Patents by Inventor Robert D. Briggs

Robert D. Briggs 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: 11920218
    Abstract: This invention generally relates to the field of nonferrous metallurgy, namely to titanium alloy materials with specified mechanical properties for manufacturing the aircraft fasteners. A stock for high strength fastener is manufactured from wrought titanium alloy containing, in weight percentages, 5.5 to 6.5 Al, 3.0 to 4.5 V, 1.0 to 2.0 Mo, 0.3 to 1.5 Fe, 0.3 to 1.5 Cr, 0.05 to 0.5 Zr, 0.15 to 0.3 O, 0.05 max. N, 0.08 max. C, 0.25 max. Si, balance titanium and inevitable impurities, having the value of aluminum structural equivalent [Al] eq in the range of 7.5 to 9.5, and the value of molybdenum structural equivalent [Mo] eq in the range of 6.0 to 8.5, where the equivalents are defined by the following equations: [Al] eq=[Al]+[O]×10+[Zr]/6; [Mo] eq=[Mo]+[V]/1.5+[Cr]×1.25+[Fe]×2.5.
    Type: Grant
    Filed: August 31, 2018
    Date of Patent: March 5, 2024
    Assignees: The Boeing Company, VSMPO-AVISMA Corporation
    Inventors: Natalia G. Mitropolskaya, Robert D. Briggs, Michael Leder, Alexey Zaitsev, Igor Puzakov, Natalia Tarenkova
  • Publication number: 20210310104
    Abstract: This invention generally relates to the field of nonferrous metallurgy, namely to titanium alloy materials with specified mechanical properties for manufacturing the aircraft fasteners. A stock for high strength fastener is manufactured from wrought titanium alloy containing, in weight percentages, 5.5 to 6.5 Al, 3.0 to 4.5 V, 1.0 to 2.0 Mo, 0.3 to 1.5 Fe, 0.3 to 1.5 Cr, 0.05 to 0.5 Zr, 0.15 to 0.3 O, 0.05 max. N, 0.08 max. C, 0.25 max. Si, balance titanium and inevitable impurities, having the value of aluminum structural equivalent [Al]eq in the range of 7.5 to 9.5, and the value of molybdenum structural equivalent [Mo]eq in the range of 6.0 to 8.5, where the equivalents are defined by the following equations: [Al]eq=[Al]+[O]×10+[Zr]/6; [Mo]eq=[Mo]+[V]/1.5+[Cr]×1.25+[Fe]×2.5.
    Type: Application
    Filed: August 31, 2018
    Publication date: October 7, 2021
    Applicants: The Boeing Company, VSMPO-AVISMA Corporation
    Inventors: Natalia G. Mitropolskaya, Robert D. Briggs, Michael Leder, Alexey Zaitsev, Igor Puzakov, Natalia Tarenkova
  • Publication number: 20200149133
    Abstract: Herein disclosed includes the manufacture of sheets from a titanium alloy having a chemical composition efficiently balanced with manufacturability based on known conventional manufacturing techniques for finished products exhibiting low temperature superplastic forming properties. The result is achieved by a sheet material for low temperature superplastic made of titanium alloy with the following content of element by % wt.: 4.5-5.5Al, 4.5-5.5V, 0.1-1.0Mo, 0.8-1.5Fe, 0.1-0.5Cr, 0.1-0.5Ni, 0.16-0.25O, remainder is titanium and residual elements and having molybdenum structural equivalent [Mo]eqiv.>5 and aluminum structural equivalent [Al]equiv.<8; the equivalent values are calculated from the expressions: [Mo]eqiv.=[Mo]+[V]/1.5+[Cr]×1.25+[Fe]×2.5+[Ni]/0.8 [Al]eqiv.=[Al]+[O]×10+[Zr]/6.
    Type: Application
    Filed: April 25, 2017
    Publication date: May 14, 2020
    Applicants: The Boeing Company, Public Stock Company VSMPO-AVISMA Corporation
    Inventors: Michael Leder, Igor Puzakov, Natalia Tarenkova, Alexander Berestov, Natalia G. Mitropolskaya, Robert D. Briggs
  • Publication number: 20190308283
    Abstract: Provided is a method for welding dissimilar types of titanium. The method utilizes a filler metal that is also dissimilar to the types of titanium being welded. The method forms welds with improved fatigue life at room and high temperatures with no loss of tensile strength compared to welds formed by conventional methods of welding titanium.
    Type: Application
    Filed: April 4, 2018
    Publication date: October 10, 2019
    Inventors: Catherine J. Parrish, Robert D. Briggs, Gary W. Coleman, Frederick W. Buldhaupt
  • Patent number: 9956629
    Abstract: A method and apparatus for forming a fastener for an aircraft. An annealed titanium alloy is provided with about 5.50 to about 6.75 weight percent aluminum, about 3.50 to about 4.50 weight percent vanadium, more than 0.20 weight percent oxygen, and more than 0.30 weight percent iron. Operations are performed to form the fastener for the aircraft from the annealed titanium alloy.
    Type: Grant
    Filed: July 10, 2014
    Date of Patent: May 1, 2018
    Assignee: THE BOEING COMPANY
    Inventor: Robert D. Briggs
  • Publication number: 20160008903
    Abstract: A method and apparatus for forming a fastener for an aircraft. An annealed titanium alloy is provided with about 5.50 to about 6.75 weight percent aluminum, about 3.50 to about 4.50 weight percent vanadium, more than 0.20 weight percent oxygen, and more than 0.30 weight percent iron. Operations are performed to form the fastener for the aircraft from the annealed titanium alloy.
    Type: Application
    Filed: July 10, 2014
    Publication date: January 14, 2016
    Inventor: Robert D. Briggs
  • Patent number: 8262819
    Abstract: The present disclosure describes methods of heat treating Ti-based alloys and various improvements that can be realized using such heat treatments. In one exemplary implementation, the invention provides a method of forming a metal member that involves forming an alloy into a utile shape and cooling the alloy from a first temperature above a beta transus temperature of the alloy to a second temperature below the beta transus temperature at a cooling rate of no more than about 30° F./minute. If so desired, the alloy my be treated for a period of about 1-12 hours at about 700-1100° F. Titanium alloys treated according to aspects of the invention may have higher tensile strengths and higher fracture toughness than conventional wrought, mill-annealed Ti 64 alloy.
    Type: Grant
    Filed: July 6, 2010
    Date of Patent: September 11, 2012
    Assignee: The Boeing Company
    Inventor: Robert D. Briggs
  • Publication number: 20100269958
    Abstract: The present disclosure describes methods of heat treating Ti-based alloys and various improvements that can be realized using such heat treatments. In one exemplary implementation, the invention provides a method of forming a metal member that involves forming an alloy into a utile shape and cooling the alloy from a first temperature above a beta transus temperature of the alloy to a second temperature below the beta transus temperature at a cooling rate of no more than about 30° F./minute. If so desired, the alloy my be treated for a period of about 1-12 hours at about 700-1100° F. Titanium alloys treated according to aspects of the invention may have higher tensile strengths and higher fracture toughness than conventional wrought, mill-annealed Ti 64 alloy.
    Type: Application
    Filed: July 6, 2010
    Publication date: October 28, 2010
    Applicant: The Boeing Company
    Inventor: Robert D. Briggs
  • Patent number: 7785429
    Abstract: The present disclosure describes methods of heat treating Ti-based alloys and various improvements that can be realized using such heat treatments. In one exemplary implementation, the invention provides a method of forming a metal member that involves forming an alloy into a utile shape and cooling the alloy from a first temperature above a beta transus temperature of the alloy to a second temperature below the beta transus temperature at a cooling rate of no more than about 30° F./minute. If so desired, the alloy my be treated for a period of about 1-12 hours at about 700-1100° F. Titanium alloys treated according to aspects of the invention may have higher tensile strengths and higher fracture toughness than conventional wrought, mill-annealed Ti 64 alloy.
    Type: Grant
    Filed: June 10, 2003
    Date of Patent: August 31, 2010
    Assignee: The Boeing Company
    Inventor: Robert D. Briggs
  • Patent number: 7139559
    Abstract: A system, method, and computer program for data communication, or “handshaking,” between wireless devices and a server on a wireless network. Upon a wireless device communicating with the server, the server obtains data from the wireless device indicative of wireless device attributes, and the server determines access of the wireless device, based upon the wireless device attributes, to applications either resident on that server or on other computer devices on the wireless network.
    Type: Grant
    Filed: December 9, 2002
    Date of Patent: November 21, 2006
    Assignee: Qualcomm Inc.
    Inventors: Jason B. Kenagy, Robert D. Briggs, Gina Lombardi, Mark Staskauskas, Marc Stephen Phillips, Robert J. Miller
  • Patent number: 6868267
    Abstract: An apparatus, method, and article of manufacture that provides an efficient way to invoice the users of a communication system (100) for the system resources consumed. Invoicing is based upon flexible criteria that can be adapted depending upon the charges a resource provider charges. For example, a user may incur a one-time charge for downloading a desired application program, or the user may be charged a download fee plus a recurring monthly fee for having continual access to the program and any updates to the program. A fee might also be charged for each time the application is used. These fees are recorded as debits and transferred to an invoicing location where an invoice reflecting the debits is constructed. For example, the debits may comprise fees for wireless service access, Internet service access, downloaded application programs, data, multimedia services, or other fees.
    Type: Grant
    Filed: November 17, 2000
    Date of Patent: March 15, 2005
    Assignee: Qualcomm Inc.
    Inventors: Robert D. Briggs, Jason Kenagy, Gina Lombardi, Stephen A. Sprigg, Kent D. Baker, Marc S. Phillips
  • Publication number: 20040250932
    Abstract: The present disclosure describes methods of heat treating Ti-based alloys and various improvements that can be realized using such heat treatments. In one exemplary implementation, the invention provides a method of forming a metal member that involves forming an alloy into a utile shape and cooling the alloy from a first temperature above a beta transus temperature of the alloy to a second temperature below the beta transus temperature at a cooling rate of no more than about 30° F./minute. If so desired, the alloy my be treated for a period of about 1-12 hours at about 700-1100° F. Titanium alloys treated according to aspects of the invention may have higher tensile strengths and higher fracture toughness than conventional wrought, mill-annealed Ti 64 alloy.
    Type: Application
    Filed: June 10, 2003
    Publication date: December 16, 2004
    Inventor: Robert D. Briggs
  • Publication number: 20040110504
    Abstract: A system, method, and computer program for data communication, or “handshaking,” between wireless devices and a server on a wireless network. Upon a wireless device communicating with the server, the server obtains data from the wireless device indicative of wireless device attributes, and the server determines access of the wireless device, based upon the wireless device attributes, to applications either resident on that server or on other computer devices on the wireless network.
    Type: Application
    Filed: December 9, 2002
    Publication date: June 10, 2004
    Inventors: Jason B. Kenagy, Robert D. Briggs, Gina Lombardi, Mark Stakauskas, Marc Stephen Phillips, Robert J. Miller