Patents by Inventor John M. Vranish
John M. Vranish has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Publication number: 20140135954Abstract: A Balance-Assist Shoe system is described in which the shoes measure proximity and alignment to any surface prior to and after contact and force distribution during contact. The proximity and force sensing are first discussed in general terms as several sensing technologies apply. This is followed by a more detailed discussion where proximity and force sensing are performed by capacitance. An exercise system and a playback & analysis system, useful in using the Balance-Assist Shoes, are also described with attention to a situation awareness headset. The situation awareness headset, in turn, facilitates a PC media application which is useful, but unrelated to its original purpose.Type: ApplicationFiled: November 13, 2012Publication date: May 15, 2014Inventor: John M. Vranish
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Publication number: 20130337957Abstract: A Segmented Ground Gear Transmission (SGGT) is a two-stage epicyclical planetary transmission that converts input angular velocity and toque to a continuously variable output varying the effective diameter of ground stage ring gear. The ground stage ring gear is expanded and contracted in segments, half occupied by planets and half free. The segments occupied by planets transfer torque to ground, but do not move except in small angle twist for section curvature correction, while the free segments move in rotation to close the gaps between segments, but do not carry load. The ground stages of the two-stage planets displace to maintain correct mesh with and to correct curvature errors in the sections. The load-bearing segments and free segments exchange roles so the planets can rotate and orbit continuously for extended periods. Anti-friction rolling contacts are used throughout.Type: ApplicationFiled: June 19, 2012Publication date: December 19, 2013Inventor: John M. Vranish
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Publication number: 20120228991Abstract: A Tape Muscle is described where multiple tape loops are independently driven by synchronized grasp and pull actions from a tandem of Clamp, Clamp & Drive modules. Each tape loop is elastically bent, with its open ends threaded through individual passageways in both modules. Tape loops are nested inside each other with all tape open ends on the same side. Each loop moves its open ends in equal, opposite directions, while the loop position remains fixed. Tape movements do not interfere with each other. The open ends of each loop attach to a shared appendage, which is pulled back and forth using tensile forces. Drive and hold forces use small angle flexure bending mechanical advantage and high force density electrostatic induction methods. Tape speed results from high frequency clock speed and novel hand-off methods. Governing equations, design details and performance estimates are provided.Type: ApplicationFiled: February 6, 2012Publication date: September 13, 2012Inventor: John M. VRANISH
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Publication number: 20120126756Abstract: Charge-Driven Electrostatic Induction is a method for using modest voltage to induce large density electric charge across a large insulation gap. Large density equal and opposite charges are first created in a high performance capacitor adjacent said insulation gap. One charge is trapped on its electrode and the other charge is relocated further from the gap so the electric field from the trapped charge, with minimum interference, induces equal and opposite charge across the gap and stores large density electric energy in the insulation. With electrode area to gap ratio kept sufficiently large to limit field fringing, Charge-Driven Electrostatic Induction will rival electromagnetic motor performance. In practice it will be superior. Using layered, thin film components will eliminate permanent magnets, coils, ferromagnetic materials and large power current sources. The multi-step process will permit high operating speeds.Type: ApplicationFiled: October 13, 2011Publication date: May 24, 2012Inventor: John M. Vranish
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Publication number: 20120024633Abstract: Gyromotor is a type of action and reaction motor which generates thrust without plume ejection. Whereas rockets react equal and opposite to ejected mass momentum, Gyromotor cycles gyroscopes, each mounted on the end of a moment arm, in a back and forth rowing motion to drive a spacecraft, without external mass ejection analogous to rowing a boat. Gyroscope inertial properties are configured to provide maximum resistance torque during the drive stroke and reconfigured to provide minimum torque resistance during the return stroke. The gyroscopes are turned by a moment arm so the torque resistance provides a useful linear pseudo force component to drive the spacecraft, with said linear force greater during the drive stroke than the return stroke, analogous to an oar in water during the drive stroke and in air during the return stroke. The space craft moves in reaction to the net linear pseudo forces and momentum is conserved.Type: ApplicationFiled: July 19, 2011Publication date: February 2, 2012Inventor: John M. Vranish
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Patent number: 8016893Abstract: A gear bearing drive provides a compact mechanism that operates as an actuator providing torque and as a joint providing support. The drive includes a gear arrangement integrating an external rotor DC motor within a sun gear. Locking surfaces maintain the components of the drive in alignment and provide support for axial loads and moments. The gear bearing drive has a variety of applications, including as a joint in robotic arms and prosthetic limbs.Type: GrantFiled: June 21, 2007Date of Patent: September 13, 2011Assignees: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration, Northeastern UniversityInventors: Brian Weinberg, Constantinos Mavroidis, John M. Vranish
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Patent number: 7989992Abstract: A Linear Tape Motors sequentially bends flexures to precisely position a payload within a large, linear range. Movement is backlash free. Flexure bending is also used to drive large forces, using efficient mechanical advantage, anchor the Tape Motor against back-slipping and prevent sticking and jamming malfunctions. Existing permanent magnet motor drive technology can be easily adapted to energize and control the flexure bending motions. Combining flexures with rare earth permanent magnets, provides ultra compact Linear Tape Motors with very high power and force densities that hold position with power off. Their operating range can be is as long as required. Thus, Linear Tape Motors are attractive for space science instruments, where precision positioning in ultra cold operating conditions is required and where low mass and low power are premium.Type: GrantFiled: August 7, 2009Date of Patent: August 2, 2011Inventor: John M. Vranish
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Publication number: 20110032060Abstract: A Linear Tape Motors sequentially bends flexures to precisely position a payload within a large, linear range. Movement is backlash free. Flexure bending is also used to drive large forces, using efficient mechanical advantage, anchor the Tape Motor against back-slipping and prevent sticking and jamming malfunctions. Existing permanent magnet motor drive technology can be easily adapted to energize and control the flexure bending motions. Combining flexures with rare earth permanent magnets, provides ultra compact Linear Tape Motors with very high power and force densities that hold position with power off. Their operating range can be is as long as required. Thus, Linear Tape Motors are attractive for space science instruments, where precision positioning in ultra cold operating conditions is required and where low mass and low power are premium.Type: ApplicationFiled: August 7, 2009Publication date: February 10, 2011Inventor: John M. Vranish
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Patent number: 7762155Abstract: A partial gear bearing including an upper half, comprising peak partial teeth, and a lower, or bottom, half, comprising valley partial teeth. The upper half also has an integrated roller section between each of the peak partial teeth with a radius equal to the gear pitch radius of the radially outwardly extending peak partial teeth. Conversely, the lower half has an integrated roller section between each of the valley half teeth with a radius also equal to the gear pitch radius of the peak partial teeth. The valley partial teeth extend radially inwardly from its roller section. The peak and valley partial teeth are exactly out of phase with each other, as are the roller sections of the upper and lower halves. Essentially, the end roller bearing of the typical gear bearing has been integrated into the normal gear tooth pattern.Type: GrantFiled: May 25, 2006Date of Patent: July 27, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 7622907Abstract: The invention relates to a driven ground electrical circuit. A driven ground is a current-measuring ground termination to an electrical circuit with the current measured as a vector with amplification. The driven ground module may include an electric potential source VS driving an electric current through an impedance (load Z) to a driven ground. Voltage from the source VS excites the minus terminal of an operational amplifier inside the driven ground which, in turn, may react by generating an equal and opposite voltage to drive the net potential to approximately zero (effectively ground). A driven ground may also be a means of passing information via the current passing through one grounded circuit to another electronic circuit as input. It may ground one circuit, amplify the information carried in its current and pass this information on as input to the next circuit.Type: GrantFiled: September 27, 2006Date of Patent: November 24, 2009Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 7601091Abstract: A gearing system using modular gear bearing components. Each component is composed of a core, one or more modules attached to the core and two or more fastening modules rigidly attaching the modules to the core. The modules, which are attached to the core, may consist of gears, rollers or gear bearing components. The core orientation affects the orientation of the modules attached to the core. This is achieved via the keying arrangement of the core and the component modules that attach to the core. Such an arrangement will also facilitate the phase tuning of gear modules with respect to the core and other gear modules attached to the core.Type: GrantFiled: June 23, 2006Date of Patent: October 13, 2009Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 7544146Abstract: A gear bearing having a first gear and a second gear, each having a plurality of teeth. Each gear operates on two non-parallel surfaces of the opposing gear teeth to perform both gear and bearing functions simultaneously. The gears are moving at substantially the same speed at their contact points. The gears may be roller gear bearings or phase-shifted gear bearings, and may be arranged in a planet/sun system or used as a transmission. One preferred embodiment discloses and describes an anti-backlash feature to counter “dead zones” in the gear bearing movement.Type: GrantFiled: May 2, 2005Date of Patent: June 9, 2009Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 7513546Abstract: The present invention relates to a conformal gripping device. In an embodiment of the present invention a conformal gripper device may be disclosed comprising a frame that includes an array of movable pins. The device may also include a roller locking and unlocking system within the frame. The system may comprise a pair of locking rollers for each row of gripper pins to facilitate locking and unlocking the array of gripper pins on a column-by-column basis. The system may also include a striker element that may force the locking rollers to roll along an angled roll surface to facilitate unlocking of the array of pins on a column-by-column basis. The system may further include an electromagnetic actuator or solenoid and permanent magnets to facilitate movement of the striker element and the locking rollers.Type: GrantFiled: March 21, 2007Date of Patent: April 7, 2009Assignee: The United States of America as represented by the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 7504921Abstract: An actuator for moving a load has a frame forming a race between two surfaces thereof, at least two elements joined together by at least one flexible member, the elements and the at least one flexible member being disposed between the two surfaces of the frame that forms a race, one of the elements further joined to the load by a portion of the at least one flexible member, wherein when an element comes into contact with a surface of the frame it will stick thereto absent a repelling force, and moving means disposed to selectively attract or repel a corresponding element towards or away from one or the other of the two surfaces of the frame that forms the race. The actuator effects movement of the load in a direction towards or away from the elements, by changing a position of at least one of the elements on a surface of the frame that forms the race.Type: GrantFiled: September 29, 2006Date of Patent: March 17, 2009Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdminstrationInventor: John M. Vranish
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Publication number: 20080232946Abstract: The present invention relates to a conformal gripping device. In an embodiment of the present invention a conformal gripper device may be disclosed comprising a frame that includes an array of movable pins. The device may also include a roller locking and unlocking system within the frame. The system may comprise a pair of locking rollers for each row of gripper pins to facilitate locking and unlocking the array of gripper pins on a column-by-column basis. The system may also include a striker element that may force the locking rollers to roll along an angled roll surface to facilitate unlocking of the array of pins on a column-by-column basis. The system may further include an electromagnetic actuator or solenoid and permanent magnets to facilitate movement of the striker element and the locking rollers.Type: ApplicationFiled: March 21, 2007Publication date: September 25, 2008Applicants: SpaceInventor: John M. Vranish
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Publication number: 20080079520Abstract: An actuator for moving a load has a frame forming a race between two surfaces thereof, at least two elements joined together by at least one flexible member, the elements and the at least one flexible member being disposed between the two surfaces of the frame that forms a race, one of the elements further joined to the load by a portion of the at least one flexible member, wherein when an element comes into contact with a surface of the frame it will stick thereto absent a repelling force, and moving means disposed to selectively attract or repel a corresponding element towards or away from one or the other of the two surfaces of the frame that forms the race. The actuator effects movement of the load in a direction towards or away from the elements, by changing a position of at least one of the elements on a surface of the frame that forms the race.Type: ApplicationFiled: September 29, 2006Publication date: April 3, 2008Inventor: John M. Vranish
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Publication number: 20080074098Abstract: The invention relates to a driven ground electrical circuit. A driven ground is a current-measuring ground termination to an electrical circuit with the current measured as a vector with amplification. The driven ground module may include an electric potential source VS driving an electric current through an impedance (load Z) to a driven ground. Voltage from the source VS excites the minus terminal of an operational amplifier inside the driven ground which, in turn, may react by generating an equal and opposite voltage to drive the net potential to approximately zero (effectively ground). A driven ground may also be a means of passing information via the current passing through one grounded circuit to another electronic circuit as input. It may ground one circuit, amplify the information carried in its current and pass this information on as input to the next circuit.Type: ApplicationFiled: September 27, 2006Publication date: March 27, 2008Applicant: NASA HQ's.Inventor: John M. Vranish
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Publication number: 20080045375Abstract: A gearing system using modular gear bearing components. Each component is composed of a core, one or more modules attached to the core and two or more fastening modules rigidly attaching the modules to the core. The modules, which are attached to the core, may consist of gears, rollers or gear bearing components. The core orientation affects the orientation of the modules attached to the core. This is achieved via the keying arrangement of the core and the component modules that attach to the core. Such an arrangement will also facilitate the phase tuning of gear modules with respect to the core and other gear modules attached to the core.Type: ApplicationFiled: June 23, 2006Publication date: February 21, 2008Inventor: John M. Vranish
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Patent number: 7255483Abstract: A thrust roller bearing system comprising an inner rotating member, an outer rotating member and multiple rollers coupling the inner rotating member with outer rotating member. The inner and outer rotating members include thrust lips to enable the rollers to act as thrust rollers. The rollers contact inner and outer rotating members at bearing contact points along a contact line. Consequently, the radial/tilt and thrust forces move synchronously and simultaneously to create a bearing action with no slipping.Type: GrantFiled: June 18, 2002Date of Patent: August 14, 2007Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish
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Patent number: 7207245Abstract: A tool comprises a first handle and a second handle, each handle extending from a gripping end portion to a working end portion, the first handle having first screw threads disposed circumferentially about an inner portion of a first through-hole at the working end portion thereof, the second handle having second screw threads disposed circumferentially about an inner portion of a second through-hole at the working end portion thereof, the first and second respective through-holes being disposed concentrically about a common axis of the working end portions. First and second screw locks preferably are disposed concentrically with the first and second respective through-holes, the first screw lock having a plurality of locking/unlocking screw threads for engaging the first screw threads of the first handle, the second screw lock having a plurality of locking/unlocking screw threads for engaging the second screw threads of the second handle.Type: GrantFiled: June 30, 2005Date of Patent: April 24, 2007Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John M. Vranish