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  • Higher-performance solid-rocket propellants and methods of utilizing them | TechLink
    are interested in learning more about this patent and related research and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 8465607 Status Active Categories Aerospace A method and a related material for utilizing high performance solid rocket propellants which are molding powders A propellant molding powder are selected to have a design burning rate and a tailored compaction profile A morphology of a center port of a rocket is selected for the design burn rate and a spin rate The molding powder is compacted isostatically around a core through application of triaxial pressure therein forming a solid rocket propellant charge with the selected center port shape The solid rocket propellant charge is placed in a cartridge or a case The cartridge is selected from various types of cartridges and specialty charges The solid rocket propellant molding powders are highly filled with metallic fuels and have a binder in the range of 4 to 18 which at least partially coats the surface of the molding powder USPTO url http patft uspto gov netacgi nph Parser patentnumber 8465607 Facebook Twitter Google Plus LinkedIn Main menu Home Licensing Joint R D Technology Summaries Patents

    Original URL path: http://techlinkcenter.org/patents/8465607 (2016-02-10)
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  • Deployable shell with wrapped gores | TechLink
    about this patent and related research and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 8462078 Status Active Categories Aerospace A reflector useful for communications radar and sensing application in space and on earth includes thin shell gores emanating from a geometric center of the reflector at its hub Gores are provided in a spiraled pattern and are in elastic connection to said hub and wrapped around their point of convergence at the hub when the reflector is stowed The gores emanate from the geometric center of the reflector hub at their elastic connection to the hub when they are deployed and operational as a reflector with a point of convergence to promote operation as a reflector Thin shell gores can have an inner perimeter and outer perimeter can be provided in a spiraled pattern and can be interlocked at their outer perimeter or in between their inner and outer perimeter while also remaining in elastic connection at their inner perimeter to said hub USPTO url http patft uspto gov netacgi nph Parser patentnumber 8462078 Facebook Twitter Google Plus LinkedIn Main menu Home Licensing Joint R D Technology Summaries Patents SBIR

    Original URL path: http://techlinkcenter.org/patents/8462078 (2016-02-10)
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  • High performance | TechLink
    and related research and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 8444082 Status Active Categories Aerospace An air vehicle can be folded into or unfolded from a compact tubular storage container without assembly or disassembly of the air vehicle The air vehicle includes a fuselage two aerodynamic surfaces rotatably mounted on the fuselage along a common axis with at least one pivot mechanism and at least one spring mechanism configured to deploy the aerodynamic surfaces so they extend outwardly from the body In a stowed configuration both aerodynamic surfaces are parallel to the fuselage for stowage of the aircraft in a container Each aerodynamic surface has a winglet located at an outer edge of the tail portion of the aerodynamic surface and a rudder on each winglet The aircraft does not require a vertical stabilizer or rudder system on the fuselage An outer backward swept wing portion can be unfolded from the outer edge of each aerodynamic surface to increase the wing aspect ratio USPTO url http patft uspto gov netacgi nph Parser patentnumber 8444082 Facebook Twitter Google Plus LinkedIn Main menu Home Licensing Joint R D Technology Summaries Patents

    Original URL path: http://techlinkcenter.org/patents/8444082 (2016-02-10)
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  • Method and apparatus for parafoil guidance that accounts for ground winds | TechLink
    method further includes determining a wind model with the higher altitude wind The wind model includes a linear or logarithmic increase in wind magnitude with increasing altitude beneath the higher altitude The method further includes determining locations of a flight path for a parafoil based on calculations that use the wind model The calculations are performed by an electronic control unit that is transported by the parafoil The method also

    Original URL path: http://techlinkcenter.org/patents/8437891 (2016-02-10)
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  • Helicopter weapon mounting system | TechLink
    mounting system illustratively includes a weapon cradle supporting a machine gun for pivoting movement about a generally horizontal elevational axis A carriage supports the weapon cradle and is supported by a pintle for rotation about a generally vertical azimuth axis An ejection collection device is supported by the carriage and collects spent shell casings and links ejected from the machine gun for discharge through the pintle A trigger assembly illustratively

    Original URL path: http://techlinkcenter.org/patents/8434397 (2016-02-10)
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  • Apparatus for adapting a rocket-assisted projectile for launch from a smooth bore tube | TechLink
    a smooth bore tube If you are interested in learning more about this patent and related research and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 8434394 Status Active Categories Aerospace An apparatus for adapting a rocket assisted artillery projectile of a first caliber for firing from a smooth bore tube of a second caliber may include an adapter for connecting to an aft end of the rocket assisted artillery projectile The adapter may include a main channel for receiving rocket exhaust a plurality of sub channels that lead from the main channel to an exterior of the adapter and an ignition channel that leads from the main channel to an ignition delay disposed in the adapter A tail boom may be fixed to an aft end of the adapter The tail boom may include an opening in a fore end that communicates with the ignition delay in the adapter Lifting surfaces such as fins may be attached to the tail boom USPTO url http patft uspto gov netacgi nph Parser patentnumber 8434394 Facebook Twitter Google Plus LinkedIn Main menu Home Licensing Joint R D Technology Summaries Patents SBIR About TechLink

    Original URL path: http://techlinkcenter.org/patents/8434394 (2016-02-10)
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  • Deployable structures with quadrilateral reticulations | TechLink
    hinges at the nodes to create an effective surface The deployed surface shape is determined by the strut lengths L and the node locations and the packaged compatibility constraint in which L1 L3 L2 L4 approximately equals zero Each of the compliant hinges have degrees of freedom such that the compact configuration of the support structure is obtained by the translation of two opposite nodes of each loop upwards and

    Original URL path: http://techlinkcenter.org/patents/8384613 (2016-02-10)
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  • Rakelet | TechLink
    Categories Aerospace A rakelet comprises a raked portion and a winglet portion that selectively integrate features of raked wingtips and winglets into a wingtip device that improves aircraft endurance and range over standard wings and over other wingtip devices such as raked wings winglets and the like The features of the rakelet can be configured to improve and maximize the range and endurance for any particular aircraft USPTO url http

    Original URL path: http://techlinkcenter.org/patents/8382041 (2016-02-10)
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