Patent classifications
F16C2226/12
Blind boss ball socket assembly
A ball socket assembly is provided that includes a ball socket having a socket base with a plurality of socket legs extending therefrom, the socket legs include ball stud interface surfaces forming a ball cavity for receiving and selectively engaging a ball head of a ball stud, a plurality of slots extending between the plurality of socket legs, a lower abutment wall having a bend line and situated in the socket base, and a flexible securing substrate positioned under the lower abutment wall, the socket assembly further including a mating boss substrate having a first boss inner passage with a first passage inside diameter, a second boss inner passage having a second passage inside diameter, wherein the first passage inside diameter is greater than the second passage inside diameter, a boss transition wall between the first boss inner passage and the second boss inner passage, and a boss bottom.
FIBER REINFORCED BEARING FOR A BALL SOCKET ASSEMBLY, BALL SOCKET ASSEMBLY THEREWITH AND METHODS OF CONSTRUCTION THEREOF
A ball socket assembly, bearing therefor, and method of construction thereof are provided. The ball socket assembly includes a housing with an inner bore extending between a closed first end region and an open second end region. A fiber-reinforced bearing is disposed in the inner bore. The bearing has a lower portion presenting a lower bearing surface having a first radius of curvature and an upper portion presenting an upper bearing surface having a second radius of curvature that is greater than the first radius of curvature. The lower bearing surface and the upper bearing surface surround a ball cavity in which a spherical ball portion of a ball stud is disposed. The housing second end region is plastically deformed radially inwardly to impart a bias on the bearing upper portion to fix the bearing and the ball portion in the housing. The bias causes the second radius of curvature to be biased substantially equal to the first radius of curvature.
Composite shaft
A composite shaft with an end fitting mounted on one end of said shaft and a preload structure arranged to provide a biasing force to bias the composite shaft against the end fitting. The end fitting has a first interface surface, the first interface surface being tapered at an angle to the shaft axis and the shaft has a second interface surface for engagement with the first interface surface and is tapered at an angle to the shaft axis, the second interface surface extending axially from a first end to a second end, the shaft being thicker at the second end than at the first end. The shaft has a third interface surface and the preload structure has a fourth interface surface and the contact pressure of the third interface against the fourth interface increases from the first end of the shaft to the second end of the shaft.
STAKING ASSEMBLY, STAKING ASSEMBLY MANUFACTURING METHOD, HUB UNIT BEARING, HUB UNIT BEARING MANUFACTURING METHOD, AUTOMOBILE, AND AUTOMOBILE MANUFACTURING METHOD
Axial relative movement of an auxiliary member (30) and a hub body (22z) is performed, the hub body (22z) and an inner race (21) are combined with each other in an axial direction, and a part of the hub body (22z) deformed by a blade (33) of the auxiliary member (30) is disposed inside an engagement concave portion (26) of the inner race (21).
ROTATING ASSEMBLY, IN PARTICULAR FOR GUIDING A MOTOR VEHICLE WHEEL
A motor vehicle drive wheel assembly comprising a fixed subassembly comprising two outer raceways; and, a rotating subassembly comprising a first inner race, a second inner race and two rows of balls arranged in two pitch planes PP1 and PP2. The second inner bearing race has an outer diameter, measured in a section plane perpendicular to the axis of rotation and located between the first pitch plane and the second pitch plane, at a measurement distance DM of the first pitch plane, which is greater than a given threshold value VS.
GEAR TRAIN JOINT
A bearing support for a turbocharger, the bearing support including a body, a bore extending axially through the body and dimensioned to receive a bearing and a portion of a planet carrier, and a plurality of pilots. Each pilot may be formed on an external surface of the body, and each pilot may be machined for an interference fit with a different component of the turbocharger.
SEAL FOR TAPER ROLLER BEARING AND TAPER ROLLER BEARING ASSEMBLY
The invention provides a seal for a taper roller bearing. The seal includes: a frame having: an outer flange, extending radially outward, an inner flange, extending radially inward, an middle flange, located between the outer flange and the inner flange and extending in an axial direction. The outer flange, the inner flange and the middle flange are integrally formed; a sealing ring, at least connects and covers the radial outer side of the outer flange of the frame, and has at least one sealing lip extending outward in the radial direction. The invention also provides an assembly for a taper roller bear, which provides a taper roller bearing. An inn ring of that taper roller bearing has a shoulder with a large flange; and a seal as described above. The middle flange is in interference fit with the outer circumferential surface of the shoulder, and the inner flange presses against and covers at least a part of the large flange.
ANTI-FRICTION BEARING COMPRISING A DISCHARGING DEVICE, AND METHOD FOR THE DISCHARGE OF ELECTROSTATIC CHARGES
A roller bearing including a conduction apparatus and a method for conducting electrostatic charges at a roller bearing, the conduction apparatus including at least one elastic conductor having a first conductor section and a second conductor section for forming a contact assembly on the roller bearing, the first conductor section being mounted on a first bearing ring of the roller bearing and the second conductor section being mounted on a second bearing ring of the roller bearing, an electrically conductive connection being established between the first bearing ring and the second bearing ring. The conductor is supported at the first bearing ring, the first conductor section being inserted into at least a straight recess of the first bearing ring.
AIR BEARING-CORRUGATED THRUST BEARING DISC
A thrust disc for an aircraft and methods of making and using the thrust disc are provided. The thrust disc includes a planar body, and a region unitarily formed from a portion of the body, wherein the region has a plurality of sides defining the region on the planar body, wherein the region has a textured feature, and wherein a subset of the plurality of sides are cut and at least one of the plurality of sides is integrally connected to the body.
Socket Assembly And Method Of Making A Socket Assembly
The socket assembly includes a housing with an inner bore that extends from a wall at a closed end to an open end. A ball stud is received in the inner bore, and a shank portion of the ball stud projects out through the open end. A backing bearing is movably disposed in the inner bore. The backing bearing presents a bearing surface which is in sliding contact with a ball portion of the ball stud. An exit bearing is locked into a fixed position within the inner bore and has another bearing surface which is in sliding contact with the ball portion. A spring is positioned between the wall and the backing bearing and imparts a preload force against the backing bearing. The wall is deformed to preload the spring against the backing bearing and reduce clearances between components in the socket assembly.