archive-org.com » ORG » T » TECHLINKCENTER.ORG

Total: 1016

Choose link from "Titles, links and description words view":

Or switch to "Titles and links view".
  • Airbag Projectile For Impeding Surface Vessel | TechLink
    Through the rapid inflation of the air bag the stability and orientation of the target surface vessel may be disturbed Disturbance at a minimum may reduce and change the trajectory of the surface vessel but in some circumstances the surface vessel may be overturned The air bag may be designed with an anti slip coating to directly couple to the wet hull of the surface vessel In some embodiments the

    Original URL path: http://techlinkcenter.org/patents/20140066236 (2016-02-10)
    Open archived version from archive


  • System And Method For Detecting The Amount Of Stabilizer Degradation In Solid Rocket Propellant | TechLink
    Rocket Propellant 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 20140022551 Categories Aerospace A spectrometric system including a solid rocket fuel an illuminating source including at least two wavelengths within a spectral range from 100 nm to 200 000 nm a first wavelength or range of wavelengths having a distinguishably greater or lesser absorbance for the stabilizer than for components of the propellant and a second wavelength or range of wavelengths having an absorbance for the stabilizer not distinguishably different than the absorbance for the components of the propellant an illuminating fiber to illuminate a surface of a solid rocket fuel a collecting fiber to collect back scattered reflected or transmitted light being given off from the surface of the solid rocket fuel and a spectrometer to determine the light intensities of the two wavelengths of the back scattered reflected or transmitted light collected USPTO url http appft1 uspto gov netacgi nph Parser Sect1 PTO1 Sect2 HITOFF d PG01 p 1 u Facebook Twitter Google Plus LinkedIn Main menu Home Licensing Joint R D Technology Summaries Patents

    Original URL path: http://techlinkcenter.org/patents/20140022551 (2016-02-10)
    Open archived version from archive

  • Tie Down And Jack Fitting Assembly For Helicopter | TechLink
    and related research and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 20140008494 Categories Aerospace The present invention is an assembly 100 for use as a jack contact point and a secure tie down location for a helicopter The assembly includes a hollow waffled dome element 110 having support elements 116A 116B 116C 116D 116E 116F which form attachment openings or securing holes 118A 118B 118C between the upper and lower rims of the dome element A jack securing mechanism 130 is provided with a threaded screw region 132 which connects to a jack mounting region 134 The threaded screw region extends through a hole 122 in a planar top 120 of the dome element 110 so as to be secured to a planar region of a structurally suitable location on the helicopter The jack mounting region is shaped to accommodate a jack used to raise the helicopter The attachment openings 118A 118B 118C are used to accommodate secure tie down of the helicopter USPTO url http appft1 uspto gov netacgi nph Parser Sect1 PTO1 Sect2 HITOFF d PG01 p 1 u Facebook Twitter Google Plus LinkedIn Main menu Home Licensing

    Original URL path: http://techlinkcenter.org/patents/20140008494 (2016-02-10)
    Open archived version from archive

  • Retention System For A Deployable Projectile Fin | TechLink
    of fin retention units and in which each unit is associated with one deployable fin of the projectile Each retention unit has an alignment device and a pair of span arms extending outwardly from opposite sides of the alignment device An attachment device attaches the free ends of the span arms of adjacent fin retention units together In doing so the alignment device engages and holds each fin in its

    Original URL path: http://techlinkcenter.org/patents/20140008483 (2016-02-10)
    Open archived version from archive

  • Extending boom for stabilizing projectiles launched from an apparatus | TechLink
    for launch from an apparatus is disclosed herein In some embodiments the projectile includes a body a boom having a first end extendable from the body and an armature coupled to the first end of the boom wherein the armature is configured to be moveable along and launchable from the apparatus and the armature is configured to be separable from the first end of the extended boom after launch from

    Original URL path: http://techlinkcenter.org/patents/8590453 (2016-02-10)
    Open archived version from archive

  • Real-time evaluation of change in thermal conductivity across an interface | TechLink
    Managers at http techlinkcenter org about staff Patent Identifier 8585283 Status Active Categories Aerospace A method of using Structural Health Monitoring SHM techniques for determining whether changes in thermal conductivity have occurred to a particular interface between two joined structural members is described which is particularly useful in satellites or other structures ordinarily subjected to vacuum pressure USPTO url http patft uspto gov netacgi nph Parser Sect1 PTO1 Sect2 HITOFF

    Original URL path: http://techlinkcenter.org/patents/8585283 (2016-02-10)
    Open archived version from archive

  • Rolling textile protective system for textile structural members | TechLink
    and licensing opportunities please contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 8584608 Status Active Categories Aerospace A rolling textile protective system for textile structural members includes n number of concentric sleeves having void spaces therebetween The n number of concentric sleeves are concentrically positioned about a common axis N number of concentric sleeves includes an inner sleeve a middle sleeve and an outer sleeve The outer sleeve is a polytetrafluoroethylene cloth layer A first fiberglass cloth layer is adjacent to the polytetrafluoroethylene cloth layer A polybenzimidazole cloth layer is adjacent to the fiberglass cloth layer A para aramid synthetic fibrous cloth layer is adjacent to the polybenzimidazole cloth layer A second fiberglass cloth layer is adjacent to the para aramid synthetic fibrous cloth layer The polytetrafluoroethylene cloth layer the first fiberglass cloth layer the polybenzimidazole cloth layer the para aramid synthetic fibrous cloth layer and the second fiberglass cloth layer are stitched together The n number of concentric sleeves are stitched together and to a textile structural member USPTO url http patft uspto gov netacgi nph Parser Sect1 PTO1 Sect2 HITOFF d PALL p 1 u Facebook Twitter Google Plus LinkedIn Main menu

    Original URL path: http://techlinkcenter.org/patents/8584608 (2016-02-10)
    Open archived version from archive

  • Guided projectile with motion restricting piezoelectric actuator | TechLink
    dimension along an axis A sensing element may be disposed in the internal volume The sensing element may have a dimension along the axis that is less than the dimension of the internal volume At least one piezoelectric actuator may be disposed in the housing adjacent the sensing element When the at least one piezoelectric actuator is activated it may prevent movement of the sensing element along the axis When

    Original URL path: http://techlinkcenter.org/patents/8573056 (2016-02-10)
    Open archived version from archive



  •