Patents by Inventor Daniel G. Sanders

Daniel G. Sanders 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).

  • Publication number: 20230383412
    Abstract: Implementations are provided for fabricating a finished workpiece having a shaped portion. One implementation includes: a superplastic formation diffusion bonding (SPFDB) component; a cold spray additive manufacturing (CSAM) component; and a mold having a concavity. Various configurations can operate on a workpiece with the SPFDB and CSAM components in different orders. An implementation is configured to cold spray (with the CSAM component) an additive material onto the workpiece; and perform superplastic forming (with the SPFDB component) on the workpiece with the mold, thereby rendering the workpiece into the finished workpiece having the shaped portion. The shaped portion conforms to a shape defined by the concavity. Cold spraying results in an increased thickness of the finished workpiece in a target region, which can provide structural reinforcement, and which can have a tapered edge. The workpiece can be a metal substrate made of titanium, aluminum, stainless steel, or another material.
    Type: Application
    Filed: August 2, 2023
    Publication date: November 30, 2023
    Applicant: The Boeing Company
    Inventors: Bruno Zamorano Senderos, Dennis Lynn Coad, Daniel G. Sanders
  • Patent number: 11753723
    Abstract: Implementations are provided for fabricating a finished workpiece having a shaped portion. One implementation includes: a superplastic formation diffusion bonding (SPFDB) component; a cold spray additive manufacturing (CSAM) component; and a mold having a concavity. Various configurations can operate on a workpiece with the SPFDB and CSAM components in different orders. An implementation is configured to cold spray (with the CSAM component) an additive material onto the workpiece; and perform superplastic forming (with the SPFDB component) on the workpiece with the mold, thereby rendering the workpiece into the finished workpiece having the shaped portion. The shaped portion conforms to a shape defined by the concavity. Cold spraying results in an increased thickness of the finished workpiece in a target region, which can provide structural reinforcement, and which can have a tapered edge. The workpiece can be a metal substrate made of titanium, aluminum, stainless steel, or another material.
    Type: Grant
    Filed: June 2, 2020
    Date of Patent: September 12, 2023
    Assignee: THE BOEING COMPANY
    Inventors: Bruno Zamorano Senderos, Dennis Lynn Coad, Daniel G. Sanders
  • Publication number: 20230278696
    Abstract: A metallic structure includes a metallic sheet, including a metallic-sheet first surface and a metallic-sheet second surface. The metallic structure includes a metallic doubler, extending from the metallic-sheet first surface, and a first junction between the metallic-sheet first surface and the metallic doubler. The metallic structure includes a metallic article, extending from the metallic-sheet second surface, and a second junction between the metallic-sheet second surface and the metallic article. The first junction has a first-junction boundary. The second junction has a second-junction boundary. When viewed at any point along the second-junction boundary in a direction, perpendicular to the metallic-sheet first surface, the second-junction boundary does not extend outside of the first-junction boundary.
    Type: Application
    Filed: March 7, 2022
    Publication date: September 7, 2023
    Applicant: The Boeing Company
    Inventors: Daniel G. Sanders, Justin L′Hote, Eric D. Bol, Cory C. Cunningham
  • Patent number: 11633835
    Abstract: Systems for managing abrasive media in cavitated fluid include a set of sensors in communication with cavitated fluid in a processing tank and a processor coupled to the set of sensors. The processor is configured to determine a density of an abrasive media in the cavitated fluid in the processing tank and facilitate maintaining the density of abrasive media in the cavitated fluid in the processing tank at a level that is greater than or equal to a threshold level of abrasive media. The processor is further configured to command the abrasive media addition device to add the recycled abrasive media to the processing tank to increase the density of abrasive media in the cavitated fluid in response to determining that an average density of abrasive media is less than the threshold density of abrasive media.
    Type: Grant
    Filed: December 14, 2018
    Date of Patent: April 25, 2023
    Assignee: The Boeing Company
    Inventor: Daniel G. Sanders
  • Publication number: 20230029286
    Abstract: Disclosed herein is a system for surface treating an internal surface of a part. The system comprises a tank within which the part is locatable. The system also comprises a fluid within the tank and capable of submersing the part when the part is located within the tank. The system further comprises a nozzle submersed in the fluid and configured to generate a stream of cavitated fluid directed in a first direction. The system additionally comprises a deflection tool submersed in the fluid and comprising a deflection surface that redirects the stream of cavitated fluid from the first direction to a second direction. The first direction is away from the internal surface of the part and the second direction is toward the internal surface of the part.
    Type: Application
    Filed: October 4, 2022
    Publication date: January 26, 2023
    Inventors: Daniel G. Sanders, Amanda J. Wickramaratne, Hali T. Diep, Gregory L. Ramsey
  • Patent number: 11465259
    Abstract: Disclosed herein is a system for surface treating an internal surface of a part. The system comprises a tank within which the part is locatable. The system also comprises a fluid within the tank and capable of submersing the part when the part is located within the tank. The system further comprises a nozzle submersed in the fluid and configured to generate a stream of cavitated fluid directed in a first direction. The system additionally comprises a deflection tool submersed in the fluid and comprising a deflection surface that redirects the stream of cavitated fluid from the first direction to a second direction. The first direction is away from the internal surface of the part and the second direction is toward the internal surface of the part.
    Type: Grant
    Filed: February 13, 2019
    Date of Patent: October 11, 2022
    Assignee: The Boeing Company
    Inventors: Daniel G. Sanders, Amanda J. Thoreson, Hali T. Diep, Gregory L. Ramsey
  • Publication number: 20210371986
    Abstract: Implementations are provided for fabricating a finished workpiece having a shaped portion. One implementation includes: a superplastic formation diffusion bonding (SPFDB) component; a cold spray additive manufacturing (CSAM) component; and a mold having a concavity. Various configurations can operate on a workpiece with the SPFDB and CSAM components in different orders. An implementation is configured to cold spray (with the CSAM component) an additive material onto the workpiece; and perform superplastic forming (with the SPFDB component) on the workpiece with the mold, thereby rendering the workpiece into the finished workpiece having the shaped portion. The shaped portion conforms to a shape defined by the concavity. Cold spraying results in an increased thickness of the finished workpiece in a target region, which can provide structural reinforcement, and which can have a tapered edge. The workpiece can be a metal substrate made of titanium, aluminum, stainless steel, or another material.
    Type: Application
    Filed: June 2, 2020
    Publication date: December 2, 2021
    Inventors: Bruno Zamorano Senderos, Dennis Lynn Coad, Daniel G. Sanders
  • Patent number: 10871471
    Abstract: A system and method for inspecting an additively manufactured component include an additive manufacturing head configured to form a component layer-by-layer, and an electromagnetic acoustic transducer (EMAT) configured to inspect one or more layers of the component.
    Type: Grant
    Filed: January 2, 2020
    Date of Patent: December 22, 2020
    Assignee: THE BOEING COMPANY
    Inventors: Daniel G. Sanders, John R. Hull, Gary E. Georgeson
  • Patent number: 10843291
    Abstract: A component is formed by welding a plurality of sheets of metal to form a blank with a number of weld nuggets, placing the blank between a die section and a lid section, heating the die section to heat the blank, and introducing a pressurized gas between the lid section and the die section to press the blank into a mold in the die section to form a component. The number of weld nuggets has a desired thickness ratio between about 1.1 to about 1.25 such that the plurality of sheets of metal and the component formed have a number of characteristics that are substantially the same.
    Type: Grant
    Filed: November 12, 2009
    Date of Patent: November 24, 2020
    Assignee: The Boeing Company
    Inventors: Daniel G. Sanders, Luis R. Leon, Paul D. Edwards, Gregory L. Ramsey, Gary W. Coleman
  • Publication number: 20200254586
    Abstract: Disclosed herein is a system for surface treating an internal surface of a part. The system comprises a tank within which the part is locatable. The system also comprises a fluid within the tank and capable of submersing the part when the part is located within the tank. The system further comprises a nozzle submersed in the fluid and configured to generate a stream of cavitated fluid directed in a first direction. The system additionally comprises a deflection tool submersed in the fluid and comprising a deflection surface that redirects the stream of cavitated fluid from the first direction to a second direction. The first direction is away from the internal surface of the part and the second direction is toward the internal surface of the part.
    Type: Application
    Filed: February 13, 2019
    Publication date: August 13, 2020
    Inventors: Daniel G. Sanders, Amanda J. Thoreson, Hali T. Diep, Gregory L. Ramsey
  • Publication number: 20200189068
    Abstract: Disclosed herein are systems, methods, and apparatuses for managing abrasive media in cavitated fluid. One system includes a set of sensors in communication with the cavitated fluid in the processing tank and a processor coupled to the set of sensors. The processor is configured to determine a density of an abrasive media in the cavitated fluid in the processing tank and facilitate maintaining the density of abrasive media in the cavitated fluid in the processing tank at a level that is greater than or equal to a threshold level of abrasive media. A method includes determining a density of abrasive media in the cavitated fluid in the processing tank and maintaining the density of abrasive media in the cavitated fluid in the processing tank at a level that is greater than or equal to a threshold density of abrasive media. One apparatus includes modules for performing the method.
    Type: Application
    Filed: December 14, 2018
    Publication date: June 18, 2020
    Inventor: Daniel G. Sanders
  • Patent number: 10294815
    Abstract: A propulsion system comprises a turbine engine, and an engine nacelle including an SPF/DB inner wall having a hot side face sheet against the engine and a cold side face sheet that has noise attenuation openings.
    Type: Grant
    Filed: March 1, 2012
    Date of Patent: May 21, 2019
    Assignee: The Boeing Company
    Inventors: Max R. Runyan, Daniel G. Sanders, Larry D. Hefti, David R. Papenfuss, Jack W. Mauldin, Luis R. Leon
  • Patent number: 9623977
    Abstract: A hybrid structure comprises a metallic built-up sandwich structure, and a monolithic superplastic formed and diffusion bonded structure joined to the built-up sandwich structure.
    Type: Grant
    Filed: March 20, 2014
    Date of Patent: April 18, 2017
    Assignee: The Boeing Company
    Inventors: Max R. Runyan, Daniel G. Sanders, Jack W. Mauldin, Brent C. Ludwig, John M. Comfort, Larry D. Hefti, Jason F. Joel
  • Publication number: 20160193645
    Abstract: A ceramic refractory insulation block for a hot press is provided that is reinforced in a manner that reduces the likelihood of cracking and, once cracked, reduces the rate at which the crack will propagate through the ceramic refractory insulation block. The ceramic refractory insulation block includes a ceramic body defining a plurality of outer surfaces. Each of the surfaces is a planar surface. The ceramic body also defines a centerline about which the ceramic body is subjected to a bending moment. The ceramic refractory insulation body also includes a plurality of reinforcing rods extending through the ceramic body. The reinforcing rods have a greater flexural strength than the ceramic body. One or more of the plurality of reinforcing rods extend through the ceramic body on each of the opposed sides of the centerline about which the ceramic body is subjected to the bending moment.
    Type: Application
    Filed: January 6, 2015
    Publication date: July 7, 2016
    Inventors: Daniel G. Sanders, Larry D. Hefti, Mark T. Schergen, James Philp, Peter N. Comley
  • Publication number: 20150266586
    Abstract: A hybrid structure comprises a metallic built-up sandwich structure, and a monolithic superplastic formed and diffusion bonded structure joined to the built-up sandwich structure.
    Type: Application
    Filed: March 20, 2014
    Publication date: September 24, 2015
    Applicant: The Boeing Company
    Inventors: Max R. Runyan, Daniel G. Sanders, Jack W. Mauldin, Brent C. Ludwig, John M. Comfort, Larry D. Hefti, Jason F. Joel
  • Patent number: 8991683
    Abstract: A method of forming a pack in a die by superplastic formation and diffusion bonding comprises applying a forming pressure within the pack to expand the pack within the die; and supplying gas between the die and the pack to apply a back pressure around an outside of the pack while the pack is being expanded to counteract the forming pressure to reduce surface mark off.
    Type: Grant
    Filed: September 10, 2012
    Date of Patent: March 31, 2015
    Assignee: The Boeing Company
    Inventors: Daniel G. Sanders, Larry D. Hefti, Gregory L. Ramsey
  • Publication number: 20130251510
    Abstract: A propulsion system comprises a turbine engine, and an engine nacelle including an SPF/DB inner wall having a hot side face sheet against the engine and a cold side face sheet that has noise attenuation openings.
    Type: Application
    Filed: March 1, 2012
    Publication date: September 26, 2013
    Applicant: THE BOEING COMPANY
    Inventors: Max R. Runyan, Daniel G. Sanders, Larry D. Hefti, David R. Papenfuss, Jack W. Mauldin, Luis R. Leon
  • Publication number: 20130240609
    Abstract: A component is formed by welding a plurality of sheets of metal to form a blank with a number of weld nuggets, placing the blank between a die section and a lid section, heating the die section to heat the blank, and introducing a pressurized gas between the lid section and the die section to press the blank into a mold in the die section to form a component. The number of weld nuggets has a desired thickness ratio between about 1.1 to about 1.25 such that the plurality of sheets of metal and the component formed have a number of characteristics that are substantially the same.
    Type: Application
    Filed: November 12, 2009
    Publication date: September 19, 2013
    Applicant: THE BOEING COMPANY
    Inventors: Daniel G. Sanders, Luis R. Leon, Paul D. Edwards, Gregory L. Ramsey, Gary W. Coleman
  • Publication number: 20130001276
    Abstract: A method of forming a pack in a die by superplastic formation and diffusion bonding comprises applying a forming pressure within the pack to expand the pack within the die; and supplying gas between the die and the pack to apply a back pressure around an outside of the pack while the pack is being expanded to counteract the forming pressure to reduce surface mark off.
    Type: Application
    Filed: September 10, 2012
    Publication date: January 3, 2013
    Applicant: THE BOEING COMPANY
    Inventors: Daniel G. Sanders, Larry D. Hefti, Gregory L. Ramsey
  • Patent number: 8329312
    Abstract: A superplastically formed structural assembly is provided, as is an associated preform and method for forming such an assembly. The assembly includes a skin member and a support member that are joined to define a space between the members and between the joints. The assembly can be produced by joining the members in a flat configuration, and then forming the resulting preform to a predetermined shape of the structural assembly. The support member defines at least one aperture in communication with the space between the members. Thus, the skin member can be formed by delivering a pressurized fluid through the support member to the skin member, e.g., to superplastically form the skin member against a die that defines a contour surface corresponding in shape to the predetermined configuration of the assembly. The support member can extend in a substantially direct configuration between opposing portions of the skin member.
    Type: Grant
    Filed: June 27, 2011
    Date of Patent: December 11, 2012
    Assignee: The Boeing Company
    Inventors: Daniel G. Sanders, David W. Foutch, Jeff D. Will, Luis Leon, Gregory L. Ramsey, Garry A. Booker