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254 results about "Lighter than air" patented technology

Lighter than air refers to materials that are buoyant in air because they have densities lower than that of air. Dry air has a density of about 1.29 g/L at standard conditions for temperature and pressure, and an average molecular mass of 28.97 g/mol. Some of these gases are used as lifting gases in lighter-than-air aircraft, which include free balloons, moored balloons, and airships, to make the whole craft, on average, lighter than air..

System and method of aerial surveillance

A system and method for an aerial surveillance system are disclosed. Briefly described, one embodiment comprises a lighter-than-air aerial platform, at least one image capture device carried by the lighter-than-air aerial platform and operable to sequentially capture a plurality of images, and at least one control surface physically coupled to the lighter-than-air aerial platform and operable to control direction of movement of the lighter-than-air aerial platform along a surveillance path in response to a guidance control signal determined in part upon the sequentially captured plurality of images.
Owner:ROBOTICVISIONTECH

Methods of using fuel cell system configured to provide power to one or more loads

A fuel cell system is described for providing primary and / or auxiliary / backup power to one or more loads selected from the group comprising: lawn & garden equipment; radios; telephone; targeting equipment; battery rechargers; laptops; communications devices; sensors; night vision equipment; camping equipment; stoves; lanterns; lights; vehicles; cars; recreational vehicles; trucks; boats; ferries; motorcycles; motorized scooters; forklifts; golf carts; lawnmowers; industrial carts; passenger carts (airport); luggage handling equipment (airports); airplanes; lighter than air crafts; blimps; dirigibles; hovercrafts; trains; locomotives; submarines (manned and unmanned); torpedoes; security systems; electrical energy storage devices for solar-based, tidal-based, hydro-based, wind-based, and other renewable energy source; equipment for which a primary and / or backup power source is necessary or desirable to enable the equipment to function for its intended purpose, military-usable variants of above, and suitable combinations of any two or more thereof. The system provides power to the one or more loads upon the occurrence of a power outage condition, which includes a disruption or discontinuation in the delivery of primary power (i.e., power from a system-external primary source, namely, a source other than the fuel cell system) to, or power demand condition by, the one or more loads. A controller senses outage of primary power to, or demand for primary power by, the one or more loads, and, responsive thereto, operatively engages one or more fuel cells to provide power to the one or more loads.
Owner:METALLIC POWER INC

Systems and Methods for Long Endurance Airship Operations

ActiveUS20130037650A1Improve stationkeeping performanceAltering aerodynamic characteristicsAircraft componentsConvertible aircraftsLighter than airPayload
In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain aloft for greater than 30 days without physical connection to the ground. Illustrative methods for long endurance airship operations are also provided.
Owner:STRATOSPHERIC AIRSHIPS

Systems and applications of lighter-than-air (LTA) platforms

InactiveUS20050014499A1Large costLarge deploymentHydrogenAircraft controlEngineeringFloating platform
Innovative new methods in connection with lighter-than-air (LTA) free floating platforms, of facilitating legal transmitter operation, platform flight termination when appropriate, environmentally acceptable landing, and recovery of these devices are provided. The new systems and methods relate to rise rate control, geo-location from a LTA platform including landed payload and ground-based vehicle locations, and steerable recovery systems.
Owner:SPACE DATA CORP

Accident monitoring using remotely operated or autonomous aerial vehicles

A system to monitor vehicle accidents using a network of aerial based monitoring systems, terrestrial based monitoring systems and in-vehicle monitoring systems is described. Aerial vehicles used for this surveillance include manned and unmanned aircraft, satellites and lighter than air craft. Aerial vehicles can also be deployed from vehicles. The deployment is triggered by sensors registering a pattern in the data that is indicative of an accident that has happened or an accident about to happen.
Owner:SCOPE TECH HLDG

Airborne basestation

A wireless communications basestation that utilizes a light weight high directivity electronically-steerable antenna mounted on a lighter-than-air vehicle to providing relay broadband communication service among mobile units in a geographic area is provided. The lighter-than-air vehicle carries aloft the antenna; a radio and a switching device for routing. A gateway may also be provided to enable communications with a wide area network. A communication system for a geographic area utilizing the airborne wireless communications basestation is also presented. The system includes a number of user equipment units located in the geographic area in communication with the airborne wireless communications basestation. The user equipment units may utilize omni-directional antennas for low data rate communications, and / or a high directivity antenna.
Owner:THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY

Apparatus having an energy generating skin as an outer covering

The invention relates to an outer covering of an apparatus made of an energy generating skin. The energy generating skin encloses a fuel that is capable of reacting with oxygen in an electrochemical reaction to form electricity and gaseous products. In preferred embodiments, the energy generating skin is a hydrogen oxygen fuel cell which serves as the outer covering of an aircraft such as a lighter than air ship or an airplane.
Owner:LOCKHEED MARTIN CORP

Lighter than air balloon made from a biaxially oriented polyester film

A long life balloon formed from a lamination. The lamination includes a polyester film with a total thickness of 4 μm to 12 μm. The polyester film includes a biaxially oriented polyester core layer and at least one amorphous copolyester skin layer. The lamination also includes a sealant layer and a gas barrier layer on an opposite side of the polyester film from the sealant layer. The oxygen transmission rate of the balloon is less than 0.1 cc / 100 sqin / day, a bonding strength of the gas barrier layer to the surface of the polyester film is more than 300 g / in at dry conditions, a sealing strength of the balloon is more than 3.5 kg / in, and a floating time of the balloon is more than 20 days.
Owner:TORAY PLASTICS AMERICA +1

Hybrid lift air vehicle

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 engagement with the envelope and at least two variable thrust lateral thrusters in secure engagement with the envelope, means for temporarily securely engaging the load to the envelope wherein the volume of lighter-than-air gas has a buoyancy that offsets at least 25% of the weight of the air vehicle when unloaded, wherein the thrust from the at least two vertical thrusters may be varied to raise and lower the air vehicle and the load when engaged, and wherein the thrust from the at least two lateral thrusters may be varied to maneuver and transport the raised air vehicle and the load when engaged.
Owner:JESS PETER E +1

Balloon trajectory control system

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. As a result, fewer flights must be terminated early due to an inability to control the trajectory, and it is easier to obtain permission to launch since a planned flight path can be achieved within a greater range of conditions.
Owner:GLOBAL AEROSPACE

Apparatus and method to control the flight dynamics in a lighter-than-air airship

An apparatus and method to control the attitude, heading course, altitude and position of a lighter-than-air airship. In one aspect, a hybrid airship including a lighter-than-air gas filled envelope, a thrust vectored front propulsion system, a back rotary wing system and a onboard control system. In one aspect, at least one system to modify the on board mass, a system to control the internal pressure, at least a power battery pack and a radio link communications for unmanned piloting. Said hybrid airship has improved maneuverability, safely flights and is capable to fly as Lighter-than-air airship and Heavy-than-air aircraft.
Owner:QUINTANA JAVIER

Wind power generation system for lighter than air (LTA) platforms

An apparatus includes a lighter than air platform, a reversible propulsive / wind turbine, a deployable anchor to constrain movement of the lighter than air platform with respect to an anchor point allowing wind to drive the turbine, and a generator / motor coupled to the turbine to produce electrical power when movement of the lighter than air platform is constrained. A method performed by the apparatus is also provided.
Owner:NORTHROP GRUMMAN SYST CORP

Solar-powered aircraft

A solar-powered aircraft uses solar energy to electrolyze on-board water to produce hydrogen. The hydrogen fills various on-board tanks, causing the aircraft to become lighter than air. The hydrogen is also used to operate a fuel cell which provides power for electrical equipment, including a motor for turning a propeller. Water produced as waste by the fuel cell is recycled for use in the production of hydrogen. When hydrogen is removed from the tanks, either because it is consumed by the fuel cell or because it is compressed and pumped out of the tanks, air returns to the tanks, and the aircraft becomes heavier than air. The aircraft can thus be made to climb and descend by making it lighter than air, or heavier than air. The aircraft emits no harmful substances into the environment. The aircraft can remain aloft indefinitely, limited only by an insignificant amount of leakage of hydrogen and water.
Owner:FULLER HOWARD J

Hybrid air vehicle having air cushion landing gear

InactiveUS6880783B2Efficient aerodynamic liftSimple interfaceFloatsNon-rigid airshipsJet aeroplaneFlight vehicle
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 the 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.
Owner:HYBRID AIR VEHICLES

Hovering Surveillance Air Vehicle

A hovering surveillance device. An electronic imaging device is disposed on a housing having a primary lift element, at least one compressed lighter-than-air gas element, a pitch adjustment element, and, a steering element. The compressed lighter-than-air gas is channeled to the primary lift element and the pitch adjustment element to selectively vary the altitude and angle for the housing such that scene of interest may be imaged. The lighter-than-air gas may be selected from the group of helium, hydrogen, heated air, neon, ammonia, and methane.
Owner:PFG IP

Reduced weight flexible laminate material for lighter-than-air vehicles

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.
Owner:LOCKHEED MARTIN CORP

Apparatus and method utilizing cells to provide lift in lighter-than-air airships

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.
Owner:BROTZ GREGORY R

Apparatus and method for lighter-than-air aircraft

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.
Owner:THE BOEING CO

Lighter-than-air vehicle for shading

The lighter-than-air vehicle for shading is an airborne, movable system that provides shade from the sun for an open area. The vehicle is a substantially flat flying device having upper and lower surfaces, and which is filled with a lighter-than-air gas or gases, such as helium or hydrogen. The vehicle may be tethered to the ground through control wires, or may be fully autonomous and controlled by propeller fans. The required power may be provided by wire from ground, or through a portable power source, such as solar cells, mounted atop of vehicle. The vehicle has sun sensors that allow it to track the sun, and provides around the clock shaded area underneath its surface. The vehicle can also have pressure sensors and altitude sensors that may trigger an alarm in case of an emergency descent to the ground.
Owner:KING FAHD UNIVERSITY OF PETROLEUM AND MINERALS

Atmospheric data collection and recovery systems and methods

A payload delivery and recovery system, having a payload including a data collection device arranged to collect data, and a controllable ascent vehicle comprising a controllable lighter than air (LTA) mechanism detachably coupled to the payload and used during an ascent phase to deliver the payload to a pre-determined altitude. The payload delivery and recovery system also having a controllable descent mechanism releasably attached to the controllable ascent vehicle and that can be used during a descent phase for reducing a rate of descent of the payload subsequent to release of the payload at the pre-determined altitude and including a control system for navigating the payload to a desired ground location during a recovery phase.
Owner:LONGMIER BENJAMIN +5

Adjusting rigid foil spar system

InactiveUS20130014683A1Easy to adjustWithout the loss of upwind pointing performanceWind propelled vesselsFloating buildingsLeading edgeTrailing edge
A rigid foil sail having a full length vertical leading edge whose trim angle / angle of attack is controlled by the main sheet and trailing edge flaps attached rearwardly of the leading edge, each of which can be independently trimmed from a convenient deck level control tray to achieve easily adjustable camber. The design of the rigid foil sail allows depowering of the sail without altering mainsheet trim by decreasing the camber of the upper trailing flap thus also decreasing the heeling force created by the power of the upper trailing flap. Further, a void within the foil is filled with a lighter than air gas to assist in countering heeling moment to allow the boat to be driven without the loss of upwind pointing performance and without the loss of power and also allowing the boat to be driven to windward more efficiently with a minimum heel angle.
Owner:HOYT JOHN GARRISON
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