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Anil B.
Anil B. Lingambudi, Bangalore IN
| Patent application number | Description | Published |
|---|---|---|
| 20110290524 | Cable For High Speed Data Communications - A cable for high speed data communications that includes a first inner conductor enclosed by a first dielectric layer and a second inner conductor enclosed by a second dielectric layer, the inner conductors and the dielectric layers disposed within the cable in parallel with a longitudinal axis of the cable; drain conductors disposed within the cable laterally to the inner conductors adjacent to the dielectric layers along the longitudinal axis of the cable and within thirty degrees of a horizontal axis through the inner conductors; and a conductive shield composed of a strip of conductive shield material wrapped in a rotational direction along and about the longitudinal axis around the inner conductors, the dielectric layers, and the drain conductors, including overlapped wraps of the conductive shield material along the longitudinal axis. | 12-01-2011 |
Anil B. Mertol, Bremen DE
| Patent application number | Description | Published |
|---|---|---|
| 20100001131 | Method of and Apparatus for Producing Aerodynamic Resistance on an Aircraft - The invention concerns an apparatus for and a method of producing aerodynamic resistance on an aircraft, comprising at least one braking flap, wherein the at least one braking flap can be extended into the airflow around the aircraft. In accordance with the invention at least one braking flap is arranged on the fuselage of the aircraft in a region over the wings of the aircraft. | 01-07-2010 |
Anil B. Patel, La Crescenta, CA US
| Patent application number | Description | Published |
|---|---|---|
| 20110024658 | Livewell Fill Valve - Embodiments of the invention provide a fill valve for use in a livewell of a boat. The fill valve includes an intake and a valve housing coupled to the intake. The valve housing includes a rounded half-sphere shaped front wall coupled to a substantially flat back wall. The front wall includes one or more inlet openings in fluid communication with the intake. The fill valve also includes a valve switch positioned in the valve housing to switch between a first position allowing fluid communication between the inlet openings and the intake and a second position providing a substantially liquid-tight seal between the inlet openings and the intake. | 02-03-2011 |
Anil B. Rajanna, Karnataka State IN
| Patent application number | Description | Published |
|---|---|---|
| 20080260535 | BLADE/DISK DOVETAIL BACKCUT FOR BLADE/DISK STRESS REDUCTION (6FA+E, STAGE2) - Blade load path on a gas turbine disk can be diverted to provide a significant disk fatigue life benefit. A plurality of gas turbine blades are attachable to a gas turbine disk, where each of the gas turbine blades includes a blade dovetail engageable in a correspondingly-shaped dovetail slot in the gas turbine disk. In order to reduce gas turbine disk stress, an optimal material removal area is defined according to blade and/or disk geometry to maximize a balance between stress reduction on the gas turbine disk, a useful life of the gas turbine blade, and maintaining or improving the aeromechanical behavior of the gas turbine blade. Removing material from the material removal area effects the maximized balance. | 10-23-2008 |