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232results about "Modular constructions" patented technology
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Helicopter with multi-rotors and wireless capability
InactiveUS20120083945A1Simple flightSimple usageAutonomous decision making processUnmanned aerial vehiclesNavigation systemFuselage
The present invention relates to a helicopter having a modular airframe, with multiple layers which can be connected easily, the layers which house the electronics (autopilot and navigation systems), batteries, and payload (including camera system) of the helicopter. The helicopter has four, six, and eight rotors, which can be easily changed via removing one module of the airframe. In one embodiment, the airframe has a vertical stacked appearance, and in another embodiment, a domed shape (where several of the layers are stacked internally). In one embodiment, there is a combination landing gear and camera mount. The helicopter allows for simple flight and usage by remote control, and non-remote control, users.
Owner:GEOTECH ENVIRONMENTAL EQUIP
Unmanned aerial vehicle including a removable parcel carrier
ActiveUS20170313421A1Reduce the required powerArresting gearLaunching/towing gearUncrewed vehicleCarrier system
Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information.
Owner:UNITED PARCEL SERVICE OF AMERICAN INC
Methods for landing an unmanned aerial vehicle
ActiveUS20170316701A1Reduce the required powerArresting gearLaunching/towing gearUncrewed vehicleChassis
Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information.
Owner:UNITED PARCEL SERVICE OF AMERICAN INC
Modular adaptive configured helicopter
InactiveUS7946530B1Requirement is not sufficientMinimum dragAircraft ejection meansConvertible aircraftsModularitySelf adaptive
A method and apparatus for a composite helicopter comprising a rotary wing parent vehicle with various modular cabins detachable therefrom to facilitate various configuration aircraft platforms, dual operation and modular economy.
Owner:TALMAGE JR ROBERT N
Transformable airplane
ActiveUS7093798B2Reconfigured easily and rapidlyLow costFuselage framesFuselage bulkheadsCommand and controlFlight vehicle
A transformable airplane may be reconfigured easily and rapidly to perform any one or a combination of tanking, transport, bombing, or command and control missions as desired for a tactical situation by installing or replacing mission-specific modules as desired. A reconfigurable aircraft includes a pair of wings and an aircraft body having at least one bay defined in an interior of the aircraft body. The at least one bay is configured to accept a plurality of removably replaceable modules that configure the aircraft to perform a plurality of missions. Transport mission modules may include space and tie-downs for cargo pallets and / or palletized seating. A roll-on / roll-off ramp may be provided. Tanking mission modules may include a remote aerial refueling operator station. Bombing mission modules may include a bomb rack and a bomb ejector. ISR mission modules may include command and control stations in signal communication with phased array antennas.
Owner:THE BOEING CO
One-piece closed-shape structure and method of forming same
The present invention relates to a one-piece closed-shape structure and a method for manufacturing a one-piece closed-shape structure. In particular, the present invention relates to a one-piece fuselage and a method for manufacturing a one-piece fuselage. One embodiment of the method of the invention involves the use of molding technology, tooling technology, the integration of the molding and tooling technology, and fiber placement to manufacture a one-piece closed shape structure.
Owner:TOYOTA MOTOR CO LTD
Helicopter with multi-rotors and wireless capability
InactiveUS8774982B2Easy to useEasy to disassembleAutonomous decision making processUnmanned aerial vehiclesNavigation systemFuselage
Owner:GEOTECH ENVIRONMENTAL EQUIP
Methods for delivering a parcel to a restricted access area
ActiveUS9928749B2Reduce the required powerArresting gearLaunching/towing gearUncrewed vehicleRestricted access
Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information.
Owner:UNITED PARCEL SERVICE OF AMERICAN INC
Landing assist apparatus interface bulkhead and method of installation
ActiveUS7344108B2Avoid areaAvoid damageArrester hooksAnchoring installationsControl mannerAircraft landing
An aircraft landing assist apparatus is designed to be retrofit to existing aircraft having internal constructions that have been modified to support the apparatus. The apparatus is designed so that on rough landings of the aircraft on a ship deck, the apparatus will collapse in a controlled manner to avoid any damage to ammunition and / or fuel storage areas of the aircraft.
Owner:THE BOEING CO
Cargo aircraft
ActiveUS7261257B2Provide structural rigiditySpeed efficientUnmanned aerial vehiclesEfficient propulsion technologiesEngineeringCargo container
An aircraft for carrying at least one rigid cargo container includes a beam structure with a forward fuselage attached to the forward end of the beam structure and an empennage attached to the rearward end of the beam structure. Wings and engines are mounted relative to the beam structure and a fairing creates a cargo bay able to receive standard sized intermodal cargo containers. Intermodal cargo containers of light construction and rigid structure are positioned within the cargo bay and securely mounted therein. The beam structure is designed to support flight, takeoffs and landings when the aircraft is empty but requires the added strength of the containers securely mounted to the beam structure when the aircraft is loaded. The aircraft is contemplated to be a drone.
Owner:BIOSPHERE AEROSPACE
Universal vehicle with improved stability for safe operation in air, water and terrain environments
ActiveUS20180244383A1Enhanced flight envelopeSafely transitioningAircraft navigation controlPropellersTerrainSystems design
The universal vehicle system is designed with a lifting body which is composed of a plurality of interconnected modules which are configured to form an aerodynamically viable contour of the lifting body which including a front central module, a rear module, and thrust vectoring modules displaceably connected to the front central module and operatively coupled to respective propulsive mechanisms. The thrust vectoring modules are controlled for dynamical displacement relative to the lifting body (in tilting and / or translating fashion) to direct and actuate the propulsive mechanism(s) as needed for safe and stable operation in various modes of operation and transitioning therebetween in air, water and terrain environments.
Owner:UNIV OF MARYLAND
Modular unmanned air-vehicle
InactiveUS7922115B2Lower life cycle costsEasy to transportAircraft stabilisationUnmanned aerial vehiclesJet aeroplaneFlight vehicle
The present invention is an unmanned air vehicle designed for reconnaissance, surveillance, data acquisition, and general research. The air vehicle is a monoplane that consists of several pieces that can easily be assembled using a minimal amount of tools. The air vehicle consists of a forward and aft fuselage section, two identical horizontal stabilizers, and four identical wing sections. The aircraft can fly with all four wing sections, or with just two wing sections (the short wing configuration). Each of the four wing sections of the air vehicle can be interchanged with any of the other wing sections for the purpose of minimizing assembly time and spare parts.
Owner:COLGREN RICHARD D +2
Modular aerospace plane
InactiveUS7234667B1Improve securityImprove performanceAircraft ejection meansRemote controlled aircraftAviationModularity
This invention relates to the design of a Modular Aerospace Plane (MAP) comprising a forward fuselage section, a main wing section, a tail section and wing attachments. Various sections can be integrated to offer a variety of aircraft characteristics, performance and missions. This modular design offers a new method of aircraft fabrication, maintenance, repair and ground handling to reduce costs for the manufacturers, owners and operators. The forward fuselage and tail sections may utilize a parachute device whereby these sections can separate in an emergency and safely lower the occupants to the ground.
Owner:TALMAGE JR ROBERT N
Unmanned aerial vehicle pick-up and delivery systems
ActiveUS20170313422A1Reduce the required powerArresting gearLaunching/towing gearFlight vehicleUncrewed vehicle
Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information.
Owner:UNITED PARCEL SERVICE OF AMERICAN INC
Mission replaceable rotor blade tip section
ActiveUS20060104812A1Flat surfaceMinimize the numberPropellersRotary propellersButt jointEngineering
A rotor blade includes a removable blade tip section which is mounted to an outboard rotor blade section by mechanically mounting a tip spar to a main blade spar with a spar interface section which bridges a butt joint between the blade spar and the tip spar. The spar interface section is mounted within the blade spar and the tip spar with a multiple of threaded fasteners which are under shear load during rotor blade rotation.
Owner:SIKORSKY AIRCRAFT CORP
Aircraft With Integrated Lift And Propulsion System
A vertical take-off and landing (VTOL) aircraft is designed to be so efficient that it can be commercially competitive with runway dependent aircraft operating in a range of 100 to 1000 miles or more, with glide ratios of at least 24. Improvements include a combination of high efficiency tilting rotor and wing design that enable both vertical takeoff and efficient high speed cruising, a high aspect ratio wing, and a variable speed propulsion system efficient in both hover and cruise flight. Preferred aircraft use narrow chord inboard and outboard wings, and use efficient lightweight design to achieve unusually low empty weight fraction. In some embodiments, the rotors use medium rather than high modulus fibers, with wider blades of lower taper ratio, to provide the stiffness and mass properties required for high performance OSTR rotor blades. Also disclosed are VTOL aircraft with glide ratios from approximately 26 to over 40.
Owner:KAREM ABE
Mission replaceable rotor blade tip section
Owner:SIKORSKY AIRCRAFT CORP
Removable lift assembly for a rotorcraft, and a rotorcraft
ActiveUS20150284076A1Drag minimizationReduce resistanceWingsModular constructionsEngineeringFuselage
A lift assembly that is releasably fastened to a fuselage of a rotorcraft. The lift assembly comprises a wing comprising at least two spars. A main gearbox passes through an opening in the suction side of a central box of the wing so that its bottom is attached to a resilient suspension system arranged level with the pressure side of the central box, a top of the main gearbox projecting from the central box and being fastened to at least one spar by at least three suspension bars. A reversible fastener system having a plurality of fastener means serves to fasten the central box reversibly to a plurality of fastener points of a fuselage.
Owner:EUROCOPTER
Modular aircraft system
ActiveUS9505484B1Easy constructionImprove aerodynamic performanceActuated automaticallyDe-icing equipmentsCarrying capacityFlight vehicle
The modular aircraft system includes a single fuselage having a permanently installed empennage and plural sets of wing modules and engine modules, with each wing and engine module optimized for different flight conditions and missions. The fuselage and each of the modules are configured for rapid removal and installation of the modules to minimize downtime for the aircraft. Short wings having relatively low aspect ratio are provided for relatively high speed flight when great endurance and / or weight carrying capacity are not of great concern. Long wings having high aspect ratio are provided for longer range and endurance flights where speed is not absolutely vital. A medium span wing module is also provided. Turboprop, single turbojet, and dual turbojet engine modules are provided for installation depending upon mission requirements for any given flight. The aircraft is primarily adapted for use as an autonomously operated or remotely operated unmanned aerial vehicle.
Owner:AL SABAH NASSER M
Multi-Role Aircraft With Interchangeable Mission Modules
ActiveUS20140231593A1Without adding undue weightFuselage framesAll-wing aircraftAviationTrailing edge
A flight-operable, truly modular aircraft has an aircraft core to which one or more of outer wings members, fuselage, cockpit, leading and trailing edge couplings, and empennage and tail sections can be removably coupled and / or replaced during the operating life span of the aircraft. In preferred embodiments the aircraft core houses the propulsive engines, avionics, at least 80% of the fuel, and all of the landing gear. The aircraft core is preferably constructed with curved forward and aft composite spars, that transfer loads across the center section, while accommodating a mid-wing configuration. The aircraft core preferably has a large central cavity dimensioned to interchangeably carry an ordnance launcher, a surveillance payload, electronic countermeasures, and other types of cargo. Contemplated aircraft can be quite large, for example having a wing span of at least 80 ft.
Owner:KAREM ABE
Aerial vehicle with deployable components
An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and / or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.
Owner:ANDURIL IND INC
Small unmanned airborne vehicle airframe
InactiveUS7699261B2High strengthQuickly and easily assembled and dissembledUnmanned aerial vehiclesRemote controlled aircraftLow speedModularity
An unmanned aerial vehicle (UAV) is designed for low-speed, low altitude, long endurance missions typical to UAVs of this size and class. The UAV structure is configured to be substantially impervious to small arms fire and to have a very small representative radar cross-section. The UAV is modular such that the main wings and tail wing assembly are quickly and easily, detached from the fuselage for ease of transport and to provide an airframe that is quickly and easily adapted to any particular mission.
Owner:LOCKHEED MARTIN CORP
Multi-Role Aircraft with Interchangeable Mission Modules
A flight-operable, truly modular aircraft has an aircraft core to which one or more of outer wings members, fuselage, cockpit, leading and trailing edge couplings, and empennage and tail sections can be removably coupled and / or replaced during the operating life span of the aircraft. In preferred embodiments the aircraft core houses the propulsive engines, avionics, at least 80% of the fuel, and all of the landing gear. The aircraft core is preferably constructed with curved forward and aft composite spars, that couple to outer wing sections and possibly other sections using hardpoints. The aircraft core preferably has a large central cavity dimensioned to interchangeably carry an ordnance launcher, a surveillance payload, electronic countermeasures, and other types of cargo. Contemplated aircraft can be quite large, for example having a wing span of at least 80 ft.
Owner:KAREM ABE
Unmanned aerial vehicle including a removable power source
ActiveUS20170316375A1Reduce physical demandReduce the required powerArresting gearLaunching/towing gearUncrewed vehicleSource system
Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information.
Owner:UNITED PARCEL SERVICE OF AMERICAN INC
Modular Unmanned Aerial System with Multi-Mode Propulsion
InactiveUS20180155021A1Effective flight rangeConvertible aircraftsPower plant fuel tanksPropellerFuselage
A modular Unmanned Aerial System (UAS) includes an Unmanned Aerial Vehicle (UAV) parent module and UAV child modules. A main wing extends from a respective fuselage of the modules. The UAS includes docking mechanisms coupled to wingtips of the main wings. The child modules dock with the wingtips of the parent or an adjacent child module. Docking forms a linked-flight configuration, with undocking and separation from the parent or adjacent child module achieving an independent-flight configuration. The modules have booms arranged transverse to the main wings and parallel to the longitudinal axis, as well as front and rear rotors / propellers. The front and rear propellers have axes of rotation that are normal to a plane of the longitudinal axis in a vertical takeoff and landing (VTOL) configuration, with the axis of rotation of the rear propellers parallel to the longitudinal axis in a forward-flight configuration.
Owner:NASA
Methods for dispatching unmanned aerial delivery vehicles
ActiveUS20170316376A1Reduce the required powerArresting gearLaunching/towing gearDelivery vehicleUncrewed vehicle
Systems and methods include UAVs that serve to assist carrier personnel by reducing the physical demands of the transportation and delivery process. A UAV generally includes a UAV chassis including an upper portion, a plurality of propulsion members configured to provide lift to the UAV chassis, and a parcel carrier configured for being selectively coupled to and removed from the UAV chassis. UAV support mechanisms are utilized to load and unload parcel carriers to the UAV chassis, and the UAV lands on and takes off from the UAV support mechanism to deliver parcels to a serviceable point. The UAV includes computing entities that interface with different systems and computing entities to send and receive various types of information.
Owner:UNITED PARCEL SERVICE OF AMERICAN INC
Hybrid Power Supply For Electric Multirotor Rotorcraft
InactiveUS20170008627A1Increase distanceExtension of timePower plant cooling arrangmentsBatteries circuit arrangementsJet aeroplaneElectric power system
Embodiments are directed towards hybrid power supply that provides electric power to a multirotor rotorcraft to extend range or flying time. In one embodiment, an internal combustion engine and fuel tank are provided that interoperate with a battery provided by a commercial multirotor rotorcraft to substantially extend flying time or flying distance.
Owner:DE SOTO JOAQUIN +1
Methods for fuel-efficient transportation of cargo by aircraft
InactiveUS20090114773A1Much low speedHighly efficient flight profileUnmanned aerial vehiclesAir-treatment apparatus arrangementsTorsional loadUltimate tensile strength
Owner:HELOU JR ELIE
Modular arms on a rotor-based remote vehicle
ActiveUS20170015418A1The process is convenient and fastHighly configurableUnmanned aerial vehiclesRemote controlled aircraftModularityPosition sensor
A rotor-based remote flying vehicle platform includes a vehicle body. The vehicle body includes a processing unit that receives positional sensor data and provides flight controls based upon the received positional sensor data. The vehicle body also includes a first frame connection interface that is configured to interface with a plurality of different arm types. The first frame connection interface comprises a physical connection and an electronic connection. Additionally, the rotor-based remote flying vehicle platform includes a first arm, of a rotor-based remote flying vehicle platform, that is selectively connectable to the vehicle body through the first frame connection interface. The first arm comprises a first arm connection interface that is selectively connectable to the first frame connection interface. Additionally, the first arm comprises a first motor mounted to the first arm.
Owner:UAVPATENT CORP
Ventilated rotor mounting boom for personal aircraft
ActiveUS20180105268A1Easy maintenanceSafe and efficientPower plant cooling arrangmentsPower plant constructionJet aeroplaneAirplane
Described embodiments provide a rotor mounting boom assembly for a personal aircraft. The rotor mounting boom assembly includes a rotor mounting boom releasably attachable to a wing of the personal aircraft, one or more vertical lift rotors, and one or more rotor controller assemblies. Controller assemblies for each rotor are positioned on the rotor mounting booms such that downwash from the rotor causes increased airflow across the controller assembly to cool the controller assembly components. A rotor controller enclosure includes an air inlet and an air outlet to allow airflow through the enclosure to cool the controller components. The air inlet is positioned relative to the path of the rotor blades such that the downwash from the rotor that flows into the air inlet is maximized. The structure of the enclosure includes features for increasing the airflow through the enclosure.
Owner:WISK AERO LLC
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