Patents by Inventor Rajeev V. Naik

Rajeev V. Naik 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: 8540010
    Abstract: Method and apparatus for casting molten metal or alloy into a plurality of molds that are connected by mold ingate passages in melt flow communication to a melt supply passage which is configured in a manner to completely or partially fill the molds with the molten metal or alloy sequentially one after another. Filling of the molds in this manner provides uniform mold filling, reduces foreign matter in molds filled after the first-filled mold, and improves quality of the cast articles.
    Type: Grant
    Filed: April 16, 2007
    Date of Patent: September 24, 2013
    Assignee: Howmet Corporation
    Inventors: Brian D. Przeslawski, Rajeev V. Naik
  • Patent number: 6568458
    Abstract: A ceramic investment shell mold is reinforced with a carbon based fibrous reinforcement having an extremely high tensile strength that increases as the mold temperature is increased especially within the range of casting temperatures employed for casting large directionally solidified industrial gas turbine components. The carbon based fibrous reinforcement is wrapped or otherwise positioned around the repeating ceramic slurry/stucco layers forming the intermediate thickness of the shell mold wall. The reinforced shell mold can be used to cast large directionally solidified industrial gas turbine components with accurate dimensional control.
    Type: Grant
    Filed: October 30, 2001
    Date of Patent: May 27, 2003
    Assignee: Howmet Research Corporation
    Inventors: Rajeev V. Naik, John Corrigan
  • Patent number: 6460599
    Abstract: A ceramic investment shell mold is reinforced with a carbon based fibrous reinforcement having an extremely high tensile strength that increases as the mold temperature is increased especially within the range of casting temperatures employed for casting large directionally solidified industrial gas turbine components. The carbon based fibrous reinforcement is wrapped or otherwise positioned around the repeating ceramic slurry/stucco layers forming the intermediate thickness of the shell mold wall. The reinforced shell mold can be used to cast large directionally solidified industrial gas turbine components with accurate dimensional control.
    Type: Grant
    Filed: October 30, 2001
    Date of Patent: October 8, 2002
    Assignee: Howmet Research Corporation
    Inventors: Rajeev V. Naik, John Corrigan
  • Publication number: 20020134526
    Abstract: A ceramic investment shell mold is reinforced with a carbon based fibrous reinforcement having an extremely high tensile strength that increases as the mold temperature is increased especially within the range of casting temperatures employed for casting large directionally solidified industrial gas turbine components. The carbon based fibrous reinforcement is wrapped or otherwise positioned around the repeating ceramic slurry/stucco layers forming the intermediate thickness of the shell mold wall. The reinforced shell mold can be used to cast large directionally solidified industrial gas turbine components with accurate dimensional control.
    Type: Application
    Filed: October 30, 2001
    Publication date: September 26, 2002
    Applicant: Howmet Research Corporation.
    Inventors: Rajeev V. Naik, John Corrigan
  • Publication number: 20020084057
    Abstract: A ceramic investment shell mold is reinforced with a carbon based fibrous reinforcement having an extremely high tensile strength that increases as the mold temperature is increased especially within the range of casting temperatures employed for casting large directionally solidified industrial gas turbine components. The carbon based fibrous reinforcement is wrapped or otherwise positioned around the repeating ceramic slurry/stucco layers forming the intermediate thickness of the shell mold wall. The reinforced shell mold can be used to cast large directionally solidified industrial gas turbine components with accurate dimensional control.
    Type: Application
    Filed: October 30, 2001
    Publication date: July 4, 2002
    Applicant: Howmet Research Corporation
    Inventors: Rajeev V. Naik, John Corrigan
  • Patent number: 6364000
    Abstract: A ceramic investment shell mold is reinforced with a carbon based fibrous reinforcement having an extremely high tensile strength that increases as the mold temperature is increased especially within the range of casting temperatures employed for casting large directionally solidified industrial gas turbine components. The carbon based fibrous reinforcement is wrapped or otherwise positioned around the repeating ceramic slurry/stucco layers forming the intermediate thickness of the shell mold wall. The reinforced shell mold can be used to cast large directionally solidified industrial gas turbine components with accurate dimensional control.
    Type: Grant
    Filed: September 23, 1997
    Date of Patent: April 2, 2002
    Assignee: Howmet Research Corporation
    Inventors: Rajeev V. Naik, John Corrigan
  • Publication number: 20010009182
    Abstract: A ceramic investment shell mold is reinforced with a carbon based fibrous reinforcement having an extremely high tensile strength that increases as the mold temperature is increased especially within the range of casting temperatures employed for casting large directionally solidified industrial gas turbine components. The carbon based fibrous reinforcement is wrapped or otherwise positioned around the repeating ceramic slurry/stucco layers forming the intermediate thickness of the shell mold wall. The reinforced shell mold can be used to cast large directionally solidified industrial gas turbine components with accurate dimensional control.
    Type: Application
    Filed: September 23, 1997
    Publication date: July 26, 2001
    Inventors: RAJEEV V. NAIK, JOHN CORRIGAN
  • Patent number: 6029736
    Abstract: A reinforced core for use in metal casting processes, especially directional solidification casting processes, comprises an elongated, thin-walled outer quartz or silica rich tubular member and a carbon base reinforcement disposed in and extending along a length of the tubular member. The carbon base reinforcement can comprise one or more graphite rods cemented together in end-to-end relation or a carbon fiber bundle. The carbon base reinforcement can include an outer carbide surface region by coating or surface reaction.
    Type: Grant
    Filed: August 29, 1997
    Date of Patent: February 29, 2000
    Assignee: Howmet Research Corporation
    Inventors: Rajeev V. Naik, John Corrigan
  • Patent number: 4832105
    Abstract: Method and apparatus for producing an investment casting from molten material by filling a cavity in a mold with the molten material utilizing at least one porous member in the inlet conduit system of the mold, the porous member enabling evacuation of the mold cavity, through the inlet conduit system and the porous member, and having a structure including pores small enough subsequently to support the molten material upon the porous member by surface tension, with the molten material closing off essentially all atmospheric communication between the inside and the outside of the mold cavity, to thereby prevent passage of the molten material into the mold cavity until the method and apparatus subsequently raises the pressure outside the mold to provide a higher pressure outside the mold cavity and create a differential pressure between the inside and the outside of the mold cavity sufficient to overcome the surface tension and urge the molten material to pass through the pores of the porous member and fill the
    Type: Grant
    Filed: January 13, 1988
    Date of Patent: May 23, 1989
    Assignee: The Interlake Corporation
    Inventors: Raymond M. Nagan, Antulio D. Marrero, Rajeev V. Naik, Victoria Gleyzer