Patents by Inventor Sue Troup

Sue Troup has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 6258415
    Abstract: A process for plating aluminum alloy substrates (10), such as 390 aluminum alloy pistons (12), with iron comprises (a) plating on the aluminum substrate a layer of zincate from a zincate bath; (b) plating on the zincate layer a layer (14) of nickel from an electroless nickel bath; (c) plating on the nickel layer a layer (16) of iron from an iron ammonium sulfate bath; and (d) plating on the iron layer a layer (18) of tin from an alkaline tin bath. During the electroless plating, the zincate layer, which protects the underlying aluminum against oxidation, is sacrificed. All of these baths are environmentally much safer than cyanide and chloride. They are also cost effective and can be utilized in a totally closed loop plating system.
    Type: Grant
    Filed: February 3, 1994
    Date of Patent: July 10, 2001
    Assignee: Hughes Electronics Corporation
    Inventor: Sue Troup-Packman
  • Patent number: 5810992
    Abstract: A process for plating aluminum alloy substrates such as aluminum pistons with an iron-cobalt alloy comprising the steps of (a) plating on the aluminum alloy substrate a thin layer of nickel from an electroless nickel bath; and (b) plating on the nickel layer a layer of iron-cobalt alloy from an iron-cobalt electroplating bath. The iron-cobalt layer is not subject to the corrosion problems inherent in a substantially pure iron-plated coating nor the excessive hardness, costliness, and environmental concerns related to the use of nickel as the primary plated layer. The iron-cobalt electroplating bath is cost-effective and can be utilized in a totally closed loop plating system. The resulting iron-cobalt plated, aluminum alloy parts evidence good adhesion, wear, thermal conductivity, and corrosion-resistant properties.
    Type: Grant
    Filed: February 28, 1997
    Date of Patent: September 22, 1998
    Assignee: Hughes Electronics Corporation
    Inventor: Sue Troup-Packman
  • Patent number: 5534358
    Abstract: A process for plating aluminum alloy substrates (10), such as 390 aluminum alloy pistons (12), with iron comprises (a) plating on the aluminum substrate a layer of zincate from a zincate bath; (b) plating on the zincate layer a layer (14) of nickel from an electroless nickel bath; (c) plating on the nickel layer a layer (16) of iron from an iron ammonium sulfate bath; and (d) plating on the iron layer a layer (18) of tin from an alkaline tin bath. During the electroless plating, the zincate layer, which protects the underlying aluminum against oxidation, is sacrificed. All of these baths are environmentally much safer than cyanide and chloride. They are also cost effective and can be utilized in a totally closed loop plating system.
    Type: Grant
    Filed: February 2, 1994
    Date of Patent: July 9, 1996
    Assignee: Hughes Aircraft Company
    Inventor: Sue Troup-Packman
  • Patent number: 5516419
    Abstract: Aluminum and aluminum alloy parts, such as pistons, are electroplated with iron employing a ferrous electroplating solution. The solution comprises (a) ferrous iron having a concentration ranging from about 0.65 to 2.0 Moles of Fe.sup.2+ per liter of solution; (b) at least one anion selected from the group consisting of sulfamate and ammonium sulfate and associated with the Fe.sup.2+ ions; (c) a reducing agent, such as ascorbic acid, in an amount sufficient to prevent oxidation of Fe.sup.2+ to Fe.sup.3+ ; (d) Cl.sup.- anion in an amount sufficient to promote dissolution of the iron anode; and (e) a wetting agent in an amount sufficient to prevent pitting of the aluminum cathode. The ferrous electroplating bath of the present invention permits plating of relatively thick layers of iron on aluminum, typically on the order of about 0.6 to 2 mils (0.0015 to 0.0051 cm), with a microhardness of at least about 40 (Rockwell C scale).
    Type: Grant
    Filed: May 26, 1994
    Date of Patent: May 14, 1996
    Assignee: Hughes Aircraft Company
    Inventors: Nguyet H. Phan, Sue Troup-Packman
  • Patent number: 5368719
    Abstract: A process for plating aluminum and aluminum alloy substrates, such as 390 aluminum alloy pistons, with iron comprises (a) cathodically activating the aluminum-containing substrate in an acid bath and (b) plating iron from an iron sulfate-containing bath,
    Type: Grant
    Filed: May 12, 1993
    Date of Patent: November 29, 1994
    Assignee: Hughes Aircraft Company
    Inventor: Sue Troup-Packman
  • Patent number: 4960493
    Abstract: A metal such as copper is deposited as a layer upon a substrate such as molybdenum by cleaning the substrate, etching the substrate to remove gross oxides thereupon, treating the substrate in a concentrated acid, such as hydrochloric acid, with the substrate made cathodic, depositing a metal strike layer, such as nickel or gold, on the substrate, and depositing the metallic layer overlying the strike layer. The cathodic treatment in the concentrated acid permits deposition of the strike layer before the oxide layer reforms.
    Type: Grant
    Filed: April 3, 1989
    Date of Patent: October 2, 1990
    Assignee: Hughes Aircraft Company
    Inventor: Sue Troup
  • Patent number: 4938850
    Abstract: A method for application of an adherent nickel plate to titanium includes steps of surface preparation, deposition of nickel from a plating solution, and a final treatment. The surface preparation steps include a hydrochloric acid dip, a nitric acid/hydrofluoric acid activation, treatment to slow the re-formation of an oxide layer, and deposition of a nickel strike. The treatment to reduce oxide formation may be accomplished without application of a current, in a solution of acetic and hydrofluoric acid, in which titanium alloy has been electrolytically dissolved. Alternatively, the treatment may be performed with the piece to be plated made anodic in a solution of acetic acid and hydrofluoric acid.
    Type: Grant
    Filed: September 26, 1988
    Date of Patent: July 3, 1990
    Assignee: Hughes Aircraft Company
    Inventors: Bill F. Rothschild, Sue Troup