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  • Aerospace | TechLink
    unmanned surface vehicle to provide lift and control in water at sufficient speed A superstructure trimaran hull serves as a stable operation platform during low speed maneuvers or at rest Read more about Hydroplaning unmanned surface vehicle Ramp blanket Patent Identifier H2117 Vari ramp blankets holding X ray file 143 by 173 in dimensions in pockets on top of the vari ramp inlets on an F 15 aircraft have been used by us for the detection of foreign objects i e washers bolts safety wire These blankets ensure inspection consistency each and every time the aircraft is X rayed when it is grounded after flight or is in phase Read more about Ramp blanket Integrated fan core twin spool counter rotating turbofan gas turbine engine Patent Identifier H2032 A twin spool counter rotating turbofan gas turbine engine having a counter rotating fan module integrated with the high pressure compressor and driven by a counter rotating turbine utilizing only two drive shafts The two drive shafts are aerodynamically coupled and rotate in opposite directions relative to each other with or without the use of a gearbox Read more about Integrated fan core twin spool counter rotating turbofan gas turbine engine Apparatus and method of concomitant scenario topography with the aid of a digital computer Patent Identifier H1997 A system for concomitant scenario topography with the aid of a digital computer such that a two dimensional or three dimensional map is produced and displayed which illustrates the combined effects particularly geo environmental of multiple diverse criteria and factors relative to uniquely referenced uniform small areas of a plane surface or the surface of a solid Read more about Apparatus and method of concomitant scenario topography with the aid of a digital computer Vapor deposition of a thin polymer film on solid propellant rocket grain surface Patent Identifier H1824 The maximum performance of future missiles is limited by booster rocket and overall system constraints such as the ignition mass flow rise rate This rate is typically controlled by an inhibitor on the surface of a solid propellant rocket grain Read more about Vapor deposition of a thin polymer film on solid propellant rocket grain surface Oxidizing agent Patent Identifier H1768 There is a need for liquid oxidizers which are safer and which have better handling and toxicity characteristics The liquid oxidizers should also have low freezing points high thermal stability and high performance as oxidizers Typically for propulsion Read more about Oxidizing agent Hydraulic circuit leak detector and shut off mechanism Patent Identifier H1761 A leak detector and shut off apparatus shuts off hydraulic fluid downstream o prevent the hazards attendant hydraulic failure such as loss of fluid and fire A first sensor is coupled to a supply line for hydraulic fluid to produce pressure differential force F s which is representative of the flow of hydraulic fluid Read more about Hydraulic circuit leak detector and shut off mechanism Simulator Patent Identifier H1728 A flight simulator displays control choices on an out the

    Original URL path: http://techlinkcenter.org/patents/categories/aerospace?page=5 (2016-02-09)
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  • Aerospace | TechLink
    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 Read more about Helicopter weapon mounting system Apparatus for adapting a rocket assisted projectile for launch from a smooth bore tube Patent Identifier 8434394 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 Read more about Apparatus for adapting a rocket assisted projectile for launch from a smooth bore tube Extendable fins for a tube launched projectile Patent Identifier 8415598 A stabilizing fin deployment apparatus may include a base assembly for attachment to the rear end of a projectile The base assembly may include a base a spacer a fin mount a gas cavity and an opening that extends from the rear end of the base to the gas cavity A retention nut may engage the base and secure the fin mount and spacer to the base Read more about Extendable fins for a tube launched projectile Deployable structures with quadrilateral reticulations Patent Identifier 8384613 A non planar surface support structure that is compatible with deployable thin shell reflector segments The structure is composed of multiple four strut closed loops connected to compliant hinges at the nodes to create an effective surface Read more about Deployable structures with quadrilateral reticulations Rakelet Patent Identifier 8382041 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 Read more about Rakelet Stackable easily packaged and aerodynamically stable flechette Patent Identifier 8375860 A flechette has a forward section or body 12 containing its center of gravity A quill 10 is connected to the forward section and is integrally connected to a pair of fins 15A 15B each having a longitudinal angle and a radial angle When the two fins are viewed from the aft of the flechette the pair of fins demonstrate an S shaped orientation Read more about Stackable easily packaged and aerodynamically stable flechette Hand launchable unmanned aerial vehicle Patent Identifier 8366054 An unmanned aerial vehicle including a controller operating in a search mode of operation where a receiver of an acquisition sensor searches for a target and causes flight control surfaces to guide the vehicle in a downward spiral path a terminal mode of operation where the acquisition sensor detects a target and causes flight control surfaces to direct the vehicle toward the target and an ac Read more about Hand launchable unmanned aerial vehicle Structure for storing and unfurling a flexible material Patent Identifier 8356774 Flexible and resilient masts are connected by flexible and resilient inner and outer spars and flexible cords radially connect the spars A

    Original URL path: http://techlinkcenter.org/patents/categories/aerospace?page=6 (2016-02-09)
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  • Aerospace | TechLink
    control Spacecraft docking interface mechanism Patent Identifier 8006937 A demountable docking interface mechanism and method for docking and undocking two spacecraft utilizing the demountable docking interface mechanism Read more about Spacecraft docking interface mechanism Aircraft wing pylon interface mounting apparatus Patent Identifier 7966921 An apparatus for interfacing an external store to an under wing pylon suspension rack on a tactical aircraft Read more about Aircraft wing pylon interface mounting apparatus Deployable heirarchical structure Patent Identifier 7941978 A collapsible and deployable hierarchical open lattice assembly comprised of hinge boxes of 12 battens connected by hinge nodes Read more about Deployable heirarchical structure Adaptive material actuators for Coanda effect circulation control slots Patent Identifier 7861977 A system and method of use are provided for 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 Read more about Adaptive material actuators for Coanda effect circulation control slots Modular missile launching assembly Patent Identifier 7854189 The invention is related to 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 Read more about Modular missile launching assembly Rifle launcher for small unmanned aerial vehicles UAVs Patent Identifier 7849628 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 e Read more about Rifle launcher for small unmanned aerial vehicles UAVs Program to generate an aircrew display aid to assess JAM effectiveness Patent Identifier 7847723 The invention generally relates to the field of computer software particularly to an improved method of providing aircrew decision aids for use in determining the optimum placement of an Electronic Attack EA aircraft Read more about Program to generate an aircrew display aid to assess JAM effectiveness Method and system for alerting aircrew to unsafe vibration levels Patent Identifier 7839304 An onboard system for a rotary wing aircraft detects a limit cycle oscillation in the tail mast and provides a timely indication of the limit cycle oscillation to an aircrew before serious damage to the airframe is likely to occur Read more about Method and system for alerting aircrew to unsafe vibration levels Method and system for deployment of ordnance from an aircraft in mid flight Patent Identifier 7735781 A system for in air deployment of objects utilizes an aircraft having a hatch that can be opened while the aircraft is in mid

    Original URL path: http://techlinkcenter.org/patents/categories/aerospace?page=7 (2016-02-09)
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  • Aerospace | TechLink
    landing Approaches to actively protect spacecraft from damage due to collisions with ions Patent Identifier 7637461 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 conductiv Read more about Approaches to actively protect spacecraft from damage due to collisions with ions Force balancing actuator Patent Identifier 7618007 There is provided a 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 Read more about Force balancing actuator Tape spring deployable boom Patent Identifier 7617639 A self deployable monolithic open lattice frame structure of resilient tape spring members The structure is comprised of 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 Read more about Tape spring deployable boom Supersonic turning vane Patent Identifier 7581482 A supersonic turning vane includes a suction side and a pressure side the suction side including an expansion turning wall wherein the expansion turning wall creates an expansion 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 Read more about Supersonic turning vane Capsule for releasably retaining a missile Patent Identifier 7581481 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 Read more about Capsule for releasably retaining a missile Reefing apparatus for controlling the inflation of a gliding wing parachute Patent Identifier 7578480 A reefing apparatus for controlling inflation of a gliding wing parachute which has a generally rectangular or trapezoidal canopy with four outer corners Read more about Reefing apparatus for controlling the inflation of a gliding wing parachute Base bleed boat tail converter for projectile Patent Identifier 7578238 A projectile may be used in a boat tail or base bleed configuration Read more about Base bleed boat tail converter for projectile Aerodynamically stable finless projectile Patent Identifier 7568433 A finless projectile provides improved ease of use aerodynamics muzzle velocity drag target and excursion accuracy structural integrity terminal effectiveness and safety at lower cost The finless projectile includes a slug a forward projectile body an aft projectile body an obturator and a pad Read more about Aerodynamically stable finless

    Original URL path: http://techlinkcenter.org/patents/categories/aerospace?page=8 (2016-02-09)
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  • Aerospace | TechLink
    more about Mechanical Acoustic Noise Generator System for Scramjet Engine Method and system for alerting aircrew to unsafe vibration levels Patent Identifier 20090273488 An onboard system for a rotary wing aircraft detects a limit cycle oscillation in the tail mast and provides a timely indication of the limit cycle oscillation to an aircrew before serious damage to the airframe is likely to occur Read more about Method and system for

    Original URL path: http://techlinkcenter.org/patents/categories/aerospace?page=29 (2016-02-09)
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  • Electroactive Polymer Based Supercapacitors Including A Cathode Having Bbl Or Pyr-Bbl | TechLink
    including mixing Pyr BBL and a room temperature molten salt from a range of about 35 65 weight ratio dissolving the mixture in about 1 methanesulfonic acid to produce a Pyr BBL solution drop casting the solution onto glass or gold coated glass at 140 C in air and heating for about 2 hours to produce films drying the films in a vacuum oven at about 100 C for at

    Original URL path: http://techlinkcenter.org/patents/9068043 (2016-02-09)
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  • Method For The Formation Of Pbse Nanowires In Non-Coordinating Solvent | TechLink
    Identifier 9067787 Status Active Categories Electronics This disclosure concerns a method of making nanowires in a single flask and in non coordinating solvent involving the reaction of PbO with oleic acid to produce Pb oleate heating the Pb oleate to a preferred temperature with additional coordinating ligands injecting a solution of Se to produce a second solution heating the second solution and maintaining the temperature resulting in nucleation and growth

    Original URL path: http://techlinkcenter.org/patents/9067787 (2016-02-09)
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  • Sheath Flow Device And Method | TechLink
    and bottom surfaces situated so as to transport the sheath fluid laterally across the channel to provide sheath fluid fully surrounding the core solution At the point of introduction into the channel the sheath fluid and core solutions flow side by side within the channel or the core solution may be bounded on either side by the sheath fluid The system is functional over a broad channel size range and

    Original URL path: http://techlinkcenter.org/patents/9067204 (2016-02-09)
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