Abstract: A method to manufacture reticulated metal foam via a dual investment, includes pre-investment of a precursor with a diluted pre-investment ceramic plaster then applying an outer mold to the encapsulated precursor as a shell-mold.

Abstract: The invention described herein provides compositions and methods for treating or preventing Helicobacter pylori infection.

Abstract: A method to manufacture reticulated metal foam via a dual investment, includes pre-investment of a precursor with a diluted pre-investment ceramic plaster then applying an outer mold to the encapsulated precursor as a shell-mold.

Abstract: A method to manufacture reticulated metal foam via a dual investment, includes pre-investment of a precursor with a diluted pre-investment ceramic plaster then applying an outer mold to the encapsulated precursor as a shell-mold.

Abstract: A method to manufacture reticulated metal foam via a dual investment, includes pre-investment of a precursor with a diluted pre-investment ceramic plaster then applying an outer mold to the encapsulated precursor as a shell-mold.

Abstract: The present invention relates to an ink tank for an ink jet printer. The invention further relates to a method of manufacturing the ink tank, as well as well as a method of refilling the ink tank. The ink tank includes an ink tank body and an ink tank lid bonded to the ink tank body at a bond joint. The ink tank lid comprises an opening that leads to a holding area that is adapted to contain a capillary media therein. The holding area comprises a wall that forms a boundary between the capillary media and an enclosure defined by the ink tank body and the ink tank lid. The opening is sized to permit an insertion and removal of the capillary media to and from the holding area when the ink tank lid is bonded to the ink tank body at the bond joint.

Abstract: The present invention relates to an ink tank for an ink jet printer. The invention further relates to a method of manufacturing the ink tank, as well as well as a method of refilling the ink tank. The ink tank includes an ink tank body and an ink tank lid bonded to the ink tank body at a bond joint. The ink tank lid comprises an opening that leads to a holding area that is adapted to contain a capillary media therein. The holding area comprises a wall that forms a boundary between the capillary media and an enclosure defined by the ink tank body and the ink tank lid. The opening is sized to permit an insertion and removal of the capillary media to and from the holding area when the ink tank lid is bonded to the ink tank body at the bond joint.

Abstract: The present invention relates to an ink tank for an ink jet printer. The invention further relates to a method of manufacturing the ink tank, as well as well as a method of refilling the ink tank. The ink tank includes an ink tank body and an ink tank lid bonded to the ink tank body at a bond joint. The ink tank lid comprises an opening that leads to a holding area that is adapted to contain a capillary media therein. The holding area comprises a wall that forms a boundary between the capillary media and an enclosure defined by the ink tank body and the ink tank lid. The opening is sized to permit an insertion and removal of the capillary media to and from the holding area when the ink tank lid is bonded to the ink tank body at the bond joint.

Abstract: A valve includes a stem, a cap, and a deformable lip. The stem includes a first sealing portion and has a longitudinal axis. The cap is connected to the stem and includes a passageway. The deformable lip extends from a periphery of the cap and includes a second sealing portion. The stem is displaceable relative to the deformable lip along the longitudinal axis of the stem to open the first sealing portion and close the second sealing portion to allow fluid to move through the passageway in the cap.

Abstract: A system, method and program product for evaluating workflows includes formulating a list of categories for workforce projects to be evaluated. A list is then formulated of questions for each category. Ranges are set up and then applied to the categories. Base line days, a multiplier, and a weight are assigned to each range. A number of assets is assigned for the workflow being evaluated. A derived value is assigned to each range; and a range to each category pending evaluation is input. These standardized evaluation criteria are thus established for evaluating workflows.

Abstract: A system for removing particles from a slurry tank includes a filtering device and a controller. The filtering device collects and removes particles deposited within the slurry tank and the controller controls the placement and movement of the filtering device with respect to the slurry tank.

Abstract: The present invention relates to an ink tank for an ink jet printer. The invention further relates to a method of manufacturing the ink tank, as well as well as a method of refilling the ink tank. The ink tank includes an ink tank body and an ink tank lid bonded to the ink tank body at a bond joint. The ink tank lid comprises an opening that leads to a holding area that is adapted to contain a capillary media therein. The holding area comprises a wall that forms a boundary between the capillary media and an enclosure defined by the ink tank body and the ink tank lid. The opening is sized to permit an insertion and removal of the capillary media to and from the holding area when the ink tank lid is bonded to the ink tank body at the bond joint.

Abstract: A method of insuring against launch failure is provided to reduce the business risk to the satellite owner and insurance underwriters against satellite launch failure. The launch insurance includes provision for guaranteeing a rapid response recovery mission, preferably at no cost, in the event that a satellite suffers a boost failure during launch resulting in a fully-functional satellite being launched to an unintended inoperable orbit. Preferably, the launch insurance also provides for additional insurance against failure of the recovery mission to provide compensation to the satellite owner in the event that the recovery mission is also unsuccessful.

Abstract: A valve includes a stem, a cap, and a deformable lip. The stem includes a first sealing portion and has a longitudinal axis. The cap is connected to the stem and includes a passageway. The deformable lip extends from a periphery of the cap and includes a second sealing portion. The stem is displaceable relative to the deformable lip along the longitudinal axis of the stem to open the first sealing portion and close the second sealing portion to allow fluid to move through the passageway in the cap.

Abstract: A system for removing particles from a slurry tank includes a filtering device and a controller. The filtering device collects and removes particles deposited within the slurry tank and the controller controls the placement and movement of the filtering device with respect to the slurry tank.

Abstract: Inhibitors of the alpha carbonic anhydrase inhibitors are administered to treat H. pylori infection in the mammalian, including human, stomach. The inhibitors are administered to mammals, including humans, in an amount that results in 4×10−4 to 4×10−9 Molar concentration of the drug in the stomach because this concentration range is lethal to the H. pylori bacteria.

Abstract: An image display device comprising a body including a display for displaying digital images and a cover member attached to the body. The cover member is rotatable between three positions including a first position wherein the cover member is spaced from the display, second position wherein the cover member is disposed proximate the display, and a third position different than the first position wherein the display device is supported by the cover member.

Abstract: Apparatus and methods for performing satellite proximity operations such as inspection, recovery and life extension of a target satellite through operation of a “Satellite Inspection Recovery and Extension” (“SIRE”) spacecraft which can be operated in the following modes (teleoperated, automatic, and autonomous). The SIRE concept further consists of those methods and techniques used to perform certain (on-orbit) operations including, but not limited to, the inspection, servicing, recovery, and lifetime extension of satellites, spacecraft, space systems, space platforms, and other vehicles and objects in space, collectively defined as “target satellites”. The three basic types of SIRE proximity missions are defined as “Lifetime Extension”, “Recovery”, and “Utility”. A remote cockpit system is provided to permit human control of the SIRE spacecraft during proximity operations.

Abstract: Apparatus and methods for performing satellite proximity operations such as inspection, recovery and life extension of a target satellite through operation of a “Satellite Inspection Recovery and Extension” (“SIRE”) spacecraft which can be operated in the following modes (teleoperated, automatic, and autonomous). The SIRE concept further consists of those methods and techniques used to perform certain (on-orbit) operations including, but not limited to, the inspection, servicing, recovery, and lifetime extension of satellites, spacecraft, space systems, space platforms, and other vehicles and objects in space, collectively defined as “target satellites”. The three basic types of SIRE proximity missions are defined as “Lifetime Extension”, “Recovery”, and “Utility”. A remote cockpit system is provided to permit human control of the SIRE spacecraft during proximity operations.

Abstract: Apparatus and methods for performing satellite proximity operations such as inspection, recovery and life extension of a target satellite through operation of a "Satellite Inspection Recovery and Extension" ("SIRE") spacecraft which can be operated in the following modes (teleoperated, automatic, and autonomous). The SIRE concept further consists of those methods and techniques used to perform certain (on-orbit) operations including, but not limited to, the inspection, servicing, recovery, and lifetime extension of satellites, spacecraft, space systems, space platforms, and other vehicles and objects in space, collectively defined as "target satellites". The three basic types of SIRE proximity missions are defined as "Lifetime Extension", "Recovery", and "Utility". A remote cockpit system is provided to permit human control of the SIRE spacecraft during proximity operations.