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).
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Patent number: 11920218Abstract: 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: GrantFiled: August 31, 2018Date of Patent: March 5, 2024Assignees: The Boeing Company, VSMPO-AVISMA CorporationInventors: Natalia G. Mitropolskaya, Robert D. Briggs, Michael Leder, Alexey Zaitsev, Igor Puzakov, Natalia Tarenkova
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Publication number: 20210310104Abstract: 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: ApplicationFiled: August 31, 2018Publication date: October 7, 2021Applicants: The Boeing Company, VSMPO-AVISMA CorporationInventors: Natalia G. Mitropolskaya, Robert D. Briggs, Michael Leder, Alexey Zaitsev, Igor Puzakov, Natalia Tarenkova
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Publication number: 20200149133Abstract: 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: ApplicationFiled: April 25, 2017Publication date: May 14, 2020Applicants: The Boeing Company, Public Stock Company VSMPO-AVISMA CorporationInventors: Michael Leder, Igor Puzakov, Natalia Tarenkova, Alexander Berestov, Natalia G. Mitropolskaya, Robert D. Briggs
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WELDED TITANIUM STRUCTURE UTILIZING DISSIMILAR TITANIUM ALLOY FILLER METAL FOR ENHANCED FATIGUE LIFE
Publication number: 20190308283Abstract: 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: ApplicationFiled: April 4, 2018Publication date: October 10, 2019Inventors: Catherine J. Parrish, Robert D. Briggs, Gary W. Coleman, Frederick W. Buldhaupt -
Patent number: 9956629Abstract: 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: GrantFiled: July 10, 2014Date of Patent: May 1, 2018Assignee: THE BOEING COMPANYInventor: Robert D. Briggs
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Publication number: 20160008903Abstract: 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: ApplicationFiled: July 10, 2014Publication date: January 14, 2016Inventor: Robert D. Briggs
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Patent number: 8262819Abstract: 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: GrantFiled: July 6, 2010Date of Patent: September 11, 2012Assignee: The Boeing CompanyInventor: Robert D. Briggs
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Publication number: 20100269958Abstract: 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: ApplicationFiled: July 6, 2010Publication date: October 28, 2010Applicant: The Boeing CompanyInventor: Robert D. Briggs
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Patent number: 7785429Abstract: 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: GrantFiled: June 10, 2003Date of Patent: August 31, 2010Assignee: The Boeing CompanyInventor: Robert D. Briggs
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Patent number: 7139559Abstract: 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: GrantFiled: December 9, 2002Date of Patent: November 21, 2006Assignee: Qualcomm Inc.Inventors: Jason B. Kenagy, Robert D. Briggs, Gina Lombardi, Mark Staskauskas, Marc Stephen Phillips, Robert J. Miller
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Patent number: 6868267Abstract: 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: GrantFiled: November 17, 2000Date of Patent: March 15, 2005Assignee: Qualcomm Inc.Inventors: Robert D. Briggs, Jason Kenagy, Gina Lombardi, Stephen A. Sprigg, Kent D. Baker, Marc S. Phillips
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Publication number: 20040250932Abstract: 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: ApplicationFiled: June 10, 2003Publication date: December 16, 2004Inventor: Robert D. Briggs
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Publication number: 20040110504Abstract: 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: ApplicationFiled: December 9, 2002Publication date: June 10, 2004Inventors: Jason B. Kenagy, Robert D. Briggs, Gina Lombardi, Mark Stakauskas, Marc Stephen Phillips, Robert J. Miller