Patents by Inventor Harold G. Erickson
Harold G. Erickson 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).
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Patent number: 11473355Abstract: A latch assembly is provided that includes a latch arm having a rotational axis and an engagement surface on a distal end of the latch arm a length from the rotational axis. The engagement surface is stowed in a stowed state of the latch arm. The latch arm is configured to receive a pushing force to depress the latch arm a predetermined distance along the rotational axis. The latch assembly also includes a turret assembly having a top end with the latch arm mounted thereon. The turret assembly is configured to, in response to the pushing force being applied to the latch arm, raise and rotate the latch arm about the rotational axis to thereby transition the latch arm from the stowed state to a deployed state in which the engagement surface is exposed.Type: GrantFiled: March 30, 2020Date of Patent: October 18, 2022Assignee: THE BOEING COMPANYInventors: Ashley Gin, Harold G. Erickson
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Publication number: 20210301570Abstract: A latch assembly is provided that includes a latch arm having a rotational axis and an engagement surface on a distal end of the latch arm a length from the rotational axis. The engagement surface is stowed in a stowed state of the latch arm. The latch arm is configured to receive a pushing force to depress the latch arm a predetermined distance along the rotational axis. The latch assembly also includes a turret assembly having a top end with the latch arm mounted thereon. The turret assembly is configured to, in response to the pushing force being applied to the latch arm, raise and rotate the latch arm about the rotational axis to thereby transition the latch arm from the stowed state to a deployed state in which the engagement surface is exposed.Type: ApplicationFiled: March 30, 2020Publication date: September 30, 2021Inventors: Ashley Gin, Harold G. Erickson
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Patent number: 9862164Abstract: Methods for manufacturing composite panels for use in the interior of an aircraft are disclosed, specifically, methods of manufacturing joggled composite panels comprising metal inserts and the resulting composite panels and inserts.Type: GrantFiled: May 11, 2015Date of Patent: January 9, 2018Assignee: The Boeing CompanyInventors: Kyle L. Gray, Nathanial C. Cuddy, Harold G. Erickson
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Publication number: 20160332412Abstract: Methods for manufacturing composite panels for use in the interior of an aircraft are disclosed, specifically, methods of manufacturing joggled composite panels comprising metal inserts and the resulting composite panels and inserts.Type: ApplicationFiled: May 11, 2015Publication date: November 17, 2016Inventors: Kyle L. Gray, Nathanial C. Cuddy, Harold G. Erickson
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Patent number: 9234536Abstract: A receptacle for a fastener is provided that may be relatively light weight and compact, may reduce the number of parts required for mounting an object to a surface, and may allow for greater flexibility in positioning the fastener. Additionally, a corresponding method for installing a receptacle and mounting an object is provided. The receptacle has an outer housing and a floating insert, and the floating insert is positioned within an internal cavity of the outer housing. A fastener may be inserted into an internal cavity of the floating insert through apertures in the outer housing and the floating insert. The floating insert is configured such that it is movable within the outer housing. As a result, the location of the aperture of the floating insert is adjustable, providing greater tolerances during the installation process.Type: GrantFiled: June 5, 2014Date of Patent: January 12, 2016Assignee: The Boeing CompanyInventors: Hoi Truong, Harold G. Erickson
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Publication number: 20140284335Abstract: A receptacle for a fastener is provided that may be relatively light weight and compact, may reduce the number of parts required for mounting an object to a surface, and may allow for greater flexibility in positioning the fastener. Additionally, a corresponding method for installing a receptacle and mounting an object is provided. The receptacle has an outer housing and a floating insert, and the floating insert is positioned within an internal cavity of the outer housing. A fastener may be inserted into an internal cavity of the floating insert through apertures in the outer housing and the floating insert. The floating insert is configured such that it is movable within the outer housing. As a result, the location of the aperture of the floating insert is adjustable, providing greater tolerances during the installation process.Type: ApplicationFiled: June 5, 2014Publication date: September 25, 2014Inventors: Hoi Truong, Harold G. Erickson
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Patent number: 8733701Abstract: An attachment assembly for securing a secondary door to a mating structure may include a door frame and at least one telescoping structural pin disposable within a side of the door frame. The structural pin may be extendable from a retracted position to a deployed position into the mating structure.Type: GrantFiled: August 2, 2012Date of Patent: May 27, 2014Assignee: The Boeing CompanyInventors: Harold G. Erickson, Rolando G. Taguinod
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Publication number: 20120292447Abstract: An attachment assembly for securing a secondary door to a mating structure may include a door frame and at least one telescoping structural pin disposable within a side of the door frame. The structural pin may be extendable from a retracted position to a deployed position into the mating structure.Type: ApplicationFiled: August 2, 2012Publication date: November 22, 2012Applicant: THE BOEING COMPANYInventors: Harold G. Erickson, Rolando G. Taguinod
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Patent number: 8286917Abstract: An attachment assembly may be adapted for securing a panel member such as a class divider or a secondary door to a mating structure. The attachment assembly comprises at least one structural pin configured to be extendable from a retracted position to a deployed position. The attachment assembly may include a base support configured to be placed in overlapping contact with the panel member. The attachment assembly may include a primary support configured to be mountable such as in overlapping contact to the base support and having at least one sleeve sized and configured to receive the structural pin which is telescopically movable. A locking mechanism such as a quick release pin may be inserted through bores formed in the sleeve and in the structural pin to prevent axial movement of the structural pin relative to the sleeve.Type: GrantFiled: May 11, 2008Date of Patent: October 16, 2012Assignee: The Boeing CompanyInventors: Harold G. Erickson, Rolando G. Taguinod
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Patent number: 8191829Abstract: An apparatus comprising an elongate planar member, a number of flanges, and a number of channels at ends of the number of flanges. The elongate planar member may have a first side, a second side, and a number of holes. The first side may be opposite to the second side, wherein the first side may be capable of being secured to a track having a substantially planar surface with an array of holes. The number of flanges may extend from the second side of the elongate planar member. Each channel in the number of channels may have a bottom, a first wall, and a second wall. The first wall may have a first lip, and the second wall may have a second lip, wherein the first lip and the second lip may extend towards a centerline of an associated channel in the number of channels.Type: GrantFiled: November 12, 2008Date of Patent: June 5, 2012Assignee: The Boeing CompanyInventors: Harold G. Erickson, Edward L. Cepurna
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Patent number: 8136328Abstract: A panel includes a core and a fastener receptacle extending into the core. The fastener receptacle has an internal hollow and an opening to the internal hollow. The opening is formed by a lip that can engage and structurally support a push-in fastener.Type: GrantFiled: May 28, 2008Date of Patent: March 20, 2012Assignee: The Boeing CompanyInventors: Harold G. Erickson, Douglas A. Brown
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Publication number: 20110062735Abstract: In one embodiment, a kickstrip assembly comprises a base plate having a length extending along a longitudinal axis, and comprising an upper segment having an upper edge and an upper lip, a lower segment having a lower edge and a lower lip, the upper lip and the lower lip defining a middle section. The assembly further comprises an insert formed from a flexible polymeric material and comprising a faceplate, an upper edge depending from the faceplate, and a lower edge depending from the faceplate, wherein the faceplate is dimensioned to fit within middle section of the base plate.Type: ApplicationFiled: September 15, 2009Publication date: March 17, 2011Inventors: Harold G. Erickson, Paul T. Bridgeman, Bryan A. Branscome, Bobbie L. Cole, Gregory W. Nelson, Mark W. Whalon
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Publication number: 20100116933Abstract: An apparatus comprising an elongate planar member, a number of flanges, and a number of channels at ends of the number of flanges. The elongate planar member may have a first side, a second side, and a number of holes. The first side may be opposite to the second side, wherein the first side may be capable of being secured to a track having a substantially planar surface with an array of holes. The number of flanges may extend from the second side of the elongate planar member. Each channel in the number of channels may have a bottom, a first wall, and a second wall. The first wall may have a first lip, and the second wall may have a second lip, wherein the first lip and the second lip may extend towards a centerline of an associated channel in the number of channels.Type: ApplicationFiled: November 12, 2008Publication date: May 13, 2010Inventors: Harold G. Erickson, Edward L. Cepurna
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Publication number: 20090321574Abstract: An attachment assembly may be adapted for securing a panel member such as a class divider or a secondary door to a mating structure. The attachment assembly comprises at least one structural pin configured to be extendable from a retracted position to a deployed position. The attachment assembly may include a base support configured to be placed in overlapping contact with the panel member. The attachment assembly may include a primary support configured to be mountable such as in overlapping contact to the base support and having at least one sleeve sized and configured to receive the structural pin which is telescopically movable. A locking mechanism such as a quick release pin may be inserted through bores formed in the sleeve and in the structural pin to prevent axial movement of the structural pin relative to the sleeve.Type: ApplicationFiled: May 11, 2008Publication date: December 31, 2009Applicant: THE BOEING COMPANYInventors: Harold G. Erickson, Rolando G. Taguinod
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Publication number: 20090293421Abstract: A panel includes a core and a fastener receptacle extending into the core. The fastener receptacle has an internal hollow and an opening to the internal hollow. The opening is formed by a lip that can engage and structurally support a push-in fastener.Type: ApplicationFiled: May 28, 2008Publication date: December 3, 2009Applicant: THE BOEING COMPANYInventors: Harold G. Erickson, Douglas A. Brown
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Publication number: 20080116094Abstract: A receptacle for a fastener is provided that may be relatively light weight and compact, may reduce the number of parts required for mounting an object to a surface, and may allow for greater flexibility in positioning the fastener. Additionally, a corresponding method for installing a receptacle and mounting an object is provided. The receptacle has an outer housing and a floating insert, and the floating insert is positioned within an internal cavity of the outer housing. A fastener may be inserted into an internal cavity of the floating insert through apertures in the outer housing and the floating insert. The floating insert is configured such that it is movable within the outer housing. As a result, the location of the aperture of the floating insert is adjustable, providing greater tolerances during the installation process.Type: ApplicationFiled: November 17, 2006Publication date: May 22, 2008Inventors: Hoi Truong, Harold G. Erickson
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Patent number: D603173Type: GrantFiled: December 13, 2007Date of Patent: November 3, 2009Assignee: The Boeing CompanyInventors: Christopher Samhammer, Harold G. Erickson
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Patent number: D613954Type: GrantFiled: August 17, 2009Date of Patent: April 20, 2010Assignee: The Boeing CompanyInventors: Christopher Samhammer, Harold G. Erickson