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AEROMET TECHNOLOGIES, INC.
| AEROMET TECHNOLOGIES, INC. Patent applications | ||
| Patent application number | Title | Published |
|---|---|---|
| 20090120804 | APPARATUS, METHODS, AND COMPOSITIONS FOR REMOVING COATINGS FROM A METAL COMPONENT - Apparatus and methods for removing coatings from metal components, such as metal components used in aircraft and other aerospace vehicles and the oil industry, as well as aqueous bath compositions. The metal component may be DC coupled with a counter electrode and immersed in an aqueous bath that includes an active oxygen source and a ligand in a composition effective to remove the coating. The aqueous bath may include hydrogen peroxide as the active oxygen source and may be maintained in a specific pH range if the temperature of the aqueous bath is controlled. In an alternative embodiment, the composition of the aqueous bath may include a non-peroxide active oxygen source, such as sodium perborate, and be maintained in a different specific pH range. An oxygen sensor may be provided to periodically monitor the concentration of active oxygen in the aqueous bath. | 05-14-2009 |
| 20080274290 | Metal Components With Silicon-Containing Protective Coatings Substantially Free of Chromium and Methods of Forming Such Protective Coatings - A metal component ( | 11-06-2008 |
| 20080273985 | Roughened Coatings for Gas Turbine Engine Components - A gas turbine engine component ( | 11-06-2008 |
| 20080245302 | SIMPLE CHEMICAL VAPOR DEPOSITION SYSTEMS FOR DEPOSITING MULTIPLE-METAL ALUMINIDE COATINGS - A chemical vapor deposition (CVD) system and method for applying an aluminide coating constituted by two or more extrinsic metal components on a jet engine component. The aluminide coating is capable of forming a protective complex oxide upon subsequent heating in an oxidizing environment. At least one of the extrinsic metals in the aluminide coating is provided as a first vapor phase reactant from a receptacle coupled by a closed communication path with the reaction chamber of the CVD system and free of a carrier gas. The aluminide coating is formed by the chemical combination of the first vapor phase reactant with a second vapor phase reactant either created in situ in the reaction chamber or supplied by a carrier gas to the reaction chamber from a precursor source. | 10-09-2008 |
| 20080220165 | Gas Turbine Engine Components With Aluminide Coatings And Method Of Forming Such Aluminide Coatings On Gas Turbine Engine Components - A turbine engine component ( | 09-11-2008 |