system comprising a first stage manned lighter-than-air, engine propelled aircraft and a second stage air-buoyant vehicle of stratospheric altitude attaining capability statically sustainable aloft by a sufficient quantity of lighter-than-air gas contained within an expandable envelope balloon to carry the vehicle to a stratospheric float altitude and transportable from ground level to a tropospheric launching altitude by the first stage aircraft from which the air buoyant vehicle and its partially expanded gas containing envelope is releasable at the launching level while the first stage aircraft is established in a flight condition of substantially zero airspeed.

Abstract: A lighter-than-air craft [10] having an outer envelope [11] divided into an inner envelope [25] and a plurality of compartments [40,41,42]. The compartments are filled with lifting gases such as helium and hydrogen and the overall lifting force of the craft is regulated by supplying hot air to the inner envelope.

Abstract: A flexible solar skin which absorbs radiant solar energy to convert it into electricity, made possible through a conductive plastic, which conceals a conductive fiber, whereby the fiber directs generated electricity to a terminal in the form of a contact strip hemmed or fused alongside the material. Additionally, an air vehicle covered with this photovoltaic material to collect solar radiant energy during flight which is converted into electricity to assist the propulsion system of the vehicle.

Abstract: An airship is provided utilizing a spherical balloon filled with buoyant gas such as helium at a pressure substantially greater than atmospheric so that its dimensions are substantially unaffected by changes in atmospheric pressure or temperature. The spherical balloon is rotatably mounted on a normally horizontal axle having end portions projecting from opposite sides of the balloon, and includes a rigid load supporting yoke including two arms extending upwardly from a central load supporting structure and each with an upper end suspended from the axle. The yoke arms carry engines which propel the airship in a forward direction transverse to the axle, and means are provided for rotating the balloon about the axle so that the balloon front surface moves upward relative to the centre of the balloon and provides lift due to the Magnus effect.