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  • Program to generate an aircrew display aid to assess JAM effectiveness | TechLink
    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 7847723 Status Active Categories Aerospace 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 The core of the invention is a software program that will dynamically provide the EA flight crew situational awareness regarding a threat emitter s coverage relative to the position of the EA aircraft and to the position of any number of protected entities PE The software program generates information to provide visual cues representing a Jam Acceptability Region JAR contour a Jam Assessment Strobe JAS and text for display on a number of flexibly configurable display formats posted on display units The JAR and JAS graphics and text will aid the EA aircrew in rapidly assessing the effectiveness of a given jamming approach USPTO url http patft uspto gov netacgi nph Parser patentnumber 7847723 Facebook Twitter Google Plus LinkedIn Main menu Home Licensing Joint R D Technology Summaries Patents SBIR About

    Original URL path: http://techlinkcenter.org/patents/7847723 (2016-02-10)
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  • Method and system for alerting aircrew to unsafe vibration levels | TechLink
    contact any of our Tech Managers at http techlinkcenter org about staff Patent Identifier 7839304 Status Active Categories Aerospace 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 USPTO url http patft uspto gov netacgi nph Parser patentnumber 7839304

    Original URL path: http://techlinkcenter.org/patents/7839304 (2016-02-10)
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  • Method and system for deployment of ordnance from an aircraft in mid-flight | TechLink
    an aircraft having a hatch that can be opened while the aircraft is in mid flight An air and pressure tight container stowed within the aircraft has a doorway that is sealed to and about the hatch from within the aircraft Mounted within the container is an expulsion system for expelling objects from the container through its doorway and the aircraft s hatch The container may be coupled and sealed

    Original URL path: http://techlinkcenter.org/patents/7735781 (2016-02-10)
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  • Folding articulating wing mechanism | TechLink
    tapered locking plunger urged by a coiled compression spring to contact a complementary mating surface formed on the wing assembly The spring urged locking plunger is released from a retracted position by rotation of the wing assembly from the folded position to the extended position A folding mechanism for rotating the wing assembly through a compound angle from the folded position to a rigid and positively locked fully extended position

    Original URL path: http://techlinkcenter.org/patents/7732741 (2016-02-10)
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  • Battery charging arrangement for unmanned aerial vehicle utilizing the electromagnetic field associated with utility power lines to generate power to inductively charge energy supplies | TechLink
    unmanned aerial vehicle UAV The present invention relates to a UAV that comprises an inductive charging device that utilizes the electromagnetic field emanated by overhead utility power lines to charge the energy supplies The UAV also includes a releasable latch for holding power lines to allow for the perching of the UAV on power lines during the charging process The latch and the inductive charging device may be provided on

    Original URL path: http://techlinkcenter.org/patents/7714536 (2016-02-10)
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  • Aerospace | TechLink
    below the midplane axis Read more about Asymmetrical control surface system for tube launched air vehicles Weapon mounting and remote position recognition system Patent Identifier 7185575 A system for remote tracking of a tactical missile assembly orientation during targeting and leading to launch from a platform including a weapon station frame rotatably attached to the platform and a command launch unit attached to the weapon station frame A launch tube assembly is pivotably attached thereon including a launch tube in which a tactical missile is positioned prior to launch Read more about Weapon mounting and remote position recognition system Apparatus for expelling a payload from a warhead Patent Identifier 7168368 Apparatus within a warhead for expelling a payload from the rear of the warhead after a tail assembly has been removed A separate thrust chamber within the warhead has an apertured thrust tube at one end which extends into the thrust chamber and a pusher plate at the other end for propelling the payload Read more about Apparatus for expelling a payload from a warhead Stackable in line surface missile launch system for a modular payload bay Patent Identifier 7159501 An underwater missile launch system includes one or more missile loading modules for supporting a plurality of missiles in a stackable in line configuration within a pressure vessel The missiles are arranged inside the modules which may be stacked in groups inside a single pressure vessel or payload bay Read more about Stackable in line surface missile launch system for a modular payload bay Finless training projectile with improved flight stability over an extended range Patent Identifier 7150234 A finless cone nosed ogival nosed or combination ogive cone nosed training projectile is statically stable yet has adequate spin rate to compensate for aerodynamic or mass asymmetries In addition the training projectile can be fired from smooth bore or rifled cannons of various calibers including 120 mm and 105 mm Read more about Finless training projectile with improved flight stability over an extended range Launch tube system having inflatable bladder shock isolation Patent Identifier 7128013 A launch tube system has two concentric sleeves An inner sleeve having holes formed therethrough defines a launch tube and an outer sleeve surrounds the inner sleeve and is spaced apart therefrom One or more flexible bladders are disposed between the inner outer sleeves Read more about Launch tube system having inflatable bladder shock isolation Aircraft excessive fuel dumping ejection parallel to flight direction Patent Identifier 7111809 Excessive fuel is dumped by ejection under a pressurized outflow velocity from an aircraft during flight as jets in a direction parallel to air stream flow relative to the aircraft from a rearwardly facing exit opening of a fuel jettison device mounted on the lower surface of the aircraft with the exit fixedly spaced below the lower aircraft surface a short distance to avoid the Coanda effect Read more about Aircraft excessive fuel dumping ejection parallel to flight direction Helicopter with torque correcting thruster device Patent Identifier 7077358 A

    Original URL path: http://techlinkcenter.org/patents/categories/aerospace?page=11 (2016-02-10)
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  • Common bus aircraft retrofit load control | TechLink
    energization arrangement especially suitable for an aircraft wherein original factory placed wiring can be reused in common bus form for plural new loads in order to avoid the expense and hazard of disassembling original wiring bundles for new conductor incorporation Serviceable wiring possibly earlier retired in place or becoming unneeded from equipment removal can by way of the invention be used for plural diverse new loads including loads of disparate operating cycle and current requirements for example even though energized via a common bus In the disclosed apparatus both energizing current and load control signals are transmitted via the same electrical bus between control location and load areas of the aircraft where control decoding and energy tap off occur the latter by switch mode power supply if needed Control signals of sinusoidal waveform minimal electromagnetic and radio frequency interference character and limited existing bus filtering attenuation are disclosed these may be embodied as the Frequency Shift Keying FSK or Continuous Tone Coded Squelch System CTCSS frequencies used in the radio communication art Loads of differing types are disclosed as examples in the described embodiment of the invention additional loads are feasible Use of the invention in land vehicles watercraft and

    Original URL path: http://techlinkcenter.org/patents/7701078 (2016-02-10)
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  • Convertible aerial vehicle with contra-rotating wing/rotors and twin tilting wing and propeller units | TechLink
    flight mode and a rotary wing flight mode The canard design micro aerial vehicle includes a fuselage two tiltable propellers and airfoils arranged at a forward portion of fuselage a pair of coaxial drive shafts positioned aft of the tiltable propeller and airfoil arranged for contra rotation a stop rotor mechanism and a pair of wing panels each of the wing panels attached to one of the coaxial drive shafts

    Original URL path: http://techlinkcenter.org/patents/7665688 (2016-02-10)
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