Patents Assigned to SKF Aerospace France
  • Patent number: 9400013
    Abstract: A bearing liner comprising a fabric impregnated with a binder, the fabric comprising: (a) a bearing element contact surface comprising lubricating fibers and (b) structural fibers supporting the bearing element contact surface, wherein at least some of the structural fibers include a structural component and a lubricating component.
    Type: Grant
    Filed: June 12, 2015
    Date of Patent: July 26, 2016
    Assignees: AKTIEBOLAGET SKF, SKF AEROSPACE FRANCE S.A.S.
    Inventors: Andrew Bell, Michael Colton, Camille Dayot, Noemie Peron
  • Patent number: 9382945
    Abstract: A mechanical device, comprising: a bearing including a fixed ring and a pivoting ring centered on a central axis and including an interface defined therebetween; and an interface lubrication system. An acceleration field pushes the stream of lubricant from a bearing first zone to a bearing second zone, each defining an angular sector around the central axis. The lubrication system comprises a set of peripheral channels passing through the fixed ring and including first channels positioned in the first zone and defining a first intake flow rate for bringing lubricant to the interface and second channels positioned in the second zone and defining a second intake flow rate bringing lubricant to the interface. The first flow rate is higher than the second flow rate. The interface receives a larger quantity of lubricant in the first zone than in the second zone. The mechanical device can be integrated into a machine.
    Type: Grant
    Filed: December 17, 2014
    Date of Patent: July 5, 2016
    Assignee: SKF Aerospace France S.A.S
    Inventors: Thomas Doki-Thonon, Alexandre Aury, Pascal Deloeil
  • Patent number: 9261124
    Abstract: The invention relates to an angle bracket including a composite material for connecting parts. The angle bracket has two wings forming an angle along a longitudinal folding axis and coupling regions on the outside of the fold. The coupling regions attach to parts to be connected, and is associated with a securing means. At least in the longitudinal direction, the angle bracket has at least one succession of domed sections with a concave or convex profile on the inside and/or outside of the fold, providing the bracket with a corrugated form in the longitudinal direction.
    Type: Grant
    Filed: September 30, 2011
    Date of Patent: February 16, 2016
    Assignee: SKF Aerospace France
    Inventor: Jean-Michel Buchin
  • Patent number: 9259878
    Abstract: A part made of a composite is intended to be subjected, through at least a point of attachment and in cooperation with connectors, to tensile and/or compressive forces. The part includes a monolithic part having a winding of fibers oriented and embedded in a matrix, and a tubular body, wherein an attachment point, based at one end of said tubular body takes the form of a strap forming a loop turning about an axis perpendicular to the axis of the tubular body, and wherein an internal wall and/or the external wall of the loop is designed to cooperate with a portion of the connector in tension and/or in compression along one or more directions.
    Type: Grant
    Filed: July 19, 2011
    Date of Patent: February 16, 2016
    Assignee: SKF Aerospace France
    Inventor: Guy Valembois
  • Patent number: 9239077
    Abstract: A mechanical bearing having an outer ring and an inner ring, centered on a same bearing axis, the outer ring being arranged radially around the inner ring, and a cage, arranged coaxially between the inner ring and the outer ring and housing cylindrical rollers, with this cage being formed by several disjointed tubular portion which, in the assembled state of the bearing, are separated from each other by a non-zero gap. The cage is formed by at least three disjointed tubular portions that do not cooperate mechanically with each other in assembled state of the bearing.
    Type: Grant
    Filed: November 14, 2014
    Date of Patent: January 19, 2016
    Assignees: AKTIEBOLAGET, SKF AEROSPACE FRANCE S.A.S.
    Inventors: Thomas Doki-Thonon, Alexandre Aury, Pascal Deloeil
  • Publication number: 20160003293
    Abstract: A spherical plain bearing comprising an inner ring provided with a spherical outer surface and with lateral surfaces, an outer ring provided with a corresponding spherical inner surface mounted on the outer surface, and a sleeve mounted into a bore of the inner ring. The inner ring comprises at least three part rings which are mounted in contact in the circumferential direction one relative to another. At least one protrusion is provided on an outer surface of the sleeve and extends into a groove formed on the bore of the inner ring. The sleeve leaves the lateral surfaces free of the inner ring.
    Type: Application
    Filed: June 30, 2015
    Publication date: January 7, 2016
    Applicant: SKF AEROSPACE FRANCE S.A.S
    Inventors: Yvan BLACHON, Arnaud TURMEAU
  • Publication number: 20150362016
    Abstract: A bearing comprising (a) an inner ring, (b) an outer ring, and (c) a bearing liner disposed therebetween, wherein the bearing liner comprises a resin and the bearing liner has at least one of: (a) a flexural modulus of from 20 to 35 GPa and (b) a flexural strength of from 500 to 700 MPa.
    Type: Application
    Filed: June 12, 2015
    Publication date: December 17, 2015
    Applicants: SKF AEROSPACE FRANCE S.A.S, AKTIEBOLAGET SKF
    Inventors: Andrew BELL, Michael COLTON, Camille DAYOT, Noemie PERON
  • Publication number: 20150362018
    Abstract: A bearing comprising: (a) an inner ring, (b) an outer ring, and (c) a bearing liner disposed therebetween, wherein the bearing liner comprises a resin having a glass transition temperature of less than 150° C.
    Type: Application
    Filed: June 12, 2015
    Publication date: December 17, 2015
    Applicants: Aktiebolaget SKF, SKF Aerospace France S.A.S
    Inventors: Andrew BELL, Michael COLTON, Camille DAYOT, Noemie PERON
  • Publication number: 20150362017
    Abstract: A bearing liner comprising a fabric impregnated with a binder, the fabric comprising: (a) a bearing element contact surface comprising lubricating fibers and (b) structural fibers supporting the bearing element contact surface, wherein at least some of the structural fibers include a structural component and a lubricating component.
    Type: Application
    Filed: June 12, 2015
    Publication date: December 17, 2015
    Applicants: SKF AEROSPACE FRANCE S.A.S, AKTIEBOLAGET SKF
    Inventors: Andrew BELL, Michael COLTON, Camille DAYOT, Noemie PERON
  • Publication number: 20150337896
    Abstract: A spherical plain bearing comprising an inner ring having an outer spherical contact surface and an outer ring having an inner spherical contact surface. The outer spherical contact surface of the inner ring cooperates with the inner spherical contact surface of the outer ring. At least one of the inner ring and the outer ring comprises at least one internal cavity running on at least a portion of the circumference of said ring.
    Type: Application
    Filed: May 19, 2015
    Publication date: November 26, 2015
    Applicant: SKF AEROSPACE FRANCE S.A.S.
    Inventors: Camille DAYOT, Arnaud TURMEAU
  • Publication number: 20150176638
    Abstract: A device adapted to measure the wear of a ball-and-socket joint. The ball-and-socket joint comprising a first ring, which delimits a spherical housing, a second spherical ring, which is positioned concentrically in the housing of the first ring, and a lining, which is made from an elastically insulating material and is inserted between the second ring and the spherical housing of the first ring. A wear measuring feature includes at least two electrodes provided to be connected to the first ring and the second ring, respectively, or to the lining, so as to form a capacitor structure and a capacitance measuring device for measuring the capacity of the capacitor thus formed. The device further comprises an electronic circuit, which is a resonant circuit including the capacitor, an inductance and a resistance positioned in series.
    Type: Application
    Filed: December 17, 2014
    Publication date: June 25, 2015
    Applicant: SKF Aerospace France
    Inventor: Yoann HEBRARD
  • Publication number: 20150176645
    Abstract: A mechanical device, comprising: a bearing including a fixed ring and a pivoting ring centered on a central axis and including an interface defined therebetween; and an interface lubrication system. An acceleration field pushes the stream of lubricant from a bearing first zone to a bearing second zone, each defining an angular sector around the central axis. The lubrication system comprises a set of peripheral channels passing through the fixed ring and including first channels positioned in the first zone and defining a first intake flow rate for bringing lubricant to the interface and second channels positioned in the second zone and defining a second intake flow rate bringing lubricant to the interface. The first flow rate is higher than the second flow rate. The interface receives a larger quantity of lubricant in the first zone than in the second zone. The mechanical device can be integrated into a machine.
    Type: Application
    Filed: December 17, 2014
    Publication date: June 25, 2015
    Applicants: SKF AEROSPACE FRANCE, AKTIEBOLAGET SKF
    Inventors: Thomas DOKI-THONON, Alexandre AURY, Pascal DELOEIL
  • Publication number: 20150167738
    Abstract: A mechanical bearing having an outer ring and an inner ring, centred on a same bearing axis, the outer ring being arranged radially around the inner ring, and a cage, arranged coaxially between the inner ring and the outer ring and housing cylindrical rollers, with this cage being formed by several disjointed tubular portion which, in the assembled state of the bearing, are separated from each other by a non-zero gap. The cage is formed by at least three disjointed tubular portions that do not cooperate mechanically with each other in assembled state of the bearing.
    Type: Application
    Filed: November 14, 2014
    Publication date: June 18, 2015
    Applicants: SKF Aerospace France, Aktiebolaget SKF
    Inventors: Thomas Doki-Thonon, Alexandre Aury, Pascal Deloeil
  • Patent number: 8991327
    Abstract: A signaling device for signaling heating in a mechanical system susceptible to undergo contact heating during operation. The signaling device includes a body containing a thermally triggered charge generating combustion gas, ignition of the charge able to be triggered under the effect of a predetermined heat contribution, from a heating area of the body toward the charge, or under the action of an ignition command, a reservoir containing a fluid, and delivery means delivering pressurized fluid outside the reservoir through the action, directly or through an intermediate member moving in the reservoir, of the combustion gases. The signaling device also comprises at least one visual signaling element for visually signaling combustion of the charge, the visual signaling element being visible at an outer peripheral area of the signaling device after combustion of the charge. The invention also relates to a mechanical system equipped with at least one such signaling device.
    Type: Grant
    Filed: December 5, 2012
    Date of Patent: March 31, 2015
    Assignee: SKF Aerospace France
    Inventors: Herve Carrerot, Yves Maheo
  • Patent number: 8925880
    Abstract: The invention relates to an L-shaped fitting obtained after molding a composite material, including two portions defining an angle therebetween and having holes formed therein for connecting the two portions using an attachment device, and having side reinforcements in the form of brackets. At least one portion has a concave curved profile on the inner side of the fitting, and the hole(s), formed in the portion having a concave curved profile on the inner side are each formed along an axis radial to the curvature.
    Type: Grant
    Filed: December 17, 2009
    Date of Patent: January 6, 2015
    Assignee: SKF Aerospace France
    Inventor: Guy Valembois
  • Patent number: 8820172
    Abstract: A flight unit control system having at least one instrumented fastening bolt connecting an aircraft carrier structure and a load path, the instrumented bolt having at least one measurement area for detecting that the load path is under load and including a fastener for locking the instrumented bolt in a position relative to the aircraft carrier structure and load path and wherein the measurement area has two cavities and at least one strain gauge and wherein the fastener includes a plate which is positioned at a threaded end of the instrumented bolt which bears against one of the aircraft carrier structure and the load path and which extends perpendicularly to an axis of the bolt and a nut which is placed at the threaded end of the instrumented bolt to immobilize the instrumented bolt relative to the aircraft structure or the load path.
    Type: Grant
    Filed: May 5, 2011
    Date of Patent: September 2, 2014
    Assignee: SKF Aerospace France
    Inventors: Franck Bouillot, Cédric Milord
  • Patent number: 8727934
    Abstract: A reduction gear includes a stationary sun gear, a coaxial mobile sun gear, planet gears, and a planet carrier. In order to ensure easy, reliable assembly for the reduction gear, while transmitting high torques having a considerable speed reduction, the helical gear teeth of the stationary and mobile sun gears are reversed relative to one another and are mutually separated in the direction of the main axis of rotation, thus forming a free space between them, which is suitable for adjusting the axial position of the planet gear or gears when assembling the reduction gear, such as to engage the first and second gear teeth of the planet gear with the respective gear teeth of the stationary and mobile sun gears.
    Type: Grant
    Filed: January 19, 2011
    Date of Patent: May 20, 2014
    Assignee: SKF Aerospace France
    Inventor: Bastien Roussey
  • Patent number: 8690692
    Abstract: A transmission shaft for transmitting rotational movements including a tubular body having at least one tubular composite assembly including a plastic matrix and strengthening elements, at least one insert positioned at one end of the body and which is secured to the body in an interface area between the insert and the composite assembly, and at least one slug passing radially through the insert and the body for keeping the strengthening elements in place. The at least one insert has at least one recess receiving a part of the strengthening elements to maintain the strengthening elements in the interface area.
    Type: Grant
    Filed: January 11, 2012
    Date of Patent: April 8, 2014
    Assignee: SKF Aerospace France
    Inventor: Jean-Michel Buchin
  • Publication number: 20140030007
    Abstract: The ball-and-socket joint member includes an inner ring, of a general shape of revolution around a first axis, having an outer surface provided with an inner raceway, an outer ring, of a general shape of revolution around a second axis, having an inner surface provided with an outer raceway, and at least one row of balls aligned circumferentially, extending radially between the inner raceway and the outer raceway. The outer surface of the inner ring comprises a portion with a generally truncated sphere shape, forming the inner raceway. The inner surface of the outer ring comprises, for each row of balls, a groove of complementary shape to that of the balls of this row, said groove forming the outer raceway.
    Type: Application
    Filed: July 30, 2013
    Publication date: January 30, 2014
    Applicant: SKF Aerospace France
    Inventors: Gwenole Yves LE JEUNE, Yves MAHEO, Michel SENECLAUZE
  • Patent number: 8622671
    Abstract: An anti-rotation lock device for preventing movement in an assembly which includes an endpiece carrying a thread screwed into a tube together with a nut suitable for being screwed on the endpiece, the lock device including a first washer provided with an anti-rotation lock component and a second washer having at least one key and wherein the first or the second washer includes a lug, and the faces of the first and second washers are configured to adjustably lock them mutually against rotation. The device further includes a third washer which includes a member for locking the nut in rotation and an outer periphery of the third washer has a tab adapted to co-operate with the lug so as to lock the first or the second washer provided with the lug against rotation relative to the third washer.
    Type: Grant
    Filed: October 21, 2008
    Date of Patent: January 7, 2014
    Assignee: SKF Aerospace France
    Inventor: Didier Gagneur