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John Jay
John Jay Groberman, Vancouver CA
| Patent application number | Description | Published |
|---|---|---|
| 20110085843 | Two handed vehicle wash apparatus. The invention is used for washing a variety of vehicles. The apparatus has water constantly flowing through it. Soap is also inserted directly into the said invention - It is a two handed apparatus used for washing vehicles. A bucket or water receptacle is no longer required. Constant flow of water, and the soap receptacle make it so you no longer need to pause while washing. Seeing that the water is flowing through a ΒΌ inch diameter tube; you use less water than the traditional method of washing a vehicle. Hands are kept dryer due to the waterproof nylon backing of the invention. | 04-14-2011 |
John Jay Streyel, Walker, MI US
| Patent application number | Description | Published |
|---|---|---|
| 20100321890 | Avionics Chassis - An avionics chassis comprises a housing having opposing walls, a pair of spaced card rails with one rail mounted to each of the opposing walls where each rail has a channel to define an effective slot having a predetermined height extending between the rails. The avionics chassis also includes a circuit card assembly comprising a printed circuit board and a thermal plane in overlying relationship with the printed circuit board, with the printed circuit board defining a first primary plane, and the thermal plane defining a second primary plane. The spatial relationship between the printed circuit board and the thermal plane is such that the first and second primary planes are located within the slot when the circuit card assembly is mounted to the card rail assembly and the thermal plane is conductively coupled to at least one of the rails to form a first conductive path from the thermal plane to at least one of the opposing walls and the printed circuit board is conductively coupled to at least one of the rails to form a second conductive path from the printed circuit board to at least one of the opposing walls. | 12-23-2010 |
John Jay Streyle, Walker, MI US
| Patent application number | Description | Published |
|---|---|---|
| 20100319948 | Avionics Chassis - An avionics chassis comprises a composite housing, a radio wave shield, and a lightning strike conductive path, wherein the radio wave shield attenuates electromagnetic interference entering and leaving the housing, and the lightning strike conductive path directs the current from a lightning strike away from an interior of the housing. | 12-23-2010 |
| 20100321891 | Avionics Chassis - An avionics chassis comprises a carbon fiber reinforced housing, a card rail for holding an electronic circuit board mounted to an interior surface of the housing, at least one heat-dissipating fin composed of carbon fiber and extending from the outer surface of the housing, a plurality of isotropic carbon fibers extending from an interior of the fin through the housing and in abutting contact with the card rail. The plurality of isotropic fibers form a direct conductive path from the card rail to the heat-dissipating fin. | 12-23-2010 |
| 20100321892 | Avionics Chassis - An avionics chassis comprises a housing having a substantially thermally non-conductive frame comprising a composite of carbon fibers laid up in an epoxy matrix. The housing also includes at least two walls, at least one of which is a thermally conductive wall comprising a composite of carbon fibers in a carbonized matrix, and a plurality of spaced, thermally-conductive, card rails provided on the at least two walls. The at least two walls are mounted to the frame in opposing relationship such that corresponding card rails on the walls define an effective slot therebetween in which a printed circuit board may be received and the card rails and the at least one thermally conductive wall form a thermally conductive path from the interior to the exterior. | 12-23-2010 |
John Jay Streyle, Grand Rapids, MI US
| Patent application number | Description | Published |
|---|---|---|
| 20120073788 | METHOD AND SYSTEM FOR SYNTHETIC JET COOLING - A method and system for cooling a component are provided. The synthetic jet cooling system includes a plurality of synthetic jet assemblies configured to be positioned adjacent to a component that generates excess heat. Each of the plurality of synthetic jet assemblies includes a driver configured to excite a respective one of the plurality of synthetic jet assemblies at a varying frequency. | 03-29-2012 |