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Jacob D.
Jacob D. Edick, Minneapolis, MN US
| Patent application number | Description | Published |
|---|---|---|
| 20110238151 | SURFACE TREATED BIOERODIBLE METAL ENDOPROSTHESES - An endoprosthesis includes an expandable tubular body defined by a plurality of struts. In some embodiments, the expandable tubular body includes a bioerodible metal that has at least a first surface region and a second surface region. The first and second surface regions can have different surface oxide compositions. In some embodiments, the first portion has a thermally altered microstructure and the second portion has a wrought microstructure. The thermally altered microstructure can be a cast microstructure comprising dendritic grains. The first portion forms at least a portion of an outer surface of the expandable tubular body. In some embodiments, the expandable tubular body includes iron or a bioerodible iron alloy and at least one surface of the expandable tubular body includes a substantially uniform coating of iron(III) oxide. | 09-29-2011 |
Jacob D. Feala, Washington, DC US
| Patent application number | Description | Published |
|---|---|---|
| 20120015834 | METHODS FOR ARTIFICIAL COMBINATORIAL CONTROL OF BIOLOGICAL SYSTEMS - Methods and systems for determining a set of control molecules for use in a combinatorial approach for the treatment of medical conditions, including providing one or more sets of control molecules, where each control molecule within the set acts on a set of targets and the number of control molecules within the one or more sets of control molecules is fewer than the number of targets within the sets of targets; and searching within the sets of control molecules to identify a subset of control molecules that together with a subset of targets form an artificial system to produce a biological effect through the modulation of the subset of targets. | 01-19-2012 |
Jacob D. Viring, Woodinville, WA US
| Patent application number | Description | Published |
|---|---|---|
| 20100119343 | Aircraft Landing Gear Loader - An apparatus for loading and unloading a main landing gear (“MLG”) of an aircraft includes a fixture that is adapted to couple to a truck of the MLG such that a sagittal plane of the fixture is parallel to or coplanar with a sagittal plane of the MLG and both translational forces and turning moments applied to the fixture are coupled directly through the fixture to the MLG, a mechanism for controllably translating the fixture in the sagittal plane thereof, and a mechanism for controllably rotating the fixture in the sagittal plane thereof. | 05-13-2010 |
