Patents by Inventor Michael M. Stepan

Michael M. Stepan 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: 9266687
    Abstract: Systems and methods for delivery of device along a transport path are provided. One system includes a transport tube having a feed end and a point of use end and a plurality of device carriers operable to move through the transport tube from the feed end to the point of use end. The plurality of device carriers has a common external surface for operation in the transport tube to allow transport through the transport tube. At least some of the plurality of device carriers has a different internal configuration than at least some of other ones of the plurality of device carriers, wherein the internal configuration is determined based on at least one physical characteristic of a device to be inserted therein.
    Type: Grant
    Filed: June 24, 2013
    Date of Patent: February 23, 2016
    Assignee: The Boeing Company
    Inventors: Michael M. Stepan, Darrell Darwin Jones, Kenneth Paul Zaballos
  • Publication number: 20140377018
    Abstract: Systems and methods for delivery of device along a transport path are provided. One system includes a transport tube having a feed end and a point of use end and a plurality of device carriers operable to move through the transport tube from the feed end to the point of use end. The plurality of device carriers has a common external surface for operation in the transport tube to allow transport through the transport tube. At least some of the plurality of device carriers has a different internal configuration than at least some of other ones of the plurality of device carriers, wherein the internal configuration is determined based on at least one physical characteristic of a device to be inserted therein.
    Type: Application
    Filed: June 24, 2013
    Publication date: December 25, 2014
    Inventors: Michael M. STEPAN, Darrell Darwin JONES, Kenneth ZABALLOS
  • Patent number: 8464434
    Abstract: A method and apparatus for measuring diameters of holes and countersinks. A tip of a countersink measurement system may be moved to engage a countersink for a hole. A diameter of the countersink may be measured in response to the tip of the countersink measurement system engaging the countersink. A probe may be moved through the tip of the countersink measurement system into a channel for the hole, while the tip is engaged with the countersink. A number of diameters for the channel may be measured as the probe moves in the hole.
    Type: Grant
    Filed: September 15, 2010
    Date of Patent: June 18, 2013
    Assignee: The Boeing Company
    Inventors: Paul G. Kostenick, Dario I. Valenzuela, James Niemann Buttrick, Arlen Ray Pumphrey, Michael M. Stepan
  • Patent number: 8136475
    Abstract: A painting apparatus for applying a coating material to a member surface of a member comprises a housing, at least one slide rail, a rack assembly, a cross beam and a spraying device. The slide rail may be mountable within the housing and may have a plurality of rack positions. The rack assembly is mountable within the housing at one of the rack positions. The rack assembly is configured to support the member such that the member surface is exposed. The cross beam may be coupled to the slide rail. The cross beam is movable along the slide rail and is positionable at the rack positions. The spraying device is mountable on the cross beam and is configured to move along the cross beam while spraying the coating material onto the member surface.
    Type: Grant
    Filed: January 6, 2009
    Date of Patent: March 20, 2012
    Assignee: The Boeing Company
    Inventors: Bruce R. Davis, Michael M. Stepan
  • Publication number: 20100173090
    Abstract: A painting apparatus for applying a coating material to a member surface of a member comprises a housing, at least one slide rail, a rack assembly, a cross beam and a spraying device. The slide rail may be mountable within the housing and may have a plurality of rack positions. The rack assembly is mountable within the housing at one of the rack positions. The rack assembly is configured to support the member such that the member surface is exposed. The cross beam may be coupled to the slide rail. The cross beam is movable along the slide rail and is positionable at the rack positions. The spraying device is mountable on the cross beam and is configured to move along the cross beam while spraying the coating material onto the member surface.
    Type: Application
    Filed: January 6, 2009
    Publication date: July 8, 2010
    Applicant: THE BOEING COMPANY
    Inventors: Bruce R. Davis, Michael M. Stepan
  • Patent number: 7126096
    Abstract: Rib and spar webs are joined in a composite wingbox to eliminate fasteners by welding the webs along bondlines defined by overlapping sections of the webs. Heat to produce the weld is generally achieved resistively by connecting a multistrip susceptor positioned along the bond line to a current source, since the geometry makes it difficult to heat these web joints inductively. The wingbox is completed without fasteners by welding skins to the rib-spar wingbox.
    Type: Grant
    Filed: June 6, 1995
    Date of Patent: October 24, 2006
    Assignee: Th Boeing Company
    Inventors: Marc R. Matsen, Douglas A. McCarville, Michael M. Stepan
  • Patent number: 6722447
    Abstract: A power feed apparatus for applying a thrust force to an output shaft of a motor driven tool to drive the output shaft linearly towards and away from a workpiece without applying off-axis forces to the output shaft that would cause it to move out of perfect perpendicular alignment to the outer surface of the workpiece. The apparatus includes a first tubular member which is fixedly secured to a jig or other like mounting structure associated with the workpiece. A second tubular member is disposed for sliding linear movement along the first tubular member. Spaced apart annular fluid chambers are formed within the apparatus along with associated fluid ports for allowing a pressurized fluid to be used to both extend and retract the output shaft of the tool. The tool itself is supported on the second tubular member and thus moves linearly along with the second tubular member.
    Type: Grant
    Filed: May 1, 2002
    Date of Patent: April 20, 2004
    Assignee: The Boeing Company
    Inventors: Michael M. Stepan, Roger A. Gage
  • Publication number: 20030205394
    Abstract: A power feed apparatus for applying a thrust force to an output shaft of a motor driven tool to drive the output shaft linearly towards and away from a workpiece without applying off-axis forces to the output shaft that would cause it to move out of perfect perpendicular alignment to the outer surface of the workpiece. The apparatus includes a first tubular member which is fixedly secured to a jig or other like mounting structure associated with the workpiece. A second tubular member is disposed for sliding linear movement along the first tubular member. Spaced apart annular fluid chambers are formed within the apparatus along with associated fluid ports for allowing a pressurized fluid to be used to both extend and retract the output shaft of the tool. The tool itself is supported on the second tubular member and thus moves linearly along with the second tubular member.
    Type: Application
    Filed: May 1, 2002
    Publication date: November 6, 2003
    Inventors: Michael M. Stepan, Roger A. Gage
  • Patent number: 5847375
    Abstract: Rib and spar webs are joined in a composite wingbox to eliminate fasteners by welding the webs along bond lines defined by overlapping sections of the webs. Heat to produce the weld is generally achieved resistively by connecting a multistrip susceptor positioned along the bond line to a current source, since the geometry makes it difficult to heat these web joints inductively. The wingbox is completed without fasteners by welding skins to the rib-spar wingbox.
    Type: Grant
    Filed: July 19, 1996
    Date of Patent: December 8, 1998
    Assignee: The Boeing Company
    Inventors: Marc R. Matsen, Douglas A. McCarville, Michael M. Stepan
  • Patent number: 5829716
    Abstract: A hybrid metal webbed composite beam includes a metal I or T web section and a composite cap formed over and adhered to the I or T web. The beam incorporates the advantages of metals and composites in modern aerospace construction allowing thermoplastic welding of the beam to skins while having the strength of metal.
    Type: Grant
    Filed: June 7, 1995
    Date of Patent: November 3, 1998
    Assignee: The Boeing Company
    Inventors: Brad L. Kirkwood, Michael M. Stepan, Paul J. Patt
  • Patent number: 5752789
    Abstract: The invention provides a unique approach to solving a peck feeding problem in limited access areas restricting the drilling unit size. It uses a power transmission system which is comprised of a pinion gear driven by a motor source. The pinion gear drives a bevel gear that is free to travel along a polygon quill. A quill had is located on one end of the quill to house the drill. The opposing quill end is attached to a guide bushing assembly. The guide bushing assembly is connected to a bell crank mechanism that is actuated and controlled by a pneumatic piston and hydraulic speed control system. The power transmission system, and the pneumatic power transfer system combined produce a pecking cycle for drilling precision holes within a confined set-up space of 5.5 inches in a preferred embodiment. It preferably has a drill stroke up to 1 inch deep, and is capable of producing a "pecking" action which is unique for right angle drilling equipment in limited access applications.
    Type: Grant
    Filed: December 15, 1995
    Date of Patent: May 19, 1998
    Assignee: The Boeing Company
    Inventor: Michael M. Stepan
  • Patent number: 5688426
    Abstract: A hybrid metal webbed composite beam includes a metal I or T web section and a composite cap formed over and adhered to the I or T web. The beam incorporates advantages of metals and composites in modern aerospace construction allowing thermoplastic welding of the beam to skins while having the strength of metal.
    Type: Grant
    Filed: June 7, 1995
    Date of Patent: November 18, 1997
    Assignee: The Boeing Company
    Inventors: Brad L. Kirkwood, Michael M. Stepan, Paul J. Patt
  • Patent number: 5556565
    Abstract: A hybrid metal webbed composite beam includes a metal I or T web section and a composite cap formed over and adhered to the I or T web. The beam incorporates the advantages of metals and composites in modern aerospace construction allowing thermoplastic welding of the beam to skins while having the strength of metal.
    Type: Grant
    Filed: June 7, 1995
    Date of Patent: September 17, 1996
    Assignee: The Boeing Company
    Inventors: Brad L. Kirkwood, Michael M. Stepan, Paul J. Patt