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  • Apparatus for releasing a parachute from its payload | TechLink
    and related research and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 8025254 Status Active Categories Aerospace An apparatus for releasing a parachute from its payload upon ground impact by the payload The apparatus has a pair of sections releasably secured to each other Each section has an intermediate portion having a longitudinally extending axis and a spur receiving opening that extends through the intermediate portion and is transverse to the longitudinally extending axis a first end portion attached to the intermediate portion and comprising a spur that extends in a generally lateral direction with respect to the longitudinally extending axis and a second end portion attached to the intermediate portion such that the intermediate portion is between the first and second end portions Each section is configured so that a lanyard can be connected to the section wherein in order to use the apparatus a lanyard is attached to and between one section and a parachute and another lanyard is attached to and between the other section and a payload USPTO url http patft uspto gov netacgi nph Parser patentnumber 8025254 Facebook Twitter Google Plus LinkedIn Main menu Home Licensing

    Original URL path: http://techlinkcenter.org/patents/8025254 (2016-02-10)
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  • Solid fuel rocket thrust control | TechLink
    as a thrust control arrangement The electrical energy of the preheating is generated by electrical battery cells which are dispersed across the grain cross section and are triggered from an inert state into energy generation by burn face heat The preheating situs moves continually in response to movement of the grain burn face this is achieved through the use of high temperature electrical battery cell materials responding to the approach

    Original URL path: http://techlinkcenter.org/patents/8015920 (2016-02-10)
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  • Spacecraft docking interface mechanism | TechLink
    and related research and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 8006937 Status Active Categories Aerospace A demountable docking interface mechanism and method for docking and undocking two spacecraft utilizing the demountable docking interface mechanism USPTO url http patft uspto gov netacgi nph Parser patentnumber 8006937 Facebook Twitter Google Plus LinkedIn Main menu Home Licensing Joint R D Technology Summaries

    Original URL path: http://techlinkcenter.org/patents/8006937 (2016-02-10)
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  • Aircraft wing-pylon interface mounting apparatus | TechLink
    this patent and related research and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 7966921 Status Active Categories Aerospace An apparatus for interfacing an external store to an under wing pylon suspension rack on a tactical aircraft USPTO url http patft uspto gov netacgi nph Parser patentnumber 7966921 Facebook Twitter Google Plus LinkedIn Main menu Home Licensing Joint R D Technology

    Original URL path: http://techlinkcenter.org/patents/7966921 (2016-02-10)
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  • Deployable heirarchical structure | TechLink
    lattice assembly comprised of hinge boxes of 12 battens connected by hinge nodes The hinge nodes are made of a plurality of resilient flexure joints each joint connected to a batten and giving said batten a 90 degree in plane rotation capability with a neutral shaped flexure in a deployed state and a deformed shaped flexure in a compressed state whereby a restorative moment is created tending to return said flexure to its neutral state One or more trusses are formed by sets of four longerons connected to the hinge boxes by the resilient flexure joints Multiple hub boxes connected by longerons may be used to create a hierarchical truss of trusses in either two or three dimensions These assemblies may be collapsed to a linear dimension by shearing the hub boxes and trusses in a parallelogram manner The folding kinematics occur in three stages which may be performed either sequentially or simultaneously Initially the trusses connecting the hub boxes are sheared Then the hub boxes and trusses are sheared in one common dimension to reduce the assembly to a two dimensional planar configuration Finally the hub boxes and trusses are sheared in a perpendicular common dimension to reduce the

    Original URL path: http://techlinkcenter.org/patents/7941978 (2016-02-10)
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  • Adaptive material actuators for Coanda effect circulation control slots | TechLink
    introducing tangential control fluid flows along the surface of an aerodynamic member The fluid flows are directed toward a coanda surface disposed at the trailing edge of the aerodynamic member At least two injection slots are provided on opposite sides of the aerodynamic member to produce opposing forces Control of the flow of fluid from each slot determines the net effect of these opposing forces Smart material actuators are used

    Original URL path: http://techlinkcenter.org/patents/7861977 (2016-02-10)
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  • Modular missile launching assembly | TechLink
    a modular missile launching assembly more particularly a compact modular missile launching assembly that is easily attachable to smaller sized watercrafts allowing for quick installation The missile launching assembly is encased in a substantially rectangular container with a launching lid to which one or more missiles are attached A hydraulic lifting device within the substantially rectangular container is used to lift the launching lid from a closed or stowage position

    Original URL path: http://techlinkcenter.org/patents/7854189 (2016-02-10)
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  • Rifle launcher for small unmanned aerial vehicles (UAVs) | TechLink
    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 7849628 Status Active Categories Aerospace A launcher system and method for an unmanned aerial vehicle UAV wherein the launcher system comprises a barrel comprising a prepackaged internal pusher cup configured behind the UAV housed within the barrel an expansion chamber operatively connected around the barrel wherein the barrel extends out of a first end of the expansion chamber a muzzle adapter operatively connected to a second end of the expansion chamber wherein the first end of the expansion chamber is positioned opposite to the second end of the expansion chamber a rifle slip fitted to the muzzle adapter and a stand operatively connected to the expansion chamber wherein a triggering of the rifle causes the internal pusher cup to push the UAV out of the barrel at a predetermined launch velocity in order to attain a predetermined self propelled flight trajectory USPTO url http patft uspto gov netacgi nph Parser patentnumber 7849628 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/7849628 (2016-02-10)
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