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  • Rocket loading and unloading tool | TechLink
    a launcher for the rocket so that the tool may be inserted into the tube to urge the rocket precisely into a loaded position without slipping from the nozzle and damaging elements inside the nozzle The tool is configured to receive a blast paddle of the launcher when the paddle is pivoted across the tube to engage a detent and an igniter contact with the rocket in the loaded position

    Original URL path: http://techlinkcenter.org/patents/7650827 (2016-02-10)
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  • Helicopter brown-out landing | TechLink
    obfuscation of the intended landing site and other landing threats are overcome Real time optical sourced data is collected early and used during helicopter approach to the intended landing site Upgrading of this data for use during dust cloud presence is accomplished with image processing techniques applied in response to such inputs as helicopter flight data Military use of the invention especially in current theatre conflict environments is contemplated Dust

    Original URL path: http://techlinkcenter.org/patents/7642929 (2016-02-10)
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  • Approaches to actively protect spacecraft from damage due to collisions with ions | TechLink
    Categories Aerospace A method whereby one or more conducting plates electrically biased negatively with respect to a spacecraft s electrical potential and insulated from the spacecraft surface are located around the spacecraft surface whereby contaminant ions in a plasma surrounding the spacecraft are attracted to and accelerated through the conducting plates electric potential caused to collide with the conductive surface neutralized through collisions with surface atoms and then reflected away

    Original URL path: http://techlinkcenter.org/patents/7637461 (2016-02-10)
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  • Force balancing actuator | TechLink
    force balancing actuator for mounting a pressure vessel containing an engine to aircraft structure The force balancing actuator includes a cylinder and piston that is mechanically connected between the pressure vessel and aircraft structure This piston and cylinder adjustably provides force there between in response to variations in differential pressure between the pressurized cabin and ambient pressure The cylinder and piston thereby relieves excessive load on engine isolators allowing the

    Original URL path: http://techlinkcenter.org/patents/7618007 (2016-02-10)
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  • Tape-spring deployable boom | TechLink
    three or more longitudinal prismatic tape spring members longerons and non prismatic tape spring members battens that are connected transversely to the longerons The longerons can be reconfigured in a z folding manner to compact the structure The batten members have a twist at each end of the same magnitude and sense such that when connected to the longerons the concave surfaces of the battens substantially face along the longitudinal

    Original URL path: http://techlinkcenter.org/patents/7617639 (2016-02-10)
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  • Supersonic turning vane | TechLink
    fan that projects into the supersonic flow passage to turn supersonic flow into the turning vane the pressure side comprising a large radius curved surface the pressure side and the suction side converging to form a throat wherein a shock is formed upstream of the throat the shock decelerating the supersonic flow to subsonic conditions and the pressure side turning the subsonic flow the suction side including an outer nozzle

    Original URL path: http://techlinkcenter.org/patents/7581482 (2016-02-10)
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  • Capsule for releasably retaining a missile | TechLink
    this patent and related research and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 7581481 Status Active Categories Aerospace A capsule adapted for disposition in a submarine launch tube for retaining the missile until launch thereof The capsule includes a cylindrically shaped housing including a plurality of layers of glass fibers and layers of graphite the layers including an outer layer of glass fibers defining an outer skin of the housing and an inner layer of glass fibers A titanium flange is fixed on the housing and in contact with the layers of graphite An adhesive layer is disposed on the outer skin and an interface support pad is mounted on the outer skin and retained thereon by the adhesive layer A layer of metal foil is disposed inboard of the adhesive layer and between the outer layer of glass fibers and the inner layer of glass fibers to serve as a barrier to products of galvanic reaction occurring between the graphite layers and the titanium flange USPTO url http patft uspto gov netacgi nph Parser patentnumber 7581481 Facebook Twitter Google Plus LinkedIn Main menu Home Licensing Joint R D Technology

    Original URL path: http://techlinkcenter.org/patents/7581481 (2016-02-10)
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  • Reefing apparatus for controlling the inflation of a gliding wing parachute | TechLink
    four outer corners The reefing mechanism includes a primary reefing loop with four supplemental reefing loops movably secured thereto by loops and connected through mounting rings to the four corners of the canopy to retain it in a general cloverleaf shape during initial stages of deployment and responsive to cutting of the primary reefing loop for release thereof for allowing full deployment or deployment into another reefed stage of the

    Original URL path: http://techlinkcenter.org/patents/7578480 (2016-02-10)
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