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Bryan G.
Bryan G. Leonards, Sr., Crowley, LA US
| Patent application number | Description | Published |
|---|---|---|
| 20100011650 | Waterfowl decoy with retractable anchor and anchor line - A novel waterfowl decoy has a retractable anchor and accompanying anchor line. In one embodiment of the invention, an anchor line passes through a substantially hollow keel mounted at or near the base of the decoy. The line can be selectively locked in either a retracted (anchor stored) or extended (anchor deployed) position, as desired. When the anchor line is retracted, the anchor weight can be secured to the decoy keel or decoy body for convenient storage. In an alternative embodiment, the waterfowl decoy has a rotating head that can spin about an axis passing through the neck of the decoy. When the anchor is deployed, the anchor line extends from the bottom of the decoy, keel or other lower portion of said decoy. Conversely, when the anchor is not deployed, a portion of the anchor line can be spooled or wound around the neck of the decoy to remove excess slack from the anchor line. | 01-21-2010 |
Bryan G. Moosman, San Marcos, CA US
| Patent application number | Description | Published |
|---|---|---|
| 20100142582 | GAS DISCHARGE LASER CHAMBER - One aspect of the disclosed subject matter describes a gas discharge laser chamber. The gas discharge laser chamber includes a discharge region formed between a first electrode and a second electrode, a tangential fan for circulating gas through the discharge region, wherein the fan is proximate to an input side of the discharge region, an input side acoustic baffle proximate to the input side of the discharge region. The input side acoustic baffle includes a vanishing point leading edge, a vanishing point trailing edge, a gas flow smoothing offset surface aligning a gas flow from a surface of the input side acoustic baffle to an input side of a cathode support in the discharge region, a plurality of ridges separated by a plurality of trenches, wherein the plurality of ridges and the plurality of trenches are aligned with a direction of gas flow through the discharge region and wherein the plurality of ridges have a random pitch between about 0.3 and about 0.7 inch. | 06-10-2010 |
Bryan G. Parrette, Vernon, CT US
| Patent application number | Description | Published |
|---|---|---|
| 20090255307 | Turbine blade twist angle correction tooling - A tool for correcting the twist angle of a turbine blade includes an adaptor configured to engage a tip of the blade, a socket drive configured to engage the adaptor, a first handle connected to a first side of the socket drive, a second handle connected to a second side of the socket drive, and a torque gauge configured to measure a load applied to the blade. | 10-15-2009 |