Patents by Inventor David H. Gane

David H. Gane 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: 10415128
    Abstract: A method for manufacturing a part including steps of (1) casting an ingot, (2) scalping the ingot to yield a scalped ingot, (3) homogenizing the scalped ingot to yield a homogenized ingot, (4) breakdown of the homogenized ingot to yield a slab, (5) rolling the slab to yield a rolled aluminum material, (6) annealing the rolled aluminum material to yield an aluminum starting material, (7) cold working the aluminum starting material to obtain an aluminum cold worked material, and (8) forming the part from the aluminum cold worked material.
    Type: Grant
    Filed: June 11, 2018
    Date of Patent: September 17, 2019
    Assignee: The Boeing Company
    Inventors: David H. Gane, Ryan J. Glamm, Gary R. Weber, Ricole A. Johnson, Terry C. Tomt, Azzreal Pugh, Daniel J. Kane, Peter D. Verge
  • Publication number: 20180291488
    Abstract: A method for manufacturing a part including steps of (1) casting an ingot, (2) scalping the ingot to yield a scalped ingot, (3) homogenizing the scalped ingot to yield a homogenized ingot, (4) breakdown of the homogenized ingot to yield a slab, (5) rolling the slab to yield a rolled aluminum material, (6) annealing the rolled aluminum material to yield an aluminum starting material, (7) cold working the aluminum starting material to obtain an aluminum cold worked material, and (8) forming the part from the aluminum cold worked material.
    Type: Application
    Filed: June 11, 2018
    Publication date: October 11, 2018
    Applicant: The Boeing Company
    Inventors: David H. Gane, Ryan J. Glamm, Gary R. Weber, Ricole A. Johnson, Terry C. Tomt, Azzreal Pugh, Daniel J. Kane, Peter D. Verge
  • Patent number: 10030294
    Abstract: A method for manufacturing a part including steps of providing an aluminum starting material, wherein the aluminum starting material is in an anneal temper, cold working the aluminum starting material to obtain an aluminum cold worked material, and forming the part from the aluminum cold worked material.
    Type: Grant
    Filed: February 16, 2015
    Date of Patent: July 24, 2018
    Assignee: The Boeing Company
    Inventors: David H. Gane, Ryan J. Glamm, Gary R. Weber, Ricole A. Johnson, Terry C. Tomt, Azzréal Pugh, Daniel J. Kane, Peter D. Verge
  • Publication number: 20160237539
    Abstract: A method for manufacturing a part including steps of providing an aluminum starting material, wherein the aluminum starting material is in an anneal temper, cold working the aluminum starting material to obtain an aluminum cold worked material, and forming the part from the aluminum cold worked material.
    Type: Application
    Filed: February 16, 2015
    Publication date: August 18, 2016
    Inventors: David H. Gane, Ryan J. Glamm, Gary R. Weber
  • Patent number: 6656603
    Abstract: A method of making an expanded metal sandwich structure includes cleaning at least two metal superplastic core sheets to remove metal oxides and residues that would interfere with diffusion bonding of the sheets. The core sheets are placed face-to-face and a gas pressure line fitting is inserted between one edge and is welded into place. The fitting has a through bore through which gas can flow under pressure from a gas pressure control system into the space between the core sheets. The core sheets are pressed together and laser welded together into a core pack along lines which will form junction lines between the core sheets when the core pack is superplastically expanded. The core pack is chemically cleaned to remove metal oxides and residues that would interfere with diffusion bonding of the core pack sheets to face sheets. Two metal face sheets having superplastic characteristics are chemically cleaned and placed over and under the core pack.
    Type: Grant
    Filed: June 6, 2002
    Date of Patent: December 2, 2003
    Assignee: The Boeing Company
    Inventors: Frederick W. Buldhaupt, David H. Gane, Matthew G. Kistner, Jeffrey D. Will
  • Publication number: 20030049482
    Abstract: A method of making an expanded metal sandwich structure includes cleaning at least two metal superplastic core sheets to remove metal oxides and residues that would interfere with diffusion bonding of the sheets. The core sheets are placed face-to-face and a gas pressure line fitting is inserted between one edge and is welded into place. The fitting has a through bore through which gas can flow under pressure from a gas pressure control system into the space between the core sheets. The core sheets are pressed together and laser welded together into a core pack along lines which will form junction lines between the core sheets when the core pack is superplastically expanded. The core pack is chemically cleaned to remove metal oxides and residues that would interfere with diffusion bonding of the core pack sheets to face sheets. Two metal face sheets having superplastic characteristics are chemically cleaned and placed over and under the core pack.
    Type: Application
    Filed: June 6, 2002
    Publication date: March 13, 2003
    Applicant: The Boeing Company
    Inventors: Frederick W. Buldhaupt, David H. Gane, Matthew G. Kistner, Jeffrey D. Will
  • Patent number: 6508394
    Abstract: A method of making an expanded metal sandwich structure includes cleaning at least two metal superplastic core sheets to remove metal oxides and residues that would interfere with diffusion bonding of the sheets. The core sheets are placed face-to-face and a gas pressure line fitting is inserted between one edge and is welded into place. The fitting has a through bore through which gas can from under pressure from a gas pressure control system into the space between the core sheets. The core sheets are pressed together and laser welded together into a core pack along lines which will form junction lines between the core sheets when the core pack is superplastically expanded. The core pack is chemically cleaned to remove metal oxides and residues that would interfere with diffusion bonding of the core pack sheets to face sheets. Two metal face sheets having superplastic characteristics are chemically cleaned and placed over and under the core pack.
    Type: Grant
    Filed: August 31, 1999
    Date of Patent: January 21, 2003
    Assignee: The Boeing Company
    Inventors: Frederick W. Buldhaupt, David H. Gane, Matthew G. Kistner, Jeffrey D. Will
  • Patent number: 5994666
    Abstract: A method of making an expanded metal sandwich structure includes cleaning at least two metal superplastic core sheets to remove metal oxides and residues that would interfere with diffusion bonding of the sheets. The core sheets are placed face-to-face and a gas pressure line fitting is inserted between one edge and is welded into place. The fitting has a through bore through which gas can flow under pressure into the space between the core sheets. The core sheets are pressed together and laser welded together into a core pack along lines which will form junction lines between the core sheets when the core pack is superplastically expanded. The core pack and the two metal face sheets having superplastic characteristics are each chemically cleaned, and the face sheets are placed over and under the core pack.
    Type: Grant
    Filed: July 10, 1998
    Date of Patent: November 30, 1999
    Assignee: The Boeing Company
    Inventors: Frederick W. Buldhaupt, David H. Gane, Matthew G. Kistner, Jeffrey D. Will
  • Patent number: 5144825
    Abstract: Elevated temperature envelope forming includes enclosing a part blank and form tool within an envelope sealed against the atmosphere, heat treating the combination while forming pressure holds the envelope and part against the form tool, and allowing part cool down to occur in an inert atmosphere with forming pressure removed. The forming pressure is provided by evacuating the envelope and may be aided by differential force applied between the envelope and the form tool.
    Type: Grant
    Filed: September 27, 1990
    Date of Patent: September 8, 1992
    Assignee: The Boeing Company
    Inventors: Bruce M. Burg, David H. Gane, Robert M. Starowski