Patents by Inventor Guy PAILHORIES

Guy PAILHORIES 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: 11156246
    Abstract: A rivet may include a pin comprising: a threaded portion (36), a shank (38) and a head (40); and a bushing (32) comprising an essentially cylindrical body, said body comprising a deformation zone designed to form an external bulge (80); a collar (70) designed to receive the head of the pin; and a tapped portion (66) designed to engage with the threaded portion of the pin. The shank (38) of the pin comprises a first cylindrical portion (44) and a second cylindrical portion (46) connected by a shoulder (48), the first portion being adjacent to the head and having a first diameter, the second portion being adjacent to the threaded portion and having a second, smaller diameter.
    Type: Grant
    Filed: July 3, 2017
    Date of Patent: October 26, 2021
    Assignee: LISI AEROSPACE
    Inventors: Guy Pailhories, Olivier Gay
  • Patent number: 11111943
    Abstract: A nut (32) for assembling elements of a structure comprises a collar (64) capable of coming into contact with a front face of the structure; a tightening zone having an outer diameter (86) capable of being inserted into a hole of the structure; a deformation zone adjacent to the tightening zone and capable of forming a bulge against a rear face of the structure, opposite the front face; and a tapped portion (65) adjacent to the deformation zone. The nut may include grooving (82) on an outer circumference of at least one part of the deformation zone, a maximum diameter of said grooving (82) being less than or equal to the outer diameter (86) of the tightening zone.
    Type: Grant
    Filed: October 12, 2018
    Date of Patent: September 7, 2021
    Assignee: LISI AEROSPACE
    Inventors: Loic Meiffre, Guy Pailhories, Christophe Vandaele
  • Patent number: 10690167
    Abstract: The invention concerns a fastener used to attach structural components that have aligned perforations with a nominal diameter (D), where the fastener comprises a minimum grip plane (Gmin) and a maximum grip plane (Gmax), and A screw (12) comprising an enlarged head and a threaded portion (22); A sleeve (30) comprising an enlarged head, a cylindrical tubular body and a tapped portion (36) that engages the threaded portion (22) of the screw, where the tapped portion (36) is adjacent to an internally smooth portion of the body (34) of the sleeve. This smooth portion has a thickness (E), a non-deformable area (A) adjacent to the head of the sleeve and a deformable area (B) adjacent the non-deformable area (A). The sleeve's deformable area (B) can be deformed into a bulb (48) intended to come into contact with a blind side (46) of the structural components.
    Type: Grant
    Filed: June 10, 2016
    Date of Patent: June 23, 2020
    Assignee: LISI AEROSPACE
    Inventors: Antoine Villet, Nicolas Naretto, Olivier Gay, Guy Pailhories
  • Publication number: 20190186522
    Abstract: A rivet may include a pin comprising: a threaded portion (36), a shank (38) and a head (40); and a bushing (32) comprising an essentially cylindrical body, said body comprising a deformation zone designed to form an external bulge (80); a collar (70) designed to receive the head of the pin; and a tapped portion (66) designed to engage with the threaded portion of the pin. The shank (38) of the pin comprises a first cylindrical portion (44) and a second cylindrical portion (46) connected by a shoulder (48), the first portion being adjacent to the head and having a first diameter, the second portion being adjacent to the threaded portion and having a second, smaller diameter.
    Type: Application
    Filed: July 3, 2017
    Publication date: June 20, 2019
    Applicant: LISI AEROSPACE
    Inventors: Guy Pailhories, Olivier Gay
  • Publication number: 20190113063
    Abstract: The present invention relates to a nut (32) for assembling elements of a structure, said nut comprising: a collar (64) capable of coming into contact with a front face of the structure; a tightening zone having an outer diameter (86) capable of being inserted into a hole of the structure; a deformation zone adjacent to the tightening zone and capable of forming a bulge against a rear face of the structure, opposite the front face; and a tapped portion (65) adjacent to the deformation zone. The nut comprises grooving (82) on an outer circumference of at least one part of the deformation zone, a maximum diameter of said grooving (82) being less than or equal to the outer diameter (86) of the tightening zone.
    Type: Application
    Filed: October 12, 2018
    Publication date: April 18, 2019
    Applicant: LISI AEROSPACE
    Inventors: Loic MEIFFRE, Guy PAILHORIES, Christophe VANDAELE
  • Publication number: 20180238372
    Abstract: The invention concerns a fastener used to attach structural components that have aligned perforations with a nominal diameter (D), where the fastener comprises a minimum grip plane (Gmin) and a maximum grip plane (Gmax), and A screw (12) comprising an enlarged head and a threaded portion (22); A sleeve (30) comprising an enlarged head, a cylindrical tubular body and a tapped portion (36) that engages the threaded portion (22) of the screw, where the tapped portion (36) is adjacent to an internally smooth portion of the body (34) of the sleeve. This smooth portion has a thickness (E), a non-deformable area (A) adjacent to the head of the sleeve and a deformable area (B) adjacent the non-deformable area (A). The sleeve's deformable area (B) can be deformed into a bulb (48) intended to come into contact with a blind side (46) of the structural components.
    Type: Application
    Filed: June 10, 2016
    Publication date: August 23, 2018
    Applicant: LISI AEROSPACE
    Inventors: Antoine Villet, Nicolas Naretto, Olivier Gay, Guy Pailhories
  • Patent number: 9845822
    Abstract: A fastening bolt has a threaded screw (11) with a terminal portion (18) whose diameter (19) is less than that of the threaded portion, and an end surface (21) of said terminal portion has a transverse opening groove (22). The fastening bolt also has a nut (30) comprising a threaded body (32) and an unthreaded crown (34) drilled with at least two holes (35) diametrically opposite to one another and a rod (23), able to fit in the groove of the screw and in the two lateral holes of the nut to lock the bolt. The body of the nut comprises a driving portion (38), as well as a cylindrical portion (39) less thick than the driving portion, and the cylindrical portion (39) of the nut has an elliptical deformation that was previously a circular shape.
    Type: Grant
    Filed: April 28, 2014
    Date of Patent: December 19, 2017
    Assignee: LISI AEROSPACE
    Inventor: Guy Pailhories
  • Patent number: 9669457
    Abstract: A rivet for blind fastening may include a screw with a handling element, a break groove, a head separated from the handling element by the break groove, and a threaded part. The rivet may also include a sleeve with a collar and a tubular shank having an internal thread intended to come into engagement with the threaded part of the screw. The handling element includes a first handling portion able to guide introduction of the rivet in a setting tool, and a second handling portion able to transmit a torque, the two handling portions being separated by a blocking portion able to limit an axial movement of the rivet in a setting tool. A setting nose may be used for installing such a rivet, and the rivet, setting nose and a setting method can be used in the assembly of aircraft structures.
    Type: Grant
    Filed: January 14, 2015
    Date of Patent: June 6, 2017
    Assignee: LISI Aerospace
    Inventors: Frederic Bigot, Jerome Couderc, Olivier Gay, Guy Pailhories
  • Publication number: 20160177985
    Abstract: The invention relates to a securing device (10) for a structure (11) having an open-ended cylindrical bore (13a), the securing device comprising: an insert (15) comprising a tapped tubular body (16) and a head (18), the extremity (20) of the body opposite the head comprising an annular cavity holding a ring (21) made of a plastic material; a pin (22) comprising a cylindrical tapped rod (16) assembled with the tapping of the insert and a head (23), the extremity (30) of the cylindrical threaded rod being tapered; the device being characterized in that the threaded rod is introduced into the insert on the ring side such that, in the assembled state, the head of the insert and the head of the pin form the terminal ends of the securing device (10). The invention also relates to an assembly for the installation of such a device, and also to an installation method.
    Type: Application
    Filed: July 31, 2014
    Publication date: June 23, 2016
    Applicant: LISI AEROSPACE
    Inventors: Guy Pailhories, Yoann Douard
  • Publication number: 20160076579
    Abstract: The invention relates to a fastening bolt (10) comprising: A screw (11), said screw having a threaded portion (17) and a terminal portion (18) whose diameter (19) is less than that of the threaded portion, an end surface (21) of said terminal portion comprising a transverse opening groove (22); A nut (30) comprising a threaded body (32) and an unthreaded crown (34) drilled with at least two holes (35) diametrically opposite to one another; A rod (23), able to fit in the groove of the screw and in the two lateral holes of the nut to lock the bolt; the threaded rod of the nut comprises a driving portion (38), as well as a chimney (34) less thick than the driving portion; the nut comes from a method comprising an elliptical deformation of the chimney previously in a circular shape.
    Type: Application
    Filed: April 28, 2014
    Publication date: March 17, 2016
    Inventor: Guy Pailhories
  • Publication number: 20150196951
    Abstract: A rivet for blind fastening may include a screw with a handling element, a break groove, a head separated from the handling element by the break groove, and a threaded part; a sleeve with a collar and a tubular shank comprising an internal thread intended to come into engagement with the threaded part of the screw. The handling element comprises a first handling portion able to guide the introduction of the rivet in a setting tool, and a second handling portion able to transmit a torque, the two handling portions being separated by blocking portion able to limit an axial movement of the rivet in a setting tool. A setting nose for installing such a rivet, and a setting method are also described. These in particular are applicable to the assembly of aircraft structures.
    Type: Application
    Filed: January 14, 2015
    Publication date: July 16, 2015
    Applicant: LISI AEROSPACE
    Inventors: Frederic BIGOT, Jerome COUDERC, Olivier GAY, Guy PAILHORIES