Patents by Inventor Po-Shou Chen

Po-Shou Chen 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: 9365917
    Abstract: A method is provided for heat treating aluminum-lithium alloys to improve their formability. The alloy is heated to a first temperature, maintained at the first temperature for a first time period, heated at the conclusion of the first time period to a second temperature, maintained at the second temperature for a second time period, actively cooled at the conclusion of the second time period to a third temperature, maintained at the third temperature for a third time period, and then passively cooled at the conclusion of the third time period to room temperature.
    Type: Grant
    Filed: March 24, 2014
    Date of Patent: June 14, 2016
    Assignee: The United States of America as Represented by the Administrator of the National Aeronatics and Space Administration
    Inventors: Po-Shou Chen, Carolyn Kurgan Russell
  • Patent number: 6918970
    Abstract: A cast article from an aluminum alloy has improved mechanical properties at elevated temperatures. The cast article has the following composition in weight percent: Silicon 6.0-25.0, Copper 5.0-8.0, Iron 0.05-1.2, Magnesium 0.5-1.5, Nickel 0.05-0.9, Manganese 0.05-1.2, Titanium 0.05-1.2, Zirconium 0.05-1.2, Vanadium 0.05-1.2, Zinc 0.05-0.9, Strontium 0.001-0.1, Phosphorus 0.001-0.1, and the balance is Aluminum, wherein the silicon-to-magnesium ratio is 10-25, and the copper-to-magnesium ratio is 4-15. The aluminum alloy contains a simultaneous dispersion of three types of Al3X compound particles (X=Ti, V, Zr) having a L12 crystal structure, and their lattice parameters are coherent to the aluminum matrix lattice. A process for producing this cast article is also disclosed, as well as a metal matrix composite, which includes the aluminum alloy serving as a matrix containing up to about 60% by volume of a secondary filler material.
    Type: Grant
    Filed: April 10, 2002
    Date of Patent: July 19, 2005
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Jonathan A. Lee, Po-Shou Chen
  • Patent number: 6669792
    Abstract: A process for making a cast article from an aluminum alloy includes first casting an article from an alloy having the following composition, in weight percent: Silicon (Si) 14.0-25.0 Copper (Cu) 5.5-8.0 Iron (Fe)   0-0.8 Magnesium (Mg) 0.5-1.5 Nickel (Ni) 0.05-1.2  Manganese (Mn)   0-1.0 Titanium (Ti) 0.05-1.2  Zirconium (Zr) 0.12-1.2  Vanadium (V) 0.05-1.2  Zinc (Zn)   0-0.9 Phosphorus (P) 0.001-0.1  Aluminum balance In this alloy the ration of Si:Mg is 15-35, and the ratio of Cu:Mg is 4-15. After an article is cast from the alloy, the cast article is aged at a temperature within the range of 400° F. to 500° F. for a time period within the range of four to 16 hours. It has been found especially advantageous if the cast article is first exposed to a solutionizing step prior to the aging step.
    Type: Grant
    Filed: March 2, 2001
    Date of Patent: December 30, 2003
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Jonathan A. Lee, Po-Shou Chen
  • Publication number: 20030192627
    Abstract: A cast article from an aluminum alloy has improved mechanical properties at elevated temperatures. The cast article has the following composition in weight percent: Silicon 6.0-25.0, Copper 5.0-8.0, Iron 0.05-1.2, Magnesium 0.5-1.5, Nickel 0.05-0.9, Manganese 0.05-1.2, Titanium 0.05-1.2, Zirconium 0.05-1.2, Vanadium 0.05-1.2, Zinc 0.05-0.9, Strontium 0.001-0.1, Phosphorus 0.001-0.1, and the balance is Aluminum, wherein the silicon-to-magnesium ratio is 10-25, and the copper-to-magnesium ratio is 4-15. The aluminum alloy contains a simultaneous dispersion of three types of Al3X compound particles (X=Ti, V, Zr) having a L12 crystal structure, and their lattice parameters are coherent to the aluminum matrix lattice. A process for producing this cast article is also disclosed, as well as a metal matrix composite, which includes the aluminum alloy serving as a matrix containing up to about 60% by volume of a secondary filler material.
    Type: Application
    Filed: April 10, 2002
    Publication date: October 16, 2003
    Inventors: Jonathan A. Lee, Po-Shou Chen
  • Patent number: 6592687
    Abstract: A cast article from an aluminum alloy, which has improved mechanical properties at elevated temperatures, has the following composition in weight percent: Silicon 14-25.0, Copper 5.5-8.0, Iron 0.05-1.2, Magnesium 0.5-1.5, Nickel 0.05-0.9, Manganese 0.05-1.0, Titanium 0.05-1.2, Zirconium 0.05-1.2, Vanadium 0.05-1.2, Zinc 0.05-0.9, Phosphorus 0.001-0.1, and the balance is Aluminum, wherein the silicon-to-magnesium ratio is 10-25, and the copper-to-magnesium ratio is 4-15. The aluminum alloy contains a simultaneous dispersion of three types of Al3X compound particles (X═Ti, V, Zr) having a L12 crystal structure, and their lattice parameters are coherent to the aluminum matrix lattice. A process for producing this cast article is also disclosed, as well as a metal matrix composite, which includes the aluminum alloy serving as a matrix and containing up to about 60% by volume of a secondary filler material.
    Type: Grant
    Filed: July 11, 2002
    Date of Patent: July 15, 2003
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Jonathan A. Lee, Po-Shou Chen
  • Patent number: 6419769
    Abstract: A process for making a cast article from an aluminum alloy includes first casting an article from an alloy having the following composition, in weight percent: Silicon 11.0-14.0 Copper 5.6-8.0 Iron   0-0.8 Magnesium 0.5-1.5 Nickel 0.05-0.9  Manganese   0-1.0 Titanium 0.05-1.2  Zirconium 0.12-1.2  Vanadium 0.05-1.2  Zinc 0.05-0.9  Strontium 0.001-0.1  Aluminum balance In this alloy the ration of silicon:magnesium is 10-25, and the ratio of copper:magnesium is 4-15. After an article is cast from the alloy, the cast article is aged at a temperature within the range of 400° F. to 500° F. for a time period within the range of four to 16 hours. It has been found especially advantageous if the cast article is first exposed to a solutionizing step prior to the aging step.
    Type: Grant
    Filed: December 22, 2000
    Date of Patent: July 16, 2002
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Jonathan A. Lee, Po-Shou Chen
  • Patent number: 6399020
    Abstract: An aluminum alloy suitable for high temperature applications, such as heavy duty pistons and other internal combustion applications, having the following composition, by weight percent (wt %): Silicon  11.0-14.0 Copper  5.6-8.0 Iron   0-0.8 Magnesium  0.5-1.5 Nickel 0.05-0.9 Manganese   0-1.0 Titanium 0.05-1.2 Zirconium 0.12-1.2 Vanadium 0.05-1.2 Zinc 0.05-0.9 Strontium 0.001-0.1  Aluminum balance. In this alloy the ratio of silicon:magnesium is 10-25, and the ratio of copper:magnesium is 4-15. After an article is cast from this alloy, the article is treated in a solutionizing step which dissolves unwanted precipitates and reduces any segregation present in the original alloy. After this solutionizing step, the article is quenched, and is then aged at an elevated temperature for maximum strength.
    Type: Grant
    Filed: October 11, 2000
    Date of Patent: June 4, 2002
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Jonathan A. Lee, Po-Shou Chen
  • Publication number: 20010010242
    Abstract: A process for making a cast article from an aluminum alloy includes first casting an article from an alloy having the following composition, in weight percent: 1 Silicon (Si) 14.0-25.0 Copper (Cu) 5.5-8.0 Iron (Fe)   0-0.8 Magnesium (Mg) 0.5-1.5 Nickel (Ni) 0.05-1.2  Manganese (Mn)   0-1.0 Titanium (Ti) 0.05-1.2  Zirconium (Zr) 0.12-1.2  Vanadium (V) 0.05-1.2  Zinc (Zn)   0-0.9 Phosphorus (P) 0.001-0.
    Type: Application
    Filed: March 2, 2001
    Publication date: August 2, 2001
    Applicant: United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Jonathan A. Lee, Po-Shou Chen