Patents by Inventor Michael P. Renieri

Michael P. Renieri 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: 9724891
    Abstract: A beaded composite panel is fabricated using composite plies. An opening is formed in each of plies, and each ply is laid up on a bead feature and drawn down over the bead feature in the area of the opening so as to widen the opening into a gap allowing the ply to conform to the contour of the bead feature. Patches are fabricated and placed on the plies overlying over the openings. The laid-up plies are compacted and cured.
    Type: Grant
    Filed: November 25, 2014
    Date of Patent: August 8, 2017
    Assignee: THE BOEING COMPANY
    Inventors: Steven J. Burpo, Michael P. Renieri, Nicholas B. Segobiano, Neal A. Froeschner
  • Publication number: 20150079338
    Abstract: A beaded composite panel is fabricated using composite plies. An opening is formed in each of plies, and each ply is laid up on a bead feature and drawn down over the bead feature in the area of the opening so as to widen the opening into a gap allowing the ply to conform to the contour of the bead feature. Patches are fabricated and placed on the plies overlying over the openings. The laid-up plies are compacted and cured.
    Type: Application
    Filed: November 25, 2014
    Publication date: March 19, 2015
    Inventors: Steven J. Burpo, Michael P. Renieri, Nicholas B. Segobiano, Neal A. Froeschner
  • Patent number: 8916253
    Abstract: A beaded composite panel is fabricated using composite plies. An opening is formed in each of plies, and each ply is laid up on a bead feature and drawn down over the bead feature in the area of the opening so as to widen the opening into a gap allowing the ply to conform to the contour of the bead feature. Patches are fabricated and placed on the plies overlying over the openings. The laid-up plies are compacted and cured.
    Type: Grant
    Filed: August 29, 2011
    Date of Patent: December 23, 2014
    Assignee: The Boeing Company
    Inventors: Steven J. Burpo, Michael P. Renieri, Nicholas B. Segobiano, Neal A. Froeschner
  • Patent number: 8583271
    Abstract: An apparatus may comprise a nondestructive evaluation system and a cutting system. The nondestructive evaluation system may be configured to inspect a processed portion of a structure. The nondestructive evaluation system may be configured to determine whether an inconsistency is present in the processed portion. The nondestructive evaluation system may also be configured to generate information about a location of the inconsistency. The cutting system may be configured to cut a number of parts out of the processed portion of the structure in which the inconsistency may be at least substantially excluded from the number of parts.
    Type: Grant
    Filed: March 16, 2009
    Date of Patent: November 12, 2013
    Assignee: The Boeing Company
    Inventors: Roger W. Engelbart, Steven J. Burpo, Michael P. Renieri
  • Patent number: 8403586
    Abstract: A determinant assembly feature for a joint assembly and a method of assembly therefor. The joint assembly includes a structure and a web connected thereto. The structure includes a base, a pair of legs extending from the base to define a channel, and one or more location control receiving elements in either leg. The web includes a thickness control element and one or more location control elements correspondingly matched to the location control receiving elements. The method includes providing a structure comprising a base, a pair of legs extending from the base to define a channel and one or more location control receiving elements in either leg; providing a web comprising one or more location control elements and a thickness control element; and inserting the web into the structure, wherein the one or more location control elements is correspondingly matched to the one or more location control receiving elements.
    Type: Grant
    Filed: January 24, 2011
    Date of Patent: March 26, 2013
    Assignee: The Boeing Company
    Inventors: Jeffrey H. Wood, Michael P. Renieri, Thomas R. Berkel
  • Publication number: 20110311778
    Abstract: A beaded composite panel is fabricated using composite plies. An opening is formed in each of plies, and each ply is laid up on a bead feature and drawn down over the bead feature in the area of the opening so as to widen the opening into a gap allowing the ply to conform to the contour of the bead feature. Patches are fabricated and placed on the plies overlying over the openings. The laid-up plies are compacted and cured.
    Type: Application
    Filed: August 29, 2011
    Publication date: December 22, 2011
    Applicant: THE BOEING COMPANY
    Inventors: Steven J. Burpo, Michael P. Renieri, Nicholas B. Segobiano, Neal A. Froeschner
  • Patent number: 8052826
    Abstract: A beaded composite panel is fabricated using composite plies. An opening is formed in each of plies, and each ply is laid up on a bead feature and drawn down over the bead feature in the area of the opening so as to widen the opening into a gap allowing the ply to conform to the contour of the bead feature. Patches are fabricated and placed on the plies overlying over the openings. The laid-up plies are compacted and cured.
    Type: Grant
    Filed: March 24, 2009
    Date of Patent: November 8, 2011
    Assignee: The Boeing Company
    Inventors: Steven J. Burpo, Michael P. Renieri, Nicholas B. Segobiano, Neal A. Froeschner
  • Publication number: 20110123254
    Abstract: A determinant assembly feature for a joint assembly and a method of assembly therefor. The joint assembly includes a structure and a web connected thereto. The structure includes a base, a pair of legs extending from the base to define a channel, and one or more location control receiving elements in either leg. The web includes a thickness control element and one or more location control elements correspondingly matched to the location control receiving elements. The method includes providing a structure comprising a base, a pair of legs extending from the base to define a channel and one or more location control receiving elements in either leg; providing a web comprising one or more location control elements and a thickness control element; and inserting the web into the structure, wherein the one or more location control elements is correspondingly matched to the one or more location control receiving elements.
    Type: Application
    Filed: January 24, 2011
    Publication date: May 26, 2011
    Applicant: THE BOEING COMPANY
    Inventors: Jeffrey H. Wood, Michael P. Renieri, Thomas R. Berkel
  • Patent number: 7914223
    Abstract: A determinant assembly feature for a joint assembly and a method of assembly therefor. The joint assembly includes a structure and a web connected thereto. The structure includes a base, a pair of legs extending from the base to define a channel, and one or more location control receiving elements in either leg. The web includes a thickness control element and one or more location control elements correspondingly matched to the location control receiving elements. The method includes providing a structure comprising a base, a pair of legs extending from the base to define a channel and one or more location control receiving elements in either leg; providing a web comprising one or more location control elements and a thickness control element; and inserting the web into the structure, wherein the one or more location control elements is correspondingly matched to the one or more location control receiving elements.
    Type: Grant
    Filed: January 8, 2009
    Date of Patent: March 29, 2011
    Assignee: The Boeing Company
    Inventors: Jeffrey H. Wood, Michael P. Renieri, Thomas R. Berkel
  • Publication number: 20100247838
    Abstract: A beaded composite panel is fabricated using composite plies. An opening is formed in each of plies, and each ply is laid up on a bead feature and drawn down over the bead feature in the area of the opening so as to widen the opening into a gap allowing the ply to conform to the contour of the bead feature. Patches are fabricated and placed on the plies overlying over the openings. The laid-up plies are compacted and cured.
    Type: Application
    Filed: March 24, 2009
    Publication date: September 30, 2010
    Inventors: Steven J. Burpo, Michael P. Renieri, Nicholas B. Segobiano, Neal A. Froeschner
  • Publication number: 20100234977
    Abstract: An apparatus may comprise a nondestructive evaluation system and a cutting system. The nondestructive evaluation system may be configured to inspect a processed portion of a structure. The nondestructive evaluation system may be configured to determine whether an inconsistency is present in the processed portion. The nondestructive evaluation system may also be configured to generate information about a location of the inconsistency. The cutting system may be configured to cut a number of parts out of the processed portion of the structure in which the inconsistency may be at least substantially excluded from the number of parts.
    Type: Application
    Filed: March 16, 2009
    Publication date: September 16, 2010
    Applicant: THE BOEING COMPANY
    Inventors: Roger W. Engelbart, Steven J. Burpo, Michael P. Renieri
  • Publication number: 20090123225
    Abstract: A determinant assembly feature for a joint assembly and a method of assembly therefor. The joint assembly includes a structure and a web connected thereto. The structure includes a base, a pair of legs extending from the base to define a channel, and one or more location control receiving elements in either leg. The web includes a thickness control element and one or more location control elements correspondingly matched to the location control receiving elements. The method includes providing a structure comprising a base, a pair of legs extending from the base to define a channel and one or more location control receiving elements in either leg; providing a web comprising one or more location control elements and a thickness control element; and inserting the web into the structure, wherein the one or more location control elements is correspondingly matched to the one or more location control receiving elements.
    Type: Application
    Filed: January 8, 2009
    Publication date: May 14, 2009
    Inventors: JEFFREY H. WOOD, Michael P. Renieri, Thomas R. Berkel