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Gieseke
Bruce Gieseke, San Jose, CA US
| Patent application number | Description | Published |
|---|---|---|
| 20120105129 | APPARATUS FOR MONOLITHIC POWER GATING ON AN INTEGRATED CIRCUIT - A power gating apparatus includes an integrated circuit package with a first voltage reference plane and a second voltage reference plane, and an integrated circuit that includes a circuit block, and a switch block. The first and second voltage reference planes may be electrically isolated from one another. The switch block may include a plurality of switches arranged in a ring surrounding the circuit block. The first voltage reference plane may be electrically coupled between an external voltage reference and the plurality of switches, and the second voltage reference plane may be electrically coupled between the plurality of switches and the circuit block. The second voltage reference plane may also distribute an electric current throughout the circuit block. In addition, each of the switches is configured to interrupt an electrical path between the first reference voltage plane and the circuit block in response to a control signal. | 05-03-2012 |
Eric James Gieseke, Lincoln, MA US
| Patent application number | Description | Published |
|---|---|---|
| 20110264666 | METHOD AND APPARATUS FOR INDEX GENERATION AND USE - An approach is provided for generating a searchable index including an associated object graph. Data objects of a database are converted into corresponding rows in a set of searchable columns. An object graph corresponding to each row of the searchable columns are determined. An index including the set of searchable columns and the corresponding object graphs are generated. | 10-27-2011 |
Gerald G. Gieseke, Selah, WA US
| Patent application number | Description | Published |
|---|---|---|
| 20080196259 | APPARATUS OF AND METHOD OF USE OF A RADIUS TABLE AND RADIAL TEMPLATE FOR FORMING MUNTIN BAR PATTERNS FOR MULTI-PANE WINDOW UNITS WITH OVERLAPPING SPOKES - An apparatus of a radius table with spokes which supports a glass pane. The glass pane centered by a centering system. The spokes having a measuring device which is urged into contact with the glass pane thereby allowing determination of the required length of a false hollow muntin bar for formation of a muntin bar pattern within a multi-pane window unit. The cut muntin bars placed proximal spokes. A radial template placed proximal the placed muntin bars to secure the muntin bars to the radial template by muntin clamps. The radial template with attached muntin bars removed from the radius table and transported for fabrication of a multi-pane window unit. | 08-21-2008 |
Steven S. Gieseke, Richfield, MN US
| Patent application number | Description | Published |
|---|---|---|
| 20100115897 | FILTER ELEMENTS; AIR CLEANER; ASSEMBLY; AND, METHODS - A filter cartridge, a safety element and fluid cleaner assembly are described. The fluid cleaner assembly generally includes a housing having a cover and a primary fluid cleaner section. The filter cartridge generally comprises z-filter media, arranged in a straight through configuration. Preferred cartridges include a seal gasket positioned to extend continuously around at outer perimeter of the straight through flow construction. The fluid cleaner assembly can have a precleaner positioned therein. Preferred features are described. Methods of assembly and use are also provided. | 05-13-2010 |
Thomas J. Gieseke, Newport, RI US
| Patent application number | Description | Published |
|---|---|---|
| 20090031873 | Explosive Water Jet with Precursor Bubble - A water jet assembly and method of use comprising a tank with cutting fluid, fuel and oxidizer lines, and a tank discharge lines. In operation, the tank is filled with oxidizer; the oxidizer line is closed and cutting fluid is supplied compressing the oxidizer. When the fluid reaches a level, the fluid line is closed and fuel is injected. A spark generator ignites the fuel/oxidizer mixture thereby raising the tank pressure. As the pressure rises, a low pressure valve simultaneously closes at a prescribed level. The vent line and a discharge to a nozzle are opened thereby, forming a gas bubble. When the bubble reaches a desired size and pressure drops below a level, the vent closes, allowing combustion expansion to force fluid through the nozzle to form a cutting jet. The bubble allows the jet to retain coherence between the nozzle and a cutting surface. | 02-05-2009 |
| 20110061554 | Acoustic Shotgun System - A high velocity acoustic signal producing underwater shotgun system for dispersing a plurality of relatively small supercavitating projectiles over a wide spatial field at long range using the dynamics of cavity collapse for better target localization in underwater mine clearance. A typical supercavitating projectile design is enhanced to produce a two-staged projectile in order to accomplish this innovation. The first stage of the two stage design allows for the long range firing underwater typical of a supercavitating projectile while the second stage permits the coverage of a wide area with a plurality of small supercavitating projectiles just as the first stage projectile reaches its fixed range. A distinctive feature of the radiated noise from a supercavitating projectile contacting a solid object is used in conjunction with the two stage projectile design to provide a system for underwater mine clearance verification. The distinctive noise signal may also be used in conjunction with an underwater targeting system to help identify, localize and track targets as well. | 03-17-2011 |
| 20110149691 | Supercavitating Projectile Tracking System and Method - A system for three-dimensional tracking of high speed undersea projectiles may utilize a distributed field of randomly positioned passive acoustic sensors. The system measures variables related to the pressure field generated by a supercavitating projectile in flight wherein the amplitude of the pressure generated at a point in space is related to the projectile dimensions, velocity, and trajectory. The system iteratively processes data from the sensors to measure launch velocity, flight direction (trajectory), ballistic coefficient (drag), and/or maximum range. | 06-23-2011 |