A bearing includes a bearing pad for supporting a rotary component and a housing attached to or formed integrally with the bearing pad. The housing includes a flexible column extending towards the bearing pad for providing the bearing pad with an airflow. The column supports the bearing pad from a location inward of an outer periphery of the bearing pad along an axial direction of the bearing. With such a configuration, a resistance of the bearing pad along a radial direction of the bearing is less at the outer periphery than a resistance of the bearing pad along the radial direction proximate the column.

In an embodiment, in a sliding component, a sliding face S at least one sliding part of a pair of sliding parts is provided with positive pressure generation mechanisms 10 which generate dynamic pressure, an annular pressure release groove 11, and radial grooves 12 which intersect the pressure release groove 11, in which corners 13a and 13b at an intersecting portion of the pressure release groove 11 and the radial grooves 12 are each formed in a curved surface shape such that the pressure release groove 11 and the radial groove 12 are joined by a smooth curved surface. The sliding component can prevent generation of cavitation in a pressure release groove and a radial groove without setting depths of the grooves to be deeper than necessary.

The present disclosure is directed to a bearing assembly for a gas turbine engine. The bearing assembly includes a bearing housing and a bearing pad for supporting a rotary component of the gas turbine engine. The bearing pad includes at least one gas inlet and a plurality of gas outlets configured on an inner surface thereof. The gas inlet is in fluid communication with the plurality of gas outlets via a gas distribution labyrinth. Further, the gas distribution labyrinth includes a plurality of passageways configured to evenly distribute pressurized gas entering the gas inlet to an interface between the inner surface of the bearing pad and an outer diameter of the rotary component.

A hybrid dynamic pressure gas radial bearing, which comprises a bearing outer sleeve, an inner sleeve and a foil type elastic part arranged between the bearing outer sleeve and the inner sleeve, the outer circumferential face and the left and right end faces of the bearing inner sleeve are respectively provided with regular groove-type patterns, and the groove-type patterns in one end face is in mirror symmetry with the groove-type pattern in the other end face, and the axial contour lines of the groove-type patterns in the outer circumference face and the radial contour lines of the groove-type patterns in the left and right end faces are in one-to-one correspondence and are connected with each other, has the rigidity characteristic of the high-limit rotating speed of the radial bearing of the groove-type dynamic pressure gas.

A hybrid dynamic pressure gas thrust bearing, comprises two outer discs, an inner disc clamped between the two outer discs, and foil type elastic parts arranged between each outer disc and the inner disc; and the two end faces of the inner disc are respectively provided with regular groove-type patterns, and the groove-type pattern in one end face is in mirror symmetry with the groove-type pattern in the other end face. The hybrid dynamic pressure gas thrust provided by the invention has the rigidity characteristic of the high-limit rotating speed of the groove-type dynamic pressure gas thrust bearing, and has the flexible characteristic of the high impact resistance and the load capacity of the foil type dynamic pressure gas thrust bearing, it can meet the application of dynamic pressure gas thrust bearings in ultra high-speed areas under larger loads.

A bearing includes a bearing pad for supporting a rotary component and a housing attached to or formed integrally with the bearing pad. The housing includes a flexible column extending towards the bearing pad for providing the bearing pad with an airflow. The column supports the bearing pad from a location inward of an outer periphery of the bearing pad along an axial direction of the bearing. With such a configuration, a resistance of the bearing pad along a radial direction of the bearing is less at the outer periphery than a resistance of the bearing pad along the radial direction proximate the column.

Provided is a foil air bearing having a herringbone pattern to sustain a load of a rotor rotating in a predetermined rotation direction around a center line, the foil air bearing including an upper top foil disposed to face a surface of the rotor, a middle top foil disposed under the upper top foil, a lower top foil disposed under the middle top foil, a bump foil provided as an elastically deformable member and disposed under the lower top foil, and a plurality of slots provided as holes penetrating from an upper surface to a lower surface of the middle top foil, and extending along a lengthwise direction forming a predetermined angle with a rotation direction of the rotor, wherein the upper top foil is deformed in a downward concave shape at locations corresponding to the slots due to air pressure generated by rotation of the rotor.

An annular sliding component is one of two sliding rings that rotate relative to each other and partition a sealed fluid space and a leakage space, the sliding component includes a dynamic pressure generating groove that generates a dynamic pressure, and includes an inclined groove which extends from the leakage space toward the sealed fluid space with an inclination in a forward rotation direction and has a first dynamic pressure generating end portion and a reverse groove which extends from a backward rotation direction side of the inclined groove in a backward rotation direction and has a second dynamic pressure generating end portion.

An aerodynamic bearing for axial and/or radial mounting of a shaft for a turbocompressor extending along an axis of rotation, wherein the aerodynamic bearing has a first bearing part denotable as a rotor, and a second bearing part denotable as a stator with respect to which the first bearing part is rotatable about the axis of rotation. The first bearing part and/or the second bearing part have a bearing surface facing the respective other bearing part and on which an air cushion for aerodynamic mounting is generatable between the bearing parts. The bearing surface has a plurality of depressions, each following a predetermined longitudinal profile on the bearing surface and arranged to form a predetermined pattern. The depressions each have, over their respective longitudinal profiles on the bearing surface, a varying depth which is determined by a depth profile restricted to a predetermined number of depth levels.

An aerodynamic bearing for axial and/or radial mounting of a shaft for a turbocompressor, wherein the aerodynamic bearing has a first bearing part denotable as a rotor, and a second bearing part denotable as a stator. The first bearing part and/or the second bearing part have a bearing surface facing the respective other bearing part and on which a gas cushion for aerodynamic mounting is generatable between the bearing parts. The bearing surface has a plurality of depressions, each following a predetermined longitudinal profile on the bearing surface and arranged to form a predetermined pattern. The longitudinal profile has two sections which merge into one another at an apex located on an apex line which is displaced in parallel with respect to a center line of the bearing surface, so that the longitudinal profile is asymmetrical with respect to the center line.