Patent classifications
F16H2055/176
Gear housing for a planetary gear device that structurally isolates an inner gear
Separate structural units for an inner gear and a housing of a planetary gear device include an inner gear with a first raised portion formed on the outer peripheral surface of the inner gear, where the first raised portion extends towards in a direction that is inclined with respect to the axial direction of the inner gear. A housing includes a second raised portion formed on an inner peripheral surface, where the second raised portion extends in a direction that is inclined in respect to the axial direction. The housing contains the inner gear such that there is a gap formed between the inner peripheral surface of the housing and the outer peripheral surface of the inner gear. Movement of the inner gear within the interior of the housing is limited through linear contact of the first raised portion and the second raised portion.
Mounting arrangement for a gear box
A ring gear arrangement, including: a ring gear mount including: a ring gear having at least one internal gear for interaction with one or more gear wheels; a ring gear stator; and, a plurality of couplings which locate the ring gear within the gear stator, each coupling having a drive arm connected to the ring gear and a resiliently deformable connection, wherein the drive arm is movable between a first position in which the ring gear is in a rest position and a second position in which the ring gear has undergone some radial or rotational movement relative to the ring gear stator, wherein movement of the drive arm from a the first position to the second position loads the resiliently deformable connection against the ring gear, wherein the resiliently deformable connection biases the drive arm to return to the first position when in the second position.
OUTPUT RING GEAR FOR INTEGRATED DRIVE GENERATOR
An output ring gear for use in an integrated drive generator has a gear body extending between a first end and a second end and having a disc extending radially outwardly. A boss extends from the disc toward the second end. There are outer gear teeth outwardly of an outer diameter of the disc. There are inner gear teeth inwardly of an inner surface of the disc. The outer and inner gear teeth have a unique gear tooth profile with roll angles A, B, C, and D. An integrated drive generator and a method are also disclosed.
Process of forming a composition with an apparatus for mechanical exfoliation of particulate materials
Apparatus and system of components to mechanically exfoliate particulate materials using a multi-axis approach to deliver predetermined forces to a particulate material, including containers to hold particulate material and media, also including media, and, the associated parameters for operating such equipment along with methods and compositions provided by the apparatus and methods.
METHOD FOR PRODUCING A RING GEAR FOR A PLANETARY GEAR TRAIN, AND A MODULAR SYSTEM HAVING SUCH A RING GEAR
A method for producing a ring gear for a planetary gear train, wherein a continuous profile is produced by an extrusion process and the continuous profile is subsequently cut to a predetermined cutting length in order to form a ring gear body.
PLANETARY GEAR DEVICE
A planetary gear device includes a sun gear; a plurality of planetary gears; a planetary carrier at which the plurality of planetary gears are rotatably provided; and a ring gear, wherein the planetary carrier includes an oil feeding passage which feeds lubricating oil to at least one of the plurality of planetary gears, wherein the ring gear is a double helical gear in which a pair of rows of internal teeth are arranged in a direction of an axis line of the ring gear and the internal teeth of one of the rows and the internal teeth of the other of the rows are inclined in different directions, the ring gear including at least one discharge passage, wherein the at least one discharge passage includes an inlet-side portion and an outlet-side portion, the inlet-side portion being closer to an inlet configured to open in a region between the pair of rows of internal teeth at an inner peripheral surface of the ring gear, and the outlet-side portion being closer to an outlet configured to open in a region of an outer peripheral surface of the ring gear, and wherein the inlet-side portion is formed at the ring gear so that the inlet-side portion is inclined in a rotation direction of the planetary carrier, with respect to a reference line extending in a radial direction of the ring gear.
PLANETARY REDUCTION GEAR RING GEAR FOR A TURBINE ENGINE
A planetary reduction gear ring gear for a turbine engine, in particular of an aircraft, the ring gear extending about an axis (X) and including first and second coaxial annular elements and respectively two inner annular teeth oriented differently. The first and second annular elements include respectively first and second radially external annular flanges to secure the first and second elements to one another, the teeth of the first and second annular elements being axially spaced from one another and from a joint plane (P) of the first and second flanges, and defining between them an annular space externally delimited by two annular rims supporting respectively the flanges. At least one of the flanges includes joint plane notches that are substantially radial for the oil to pass through by centrifugation. The ring gear further includes an annular row of oil-retention walls protruding from the rims in the space.
Method for producing a sintered component with a toothing
A method for producing a sintered component, in particular an annular sintered component, with a toothing, having teeth with tooth roots, tooth tips and tooth flanks, includes the steps of pressing a powder to form a green compact, sintering the green compact, and hardening the sintered component, wherein after sintering, the tooth flanks and possibly the tooth tips are post-compacted and subsequently undergo post-processing by machining, and wherein a transition region between the tooth flanks and the tooth roots has an undercut design, and post-compaction of the tooth flanks is carried out only up to this transition region.
RING GEAR FOR AN AIRCRAFT MECHANICAL GEARBOX
A ring gear for an aircraft mechanical gearbox, the ring gear having an annular shape about an axis and having an internal toothing at its internal periphery, an external annular flange or splines at its external periphery, and an annular web extending between the internal toothing and the external flange or splines. The web can include an annular row of arms which are distributed about the axis, these arms connecting the internal toothing to the external flange or splines and being formed in a single piece with the internal toothing and the external flange or splines.
Gear housing for a planetary gear device that structurally isolates an inner gear
Separate structural units for an inner gear and a housing of a planetary gear device include an inner gear with a first raised portion formed on the outer peripheral surface of the inner gear, where the first raised portion extends towards in a direction that is inclined with respect to the axial direction of the inner gear. A housing includes a second raised portion formed on an inner peripheral surface, where the second raised portion extends in a direction that is inclined in respect to the axial direction. The housing contains the inner gear such that there is a gap formed between the inner peripheral surface of the housing and the outer peripheral surface of the inner gear. Movement of the inner gear within the interior of the housing is limited through linear contact of the first raised portion and the second raised portion.