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Fuat
Fuat Atabey, Saint Lambert CA
| Patent application number | Description | Published |
|---|---|---|
| 20110318123 | MULTIPLE ZONE COOLING APPARATUS - A cooling assembly for a machine tool including at least first and second nozzle rings mounted on the spindle housing, respectively defining first and second coolant conduits and respectively including first and second pluralities of nozzles in fluid communication with the respective conduit. Each first nozzle is oriented with an outlet thereof directed toward a first machining zone containing cutting edges of at last one tool having a first length. Each second nozzle is oriented with an outlet thereof directed toward a second machining zone different from the first machining zone and containing the cutting edges of at least one tool having a second length. | 12-29-2011 |
Fuat Bahadir, Omaha, NE US
| Patent application number | Description | Published |
|---|---|---|
| 20090129929 | Coaxial rotor system for helicopters - An improved coaxial rotor assembly for a helicopter includes an upper rotor system having a multiple of upper rotor blades each having outer tips and mounted on and extending outwards from a central rotor shaft and a lower rotor system having a multiple of lower rotor blades each having outer tips and mounted on and extending outwards from the central rotor shaft with the upper rotor system spaced an axial distance from the lower rotor system on the central rotor shaft. A rotor blade support ring extends circumferentially around each of the upper and lower rotor systems which movably engages and supports the outer tips of the upper and lower rotor blades in spaced apart relation such that the upper and lower rotor systems rotate in opposite directions and the rotor blade support ring means prevents contact between the upper and lower rotor systems during operation thereof. | 05-21-2009 |
| 20090189011 | Thrust Vectoring Exhaust Nozzle System for Helicopters - A thrust vectoring exhaust nozzle system for helicopters includes a vertical thrust vectoring nozzle positioned on the rear of the tail of the helicopter and a horizontal thrust vectoring nozzle positioned generally adjacent the vertical thrust vectoring nozzle, the vertical and horizontal thrust vectoring nozzles each connected to the exhaust output of the gas-turbine engine of the helicopter such that by adjusting and controlling the vertical and horizontal thrust vectoring nozzles to direct gas outflow in a selected direction, the exhaust outflow from the engine can be used to assist or modify the movement of the helicopter. | 07-30-2009 |
Fuat Bahadir, Panorama City, CA US
| Patent application number | Description | Published |
|---|---|---|
| 20110258624 | Virtual machine based secure operating system - Improved computer operating system which is impervious to attack by viruses, hackers and the like and which allow only the operating system to operate on the processor and which creates a virtual machine on which all application software is run. | 10-20-2011 |