Patents by Inventor Carl Ray

Carl Ray 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: 20150123432
    Abstract: Surgeons everywhere have to stand erect for very long periods of time, whether that be for an entire day of surgeries or for a single, complicated surgery, many of whom develop their own muscular-skeletal disorders. Most if not all Surgeons suffer from chronic back, cervical, lumbar, and neck pain due to their unforgiving postures while performing surgeries and especially during lengthy surgeries. Their arms are often times extended, which multiplies and exacerbates this problem as well as their head, neck and upper body, all of which tax the spinal cord and muscular support systems. Nothing else, no other device or supporting structure exists in this space, market and surgical suite. This invention takes the load off the surgeon and puts the load onto a mechanical device and places the surgeon into the best possible posture and comfort for which to conduct surgery and rest his own body while performing the surgery. It is a whole body ergonomic system for Surgeons.
    Type: Application
    Filed: October 14, 2014
    Publication date: May 7, 2015
    Inventor: Robert Carl Ray
  • Patent number: 8974217
    Abstract: A method and support apparatus for providing structural support to a mold or mandrel, such as a shape memory polymer (SMP) apparatus configured for shaping a composite part. The support apparatus may comprise a rigid structural member and a plurality of SMP cells attached thereto and configured to inflate or deploy in a malleable state toward and against a surface of the SMP apparatus, mold, or mandrel. Then the SMP cells may be returned to a rigid state while still pressed against this surface, thereby providing structural support when composite material is applied to an opposite surface of the SMP apparatus, mold, or mandrel. After the composite material is cured into the finished composite part, the SMP cells may be deflated or otherwise collapse toward the structural member to provide enough clearance to be removed from the cured composite part.
    Type: Grant
    Filed: September 27, 2011
    Date of Patent: March 10, 2015
    Assignee: Spirit AeroSystems, Inc.
    Inventors: Joel James Everhart, Bryan Michael Pelley, David E Havens, Steven Fillmore Hanson, Jeffrey W. Priest, Carl Ray Fiegenbaum
  • Patent number: 8951375
    Abstract: A method and apparatus for fabricating a composite part, such as a fuselage or internal stiffener, with a shape memory polymer (SMP) apparatus usable as both a rigid lay-up tool and a bladder. The SMP apparatus may be heated until malleable, shaped, and then cooled in a desired rigid tool configuration. For example, cavities may be formed into the SMP apparatus for nesting components therein to co-bond or co-cure with the composite part. Next, composite material may be applied onto the SMP apparatus and then placed into a rigid external tool and heated to composite cure temperatures at which the SMP apparatus is malleable. A pressure differential may be induced which urges the SMP apparatus to compress the composite material against the rigid external tool. When the composite material is cured, the SMP apparatus may be urged away from the cured composite material and removed from within the composite part.
    Type: Grant
    Filed: September 21, 2011
    Date of Patent: February 10, 2015
    Assignee: Spirit AeroSystems, Inc.
    Inventors: David E. Havens, Matthew C. Everhart, Randy Rex Kysar, Carl Ray Fiegenbaum, Jeffrey W. Priest, Delbert Leon Strelow, Kevin John Ford, Kristin Dru Pickell
  • Patent number: 8945325
    Abstract: A method and apparatus for fabricating a composite part, such as a fuselage or internal stiffener, with a shape memory polymer (SMP) apparatus usable as a rigid lay-up tool. The SMP apparatus may be heated until malleable, shaped, and then cooled in a desired rigid tool configuration. For example, cavities may be formed into the SMP apparatus for nesting components therein to co-bond or co-cure with the composite part. The composite material and/or nested components may be heated and compressed against the SMP apparatus. The SMP apparatus may be configured to remain rigid during the composite cure cycle. Once the composite material is cured, the SMP apparatus may be triggered to a malleable state and urged away from the cured composite material.
    Type: Grant
    Filed: September 21, 2011
    Date of Patent: February 3, 2015
    Assignee: Spirit AreoSystems, Inc.
    Inventors: Matthew C. Everhart, David E. Havens, Randy Rex Kysar, Carl Ray Fiegenbaum, Jeffrey W. Priest, Delbert Leon Strelow, Kodi Elizabeth Ann Caster
  • Publication number: 20150027029
    Abstract: A waterfowl decoy animation device comprising a frame having a first elongated frame member and a second elongated frame member configured in a cruciform configuration, a first pulley wheel rotatably attached to a first end of the first frame member, a second pulley wheel rotatably attached to a second end of the first frame member, a third pulley wheel rotatably attached to a first end of the second frame member, and a fourth pulley wheel rotatably attached to a second end of the second frame member; a drive motor operatively associated with one of the pulley wheels; a drive belt around the pulley wheels; an electric source operatively associated with the drive motor; and at least one waterfowl decoy attached to the drive belt.
    Type: Application
    Filed: April 18, 2014
    Publication date: January 29, 2015
    Inventor: Carl Ray Mager
  • Patent number: 8877114
    Abstract: A method and apparatus for removing a SMP apparatus from within a cured composite part. The method may comprise the steps of triggering the SMP apparatus from a rigid state to a malleable state, inducing a pressure differential that drives the SMP apparatus, in the malleable state, away from the cured composite part and toward an inner mandrel tool, and removing the inner mandrel tool with the SMP apparatus resting thereon out of the cured composite part. The inner mandrel tool may comprise an outer surface having varying contours such that a surface area of the outer surface is great enough to prevent the SMP apparatus from folding over onto itself or creasing when driven toward the inner mandrel tool. A maximum straight line distance between points on the outer surface may be small enough to allow the inner mandrel tool clearance for removal from the cured composite part.
    Type: Grant
    Filed: September 21, 2011
    Date of Patent: November 4, 2014
    Assignee: Spirit Aerosystems, Inc.
    Inventors: David E. Havens, Matthew C. Everhart, Kristin Marie Cable, Eric W. Traxler, Carl Ray Fiegenbaum, Jeffrey W. Priest, Kodi Elizabeth Ann Caster
  • Patent number: 8821475
    Abstract: A method for delivering a target volume of fluid to a destination is provided. The method includes delivering a first volume of fluid to the destination in increments each having approximately a first incremental volume, the first volume of fluid being less than the target volume and delivering a second volume of fluid to the destination in increments each having approximately a second incremental volume, the second incremental volume being less than the first incremental volume, such that the sum of the first volume and the second volume is approximately equal to the target volume.
    Type: Grant
    Filed: October 29, 2007
    Date of Patent: September 2, 2014
    Assignee: DEKA Products Limited Partnership
    Inventors: Carl Ray Distler, Gregory Lee Distler, Jason A. Demers, Geoffrey Spencer, Robert Bryant
  • Patent number: 8815145
    Abstract: A method and apparatus for fabricating a composite part with a shape memory polymer (SMP) apparatus usable as both a rigid tool and as a bladder. The SMP apparatus may be heated until malleable, shaped, and then cooled in a desired rigid tool configuration. The composite material may be applied onto the SMP apparatus and then placed into a rigid external mold and heated to composite cure temperatures at which the SMP apparatus is malleable. In some embodiments, an impermeable sheet of material may also be placed over portions of the composite material to compress it against the SMP apparatus. A pressure differential may be induced which urges the SMP apparatus to compress the composite material against the rigid external mold. When the composite material is cured, the pressure differential may be equalized and/or reversed and the malleable SMP apparatus may be removed from within the composite part.
    Type: Grant
    Filed: September 21, 2011
    Date of Patent: August 26, 2014
    Assignee: Spirit AeroSystems, Inc.
    Inventors: Matthew C. Everhart, David E. Havens, Joel James Everhart, Randy Rex Kysar, Carl Ray Fiegenbaum, Jeffrey W. Priest, Kevin John Ford, Delbert Leon Strelow
  • Patent number: 8734703
    Abstract: A method and apparatus for fabricating a composite part with a shape memory polymer (SMP) apparatus usable as both a rigid lay-up tool and as a bladder. The SMP apparatus may be heated until malleable, shaped, and then cooled in a desired rigid tool configuration. For example, cavities may be formed into the SMP apparatus for nesting components therein to co-bond or co-cure with the composite part. The composite material may be applied onto the SMP apparatus in the rigid tool configuration and then placed into a rigid external tool and heated to composite cure temperatures at which the SMP apparatus is malleable. A pressure differential may be induced which urges the SMP apparatus to compress the composite material against the rigid external tool. When the composite material is cured, the SMP apparatus may be urged away from the cure composite material and removed from within the composite part.
    Type: Grant
    Filed: September 21, 2011
    Date of Patent: May 27, 2014
    Assignee: Spirit AeroSystems, Inc.
    Inventors: David E. Havens, Matthew C. Everhart, Thomas Wood Margraf, Joel James Everhart, Randy Rex Kysar, Carl Ray Fiegenbaum, Jeffrey W. Priest, Delbert Leon Strelow, Kristin Dru Pickell
  • Publication number: 20140093909
    Abstract: The present invention is directed to a pre-coated substrate, such as a slide, that is useful for immobilizing a sample. The invention is further provides methods of preparing such pre-coated substrates and methods of analyzing biological samples immobilized on such pre-coated substrate. The substrate is coated with a polycationic polymeric coating material specifically selected such that that coated substrate exhibits increased stability and prolonged shelf-life. Preferred polymeric coating materials include allylic or vinylic polymers having cationic groups thereon and having no more than a small percentage of peptidic monomeric linkages, particularly polydiallyldimethylammonium (PDDA).
    Type: Application
    Filed: December 12, 2013
    Publication date: April 3, 2014
    Applicant: TriPath Imaging, Inc.
    Inventors: William A. Fox, William Carl Ray, III
  • Patent number: 8617895
    Abstract: The present invention is directed to a pre-coated substrate, such as a slide, that is useful for immobilizing a sample. The invention is further provides methods of preparing such pre-coated substrates and methods of analyzing biological samples immobilized on such pre-coated substrate. The substrate is coated with a polycationic polymeric coating material specifically selected such that that coated substrate exhibits increased stability and prolonged shelf-life. Preferred polymeric coating materials include allylic or vinylic polymers having cationic groups thereon and having no more than a small percentage of peptidic monomeric linkages, particularly polydiallyldimethylammonium (PDDA).
    Type: Grant
    Filed: September 22, 2005
    Date of Patent: December 31, 2013
    Assignee: Tripath Imaging, Inc.
    Inventors: William Alan Fox, William Carl Ray, III
  • Patent number: 8608890
    Abstract: A method and support apparatus for providing structural support to a mold or mandrel, such as a shape memory polymer (SMP) apparatus configured for shaping a composite part. The support apparatus may comprise a rigid structural member and a plurality of SMP cells attached thereto and configured to inflate or deploy in a malleable state toward and against a surface of the SMP apparatus, mold, or mandrel. Then the SMP cells may be returned to a rigid state while still pressed against this surface, thereby providing structural support when composite material is applied to an opposite surface of the SMP apparatus, mold, or mandrel. After the composite material is cured into the finished composite part, the SMP cells may be deflated or otherwise collapse toward the structural member to provide enough clearance to be removed from the cured composite part.
    Type: Grant
    Filed: September 27, 2011
    Date of Patent: December 17, 2013
    Assignee: Spirit AeroSystems, Inc.
    Inventors: Joel James Everhart, David E. Havens, Steven Fillmore Hanson, Jeffrey W. Priest, Carl Ray Fiegenbaum, Thomas Joseph Barnell
  • Publication number: 20120288655
    Abstract: A method and apparatus for fabricating a composite part with a shape memory polymer (SMP) apparatus usable as both a rigid lay-up tool and as a bladder. The SMP apparatus may be heated until malleable, shaped, and then cooled in a desired rigid tool configuration. For example, cavities may be formed into the SMP apparatus for nesting components therein to co-bond or co-cure with the composite part. The composite material may be applied onto the SMP apparatus in the rigid tool configuration and then placed into a rigid external tool and heated to composite cure temperatures at which the SMP apparatus is malleable. A pressure differential may be induced which urges the SMP apparatus to compress the composite material against the rigid external tool. When the composite material is cured, the SMP apparatus may be urged away from the cure composite material and removed from within the composite part.
    Type: Application
    Filed: September 21, 2011
    Publication date: November 15, 2012
    Applicant: Spirit AeroSystems, Inc.
    Inventors: David E. Havens, Matthew C. Everhart, Thomas Wood Margraf, Joel James Everhart, Randy Rex Kysar, Carl Ray Fiegenbaum, Jeffrey W. Priest, Delbert Leon Strelow, Kristin Dru Pickell
  • Publication number: 20120286457
    Abstract: A method and apparatus for fabricating a composite part with a shape memory polymer (SMP) apparatus usable as both a rigid tool and as a bladder. The SMP apparatus may be heated until malleable, shaped, and then cooled in a desired rigid tool configuration. The composite material may be applied onto the SMP apparatus and then placed into a rigid external mold and heated to composite cure temperatures at which the SMP apparatus is malleable. In some embodiments, an impermeable sheet of material may also be placed over portions of the composite material to compress it against the SMP apparatus. A pressure differential may be induced which urges the SMP apparatus to compress the composite material against the rigid external mold. When the composite material is cured, the pressure differential may be equalized and/or reversed and the malleable SMP apparatus may be removed from within the composite part.
    Type: Application
    Filed: September 21, 2011
    Publication date: November 15, 2012
    Applicant: SPIRIT AEROSYSTEMS, INC.
    Inventors: Matthew C. Everhart, David E. Havens, Joel James Everhart, Randy Rex Kysar, Carl Ray Fiegenbaum, Jeffrey W. Priest, Kevin John Ford, Delbert Leon Strelow
  • Publication number: 20120119417
    Abstract: A method and support apparatus for providing structural support to a mold or mandrel, such as a shape memory polymer (SMP) apparatus configured for shaping a composite part. The support apparatus may comprise a rigid structural member and a plurality of SMP cells attached thereto and configured to inflate or deploy in a malleable state toward and against a surface of the SMP apparatus, mold, or mandrel. Then the SMP cells may be returned to a rigid state while still pressed against this surface, thereby providing structural support when composite material is applied to an opposite surface of the SMP apparatus, mold, or mandrel. After the composite material is cured into the finished composite part, the SMP cells may be deflated or otherwise collapse toward the structural member to provide enough clearance to be removed from the cured composite part.
    Type: Application
    Filed: September 27, 2011
    Publication date: May 17, 2012
    Applicant: SPIRIT AEROSYSTEMS, INC.
    Inventors: Joel James Everhart, Bryan Michael Pelley, David E. Havens, Steven Fillmore Hanson, Jeffrey W. Priest, Carl Ray Fiegenbaum
  • Publication number: 20120118486
    Abstract: A method and apparatus for fabricating a composite part, such as a fuselage or internal stiffener, with a shape memory polymer (SMP) apparatus usable as a rigid lay-up tool. The SMP apparatus may be heated until malleable, shaped, and then cooled in a desired rigid tool configuration. For example, cavities may be formed into the SMP apparatus for nesting components therein to co-bond or co-cure with the composite part. The composite material and/or nested components may be heated and compressed against the SMP apparatus. The SMP apparatus may be configured to remain rigid during the composite cure cycle. Once the composite material is cured, the SMP apparatus may be triggered to a malleable state and urged away from the cured composite material.
    Type: Application
    Filed: September 21, 2011
    Publication date: May 17, 2012
    Applicant: SPIRIT AEROSYSTEMS, INC.
    Inventors: Matthew C. Everhart, David E. Havens, Randy Rex Kysar, Carl Ray Fiegenbaum, Jeffrey W. Priest, Delbert Leon Strelow, Kodi Elizabeth Ann Caster
  • Publication number: 20120119416
    Abstract: A method and support apparatus for providing structural support to a mold or mandrel, such as a shape memory polymer (SMP) apparatus configured for shaping a composite part. The support apparatus may comprise a rigid structural member and a plurality of SMP cells attached thereto and configured to inflate or deploy in a malleable state toward and against a surface of the SMP apparatus, mold, or mandrel. Then the SMP cells may be returned to a rigid state while still pressed against this surface, thereby providing structural support when composite material is applied to an opposite surface of the SMP apparatus, mold, or mandrel. After the composite material is cured into the finished composite part, the SMP cells may be deflated or otherwise collapse toward the structural member to provide enough clearance to be removed from the cured composite part.
    Type: Application
    Filed: September 27, 2011
    Publication date: May 17, 2012
    Applicant: SPIRIT AEROSYSTEMS, INC.
    Inventors: Scott Robert Huelskamp, Joel James Everhart, David E. Havens, Steven Fillmore Hanson, Jeffrey W. Priest, Carl Ray Fiegenbaum
  • Publication number: 20120118491
    Abstract: A method and support apparatus for providing structural support to a mold or mandrel, such as a shape memory polymer (SMP) apparatus configured for shaping a composite part. The support apparatus may comprise a rigid structural member and a plurality of SMP cells attached thereto and configured to inflate or deploy in a malleable state toward and against a surface of the SMP apparatus, mold, or mandrel. Then the SMP cells may be returned to a rigid state while still pressed against this surface, thereby providing structural support when composite material is applied to an opposite surface of the SMP apparatus, mold, or mandrel. After the composite material is cured into the finished composite part, the SMP cells may be deflated or otherwise collapse toward the structural member to provide enough clearance to be removed from the cured composite part.
    Type: Application
    Filed: September 27, 2011
    Publication date: May 17, 2012
    Applicant: SPIRIT AEROSYSTEMS, INC.
    Inventors: Joel James Everhart, David E. Havens, Steven Fillmore Hanson, Jeffrey W. Priest, Carl Ray Fiegenbaum
  • Publication number: 20120118487
    Abstract: A method and apparatus for fabricating a composite part, such as a fuselage or internal stiffener, with a shape memory polymer (SMP) apparatus usable as both a rigid lay-up tool and a bladder. The SMP apparatus may be heated until malleable, shaped, and then cooled in a desired rigid tool configuration. For example, cavities may be formed into the SMP apparatus for nesting components therein to co-bond or co-cure with the composite part. Next, composite material may be applied onto the SMP apparatus and then placed into a rigid external tool and heated to composite cure temperatures at which the SMP apparatus is malleable. A pressure differential may be induced which urges the SMP apparatus to compress the composite material against the rigid external tool. When the composite material is cured, the SMP apparatus may be urged away from the cured composite material and removed from within the composite part.
    Type: Application
    Filed: September 21, 2011
    Publication date: May 17, 2012
    Applicant: SPIRIT AEROSYSTEMS, INC.
    Inventors: David E. Havens, Matthew C. Everhart, Randy Rex Kysar, Carl Ray Fiegenbaum, Jeffrey W. Priest, Delbert Leon Strelow, Kevin John Ford, Kristin Dru Pickell
  • Publication number: 20120119412
    Abstract: A method and apparatus for removing a SMP apparatus from within a cured composite part. The method may comprise the steps of triggering the SMP apparatus from a rigid state to a malleable state, inducing a pressure differential that drives the SMP apparatus, in the malleable state, away from the cured composite part and toward an inner mandrel tool, and removing the inner mandrel tool with the SMP apparatus resting thereon out of the cured composite part. The inner mandrel tool may comprise an outer surface having varying contours such that a surface area of the outer surface is great enough to prevent the SMP apparatus from folding over onto itself or creasing when driven toward the inner mandrel tool. A maximum straight line distance between points on the outer surface may be small enough to allow the inner mandrel tool clearance for removal from the cured composite part.
    Type: Application
    Filed: September 21, 2011
    Publication date: May 17, 2012
    Applicant: SPIRIT AEROSYSTEMS, INC.
    Inventors: David E. Havens, Matthew C. Everhart, Kristin Marie Cable, Eric W. Traxler, Carl Ray Fiegenbaum, Jeffrey W. Priest, Kodi Elizabeth Ann Caster