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AIRCRAFT, LIGHTER-THAN-AIR

Subclass of:

244 - Aeronautics and astronautics

Patent class list (only not empty are listed)

Deeper subclasses:

Class / Patent application numberDescriptionNumber of patent applications / Date published
244030000 Airships 62
244031000 Balloons 45
244025000 Airships with sustaining wings 13
244029000 Airship and fluid sustained 3
20090314879HYBRID THERMAL AIRSHIP - An airship comprises a shell, a gas storage system, an air storage system, a cargo storage system, a heating system, and a propulsion system. The shell encompasses a volume. The gas storage system is located within the volume, wherein the gas storage system is capable of storing a lighter than air gas. The air storage system is located within the volume, wherein the air storage system is capable of storing heated air. The heating system is capable of heating air. The propulsion system is capable of propelling the shell during flight.12-24-2009
20100012771HYBRID LIFT AIR VEHICLE - 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 positioned on the airframe, and at least two variable and reversible lateral thrusters are mounted on the envelope or mounted on truss arms attached and extending out from the airframe, wherein, when the vehicle is connected to the payload for transport, the helium or other lighter-than-air gas supports or substantially supports the weight of the vehicle and the vertical thrusters are then continuously engaged to support the weight of the payload and to provide lift to the payload, wherein the lateral thrusters are then engaged to effect lateral movement of the vehicle to the delivery location, whereby, once at the delivery location, the lift provided by the variable and reversible vertical thrusters is reduced or reversed so as to allow the air vehicle to descend and the payload to again engage the ground surface, and where necessary, the variable and reversible vertical thrusters may be reversed to facilitate the unloading of the payload from the vehicle, the vehicle continuing to be kept aloft, once unloaded, by the helium or other lighter than air gas. In this manner, the vehicle utilizes the helium or lighter than air gas to offset or substantially offset the weight of the vehicle, the vertical thrusters providing the power to lift the payload.01-21-2010
20140001308AIRBORNE PLATFORM01-02-2014
244026000 Airship and helicopter sustained 2
20120273608 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.11-01-2012
20180022461Hybrid airship01-25-2018
Entries
DocumentTitleDate
20090206194AIRSHIP PHOTOCATALYTIC REACTOR ENERGY GENERATION, STORAGE, AND TRANSMISSION SYSTEMS - An energy management system for lighter-than-air vehicles which includes a reactor means for generating energy, storage means for storing the reactants used in the reactor means, and an integrated pipeless reactant and power distribution means.08-20-2009
20120001017INSTALLATION PLATFORM FOR DEPLOYING AN EARTH-BASED SENSOR NETWORK UTILIZING A PROJECTED PATTERN FROM A HEIGHT - An installation platform for deploying an earth-based sensor network utilizing a projected pattern from a height. The installation platform includes an aerostatic aircraft, at least one sensor-location projector, and a projector stabilizer. The sensor-location projector is coupled with the aerostatic aircraft, and is configurable to project the projected pattern including at least one sensor-location marker associated with a location for a sensor in the sensor network. The projector stabilizer is configurable for maintaining the sensor-location projector in a sufficiently static orientation relative to the location for the sensor to allow deployment of the sensor within a specified distance of the location on a surface of the earth from the sensor-location marker. A sensor-network-deployment system along with a method for deploying the sensor-network are also provided.01-05-2012

Patent applications in all subclasses AIRCRAFT, LIGHTER-THAN-AIR

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