Patents by Inventor Sven R. Lofstrom

Sven R. Lofstrom 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: 11932381
    Abstract: According to an aspect, a method of assembling a mandrel includes assembling a plurality of members via interlocking features arranged at opposing edges of each member of the plurality of members to form a compartment, the assembled members having a collective outer surface that conforms to an inner surface of the spar. A support member is inserted into the compartment formed radially inward from the assembled members, the support member making contact with a portion of each member of the plurality of members.
    Type: Grant
    Filed: April 17, 2023
    Date of Patent: March 19, 2024
    Assignee: LOCKHEED MARTIN CORPORATION
    Inventors: Eric Dunn, Keith M. Schenone, Sven R. Lofstrom
  • Publication number: 20230249809
    Abstract: According to an aspect, a method of assembling a mandrel includes assembling a plurality of members via interlocking features arranged at opposing edges of each member of the plurality of members to form a compartment, the assembled members having a collective outer surface that conforms to an inner surface of the spar. A support member is inserted into the compartment formed radially inward from the assembled members, the support member making contact with a portion of each member of the plurality of members.
    Type: Application
    Filed: April 17, 2023
    Publication date: August 10, 2023
    Applicant: LOCKHEED MARTIN CORPORATION
    Inventors: Eric Dunn, Keith M. Schenone, Sven R. Lofstrom
  • Patent number: 11655052
    Abstract: A system for regenerating fastener holes in a replacement tip section of a rotor blade includes a first fixture, a second fixture, and a third fixture positionable adjacent a tip section of the rotor blade. The first fixture is used to verify a position of an opening formed in the spar. The second fixture includes a removable bushing having a drillable opening. The drillable opening is aligned with the at least one opening formed in the spar and defines at least one hole to be formed in the replacement tip section. The third fixture includes a countersink opening. The countersink opening is aligned with the at least one hole to be formed in the replacement tip section and the at least one opening formed in the spar to define a countersink feature to be formed in the at least one hole.
    Type: Grant
    Filed: June 22, 2021
    Date of Patent: May 23, 2023
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Sven R. Lofstrom, Robert D. Higbie, Frank M. Caputo, Ryan Lehto, Timothy James Conti, Eric Charles Boyle
  • Patent number: 11649042
    Abstract: According to an aspect, a method of assembling a mandrel includes assembling a plurality of members via interlocking features arranged at opposing edges of each member of the plurality of members to form a compartment, the assembled members having a collective outer surface that conforms to an inner surface of the spar. A support member is inserted into the compartment formed radially inward from the assembled members, the support member making contact with a portion of each member of the plurality of members.
    Type: Grant
    Filed: July 14, 2020
    Date of Patent: May 16, 2023
    Assignee: LOCKHEED MARTIN CORPORATION
    Inventors: Eric Dunn, Keith M. Schenone, Sven R. Lofstrom
  • Patent number: 11548103
    Abstract: A pressure tool for rotor blade repair including a mobile support system including a support surface, a first bladder support assembly including a first inflatable bladder fixedly mounted to the support surface, a second bladder support assembly including a second inflatable bladder pivotally mounted relative to the support surface, and an activation mechanism operatively coupled to the second bladder support assembly. The activation mechanism is operable to selectively shift the second bladder support assembly relative to the first bladder support assembly. A fluid delivery system is operable to direct a fluid into each of the first inflatable bladder and the second inflatable bladder.
    Type: Grant
    Filed: October 20, 2020
    Date of Patent: January 10, 2023
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Ryan Lehto, David W. Littlejohn, Sven R. Lofstrom
  • Publication number: 20220194571
    Abstract: A method of mounting a replacement tip section to an exposed end of a rotor blade includes removing an existing tip section from the rotor blade to create the exposed end of the rotor blade, installing the rotor blade having the exposed end onto a holding fixture, assembling the replacement tip section about the exposed end of the rotor blade, positioning a bonding fixture about the replacement tip section, and curing the replacement tip section to the exposed end of the rotor blade.
    Type: Application
    Filed: December 30, 2021
    Publication date: June 23, 2022
    Applicant: Sikorsky Aircraft Corporation
    Inventors: Joseph Pantalone, III, Timothy James Conti, Frank M. Caputo, Sven R. Lofstrom, Keith M. Schenone, Robert D. Higbie, Eric Charles Boyle, Alicia Fernandez
  • Patent number: 11242140
    Abstract: A method of mounting a replacement tip section to an exposed end of a rotor blade includes removing an existing tip section from the rotor blade to create the exposed end of the rotor blade, installing the rotor blade having the exposed end onto a holding fixture, assembling the replacement tip section about the exposed end of the rotor blade, positioning a bonding fixture about the replacement tip section, and curing the replacement tip section to the exposed end of the rotor blade.
    Type: Grant
    Filed: August 10, 2018
    Date of Patent: February 8, 2022
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Joseph Pantalone, III, Timothy James Conti, Frank M. Caputo, Sven R. Lofstrom, Keith M. Schenone, Robert D. Higbie, Eric Charles Boyle, Alicia Fernandez
  • Publication number: 20220017215
    Abstract: According to an aspect, a method of assembling a mandrel includes assembling a plurality of members via interlocking features arranged at opposing edges of each member of the plurality of members to form a compartment, the assembled members having a collective outer surface that conforms to an inner surface of the spar. A support member is inserted into the compartment formed radially inward from the assembled members, the support member making contact with a portion of each member of the plurality of members.
    Type: Application
    Filed: July 14, 2020
    Publication date: January 20, 2022
    Inventors: Eric Dunn, Keith M. Schenone, Sven R. Lofstrom
  • Publication number: 20210309390
    Abstract: A system for regenerating fastener holes in a replacement tip section of a rotor blade includes a first fixture, a second fixture, and a third fixture positionable adjacent a tip section of the rotor blade. The first fixture is used to verify a position of an opening formed in the spar. The second fixture includes a removable bushing having a drillable opening. The drillable opening is aligned with the at least one opening formed in the spar and defines at least one hole to be formed in the replacement tip section. The third fixture includes a countersink opening. The countersink opening is aligned with the at least one hole to be formed in the replacement tip section and the at least one opening formed in the spar to define a countersink feature to be formed in the at least one hole.
    Type: Application
    Filed: June 22, 2021
    Publication date: October 7, 2021
    Applicant: Sikorsky Aircraft Corporation
    Inventors: Sven R. Lofstrom, Robert D. Higbie, Frank M. Caputo, Ryan Lehto, Timothy James Conti, Eric Charles Boyle
  • Patent number: 11091254
    Abstract: A rotor blade disassembly method includes applying spanwise support to a rotor blade body and heating a bond disposed on an end of the rotor blade body. The method also includes removing the spanwise support from the rotor blade body and exerting shear stress on the bond using weight of the rotor blade body. A blade disassembly system is also described.
    Type: Grant
    Filed: December 21, 2018
    Date of Patent: August 17, 2021
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Ryan Lehto, Eric C. Boyle, Sven R. Lofstrom, David Littlejohn
  • Patent number: 11066188
    Abstract: A system for regenerating fastener holes in a replacement tip section of a rotor blade includes a first fixture, a second fixture, and a third fixture positionable adjacent a tip section of the rotor blade. The first fixture is used to verify a position of an opening formed in the spar. The second fixture includes a removable bushing having a drillable opening. The drillable opening is aligned with the at least one opening formed in the spar and defines at least one hole to be formed in the replacement tip section. The third fixture includes a countersink opening. The countersink opening is aligned with the at least one hole to be formed in the replacement tip section and the at least one opening formed in the spar to define a countersink feature to be formed in the at least one hole.
    Type: Grant
    Filed: August 10, 2018
    Date of Patent: July 20, 2021
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Sven R. Lofstrom, Robert D. Higbie, Frank M. Caputo, Ryan Lehto, Timothy James Conti, Eric Charles Boyle
  • Publication number: 20210046591
    Abstract: A pressure tool for rotor blade repair including a mobile support system including a support surface, a first bladder support assembly including a first inflatable bladder fixedly mounted to the support surface, a second bladder support assembly including a second inflatable bladder pivotally mounted relative to the support surface, and an activation mechanism operatively coupled to the second bladder support assembly. The activation mechanism is operable to selectively shift the second bladder support assembly relative to the first bladder support assembly. A fluid delivery system is operable to direct a fluid into each of the first inflatable bladder and the second inflatable bladder.
    Type: Application
    Filed: October 20, 2020
    Publication date: February 18, 2021
    Applicant: Sikorsky Aircraft Corporation
    Inventors: Ryan Lehto, David W. Littlejohn, Sven R. Lofstrom
  • Patent number: 10836001
    Abstract: A pressure tool for rotor blade repair including a mobile support system including a support surface, a first bladder support assembly including a first inflatable bladder fixedly mounted to the support surface, a second bladder support assembly including a second inflatable bladder pivotally mounted relative to the support surface, and an activation mechanism operatively coupled to the second bladder support assembly. The activation mechanism is operable to selectively shift the second bladder support assembly relative to the first bladder support assembly. A fluid delivery system is operable to direct a fluid into each of the first inflatable bladder and the second inflatable bladder.
    Type: Grant
    Filed: July 7, 2017
    Date of Patent: November 17, 2020
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Ryan Lehto, David W. Littlejohn, Sven R. Lofstrom
  • Patent number: 10730201
    Abstract: A tool for machining chamfers includes a tool body defining a first reference and a second reference configured for proper positioning of the tool body on a workpiece. A router port is defined through the tool body to provide access to the workpiece for a router. A router attachment proximate the router port is configured to position a router mounted to the router attachment for machining a chamfer in the workpiece with reference to the first and second references.
    Type: Grant
    Filed: October 3, 2016
    Date of Patent: August 4, 2020
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Sven R. Lofstrom, Ryan Lehto, Joshua Richards
  • Publication number: 20200047919
    Abstract: A system for regenerating fastener holes in a replacement tip section of a rotor blade includes a first fixture, a second fixture, and a third fixture positionable adjacent a tip section of the rotor blade. The first fixture is used to verify a position of an opening formed in the spar. The second fixture includes a removable bushing having a drillable opening. The drillable opening is aligned with the at least one opening formed in the spar and defines at least one hole to be formed in the replacement tip section. The third fixture includes a countersink opening. The countersink opening is aligned with the at least one hole to be formed in the replacement tip section and the at least one opening formed in the spar to define a countersink feature to be formed in the at least one hole.
    Type: Application
    Filed: August 10, 2018
    Publication date: February 13, 2020
    Inventors: Sven R. Lofstrom, Robert D. Higbie, Frank M. Caputo, Ryan Lehto, Timothy James Conti, Eric Charles Boyle
  • Publication number: 20200047878
    Abstract: A method of mounting a replacement tip section to an exposed end of a rotor blade includes removing an existing tip section from the rotor blade to create the exposed end of the rotor blade, installing the rotor blade having the exposed end onto a holding fixture, assembling the replacement tip section about the exposed end of the rotor blade, positioning a bonding fixture about the replacement tip section, and curing the replacement tip section to the exposed end of the rotor blade.
    Type: Application
    Filed: August 10, 2018
    Publication date: February 13, 2020
    Inventors: Joseph Pantalone, III, Timothy James Conti, Frank M. Caputo, Sven R. Lofstrom, Keith M. Schenone, Robert D. Higbie, Eric Charles Boyle, Alicia Fernandez
  • Patent number: 10518395
    Abstract: A cuff-blade attachment bushing removal tool system includes an alignment plate comprising alignment holes defined through the alignment plate in a pattern of a plurality of bushing holes of a blade root, a bladder plate connected to the alignment plate, and a bladder positioned on the bladder plate such that a gap is formed between the bladder and the alignment plate to receive a blade root to align the alignment holes and the bushing holes of the blade root, wherein the bladder is transitionable between an uninflated position where the blade root can be inserted into the gap and an inflated position where the blade root is clamped between the bladder and the alignment plate.
    Type: Grant
    Filed: January 14, 2019
    Date of Patent: December 31, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Scott O. Smith, Sven R. Lofstrom, Philip Petering
  • Patent number: 10457422
    Abstract: A method and apparatus for securing a rotor blade is disclosed. The apparatus includes a base and an offset member configured to maintain the base at a selected distance from a set point. A clamping member is supported by the base and is receptive of the rotor blade at a selected location of the rotor blade, wherein the rotor blade is positioned against the set point. A slidable component supports the clamping member and slides the clamping member within the base to the selected location of the rotor blade. The free end of the clam shell assembly can be secured to a support beam that raises the clam shell assembly and rotor blade from the base for immersion testing.
    Type: Grant
    Filed: December 7, 2016
    Date of Patent: October 29, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: David W. Littlejohn, Sven R. Lofstrom, Scott O. Smith
  • Publication number: 20190143497
    Abstract: A cuff-blade attachment bushing removal tool system includes an alignment plate comprising alignment holes defined through the alignment plate in a pattern of a plurality of bushing holes of a blade root, a bladder plate connected to the alignment plate, and a bladder positioned on the bladder plate such that a gap is formed between the bladder and the alignment plate to receive a blade root to align the alignment holes and the bushing holes of the blade root, wherein the bladder is transitionable between an uninflated position where the blade root can be inserted into the gap and an inflated position where the blade root is clamped between the bladder and the alignment plate.
    Type: Application
    Filed: January 14, 2019
    Publication date: May 16, 2019
    Inventors: Scott O. Smith, Sven R. Lofstrom, Philip Petering
  • Publication number: 20190135421
    Abstract: A rotor blade disassembly method includes applying spanwise support to a rotor blade body and heating a bond disposed on an end of the rotor blade body. The method also includes removing the spanwise support from the rotor blade body and exerting shear stress on the bond using weight of the rotor blade body. A blade disassembly system is also described.
    Type: Application
    Filed: December 21, 2018
    Publication date: May 9, 2019
    Inventors: Ryan Lehto, Eric C. Boyle, Sven R. Lofstrom, David Littlejohn