A device for sealing a valve for controlling a coolant of an internal combustion engine of a motor vehicle is described, which valve is mounted in a cooling system together with a valve housing, wherein the valve housing contains, at the inlet and/or the outlet side, a sealing ring which has an annular wall and a spaced annular lip extending away from the annular wall from a contact point.

A device for sealing a valve for controlling a coolant of an internal combustion engine of a motor vehicle is described, which valve is mounted in a cooling system together with a valve housing, wherein the valve housing contains, at the inlet and/or the outlet side, a sealing ring which has an annular wall and a spaced annular lip extending away from the annular wall from a contact point.

A seal structure between an oil outlet formed in a first case and an oil inlet formed in a second case and having an end face facing an end face of the oil outlet with a clearance between the end faces, the seal structure including an annular first seal disposed in an increased-diameter hole, which is formed on an outlet side or an inlet side of an oil passage in one of the oil outlet and the oil inlet and has a larger diameter than the oil passage, such that the first seal contacts a step surface located at a boundary between the oil passage and the increased-diameter hole; and an annular second seal harder than the first seal and disposed in the increased-diameter hole such that the second seal contacts the first seal and the end face of the other of the oil outlet and the oil inlet.

It is an object of the present invention to provide a seal ring which has small oil leak and low torque generation performance for improving fuel consumption in a favorable balance as originally intended by the present invention. A seal ring (1) is mounted on an annular groove formed on one member consisting of either a housing having a shaft hole or a rotary shaft inserted into the shaft hole, contacts a surface of other member consisting of either the housing or the rotary shaft, and slidably contacts a side wall surface of the annular groove at a non-sealed fluid side thereof. V-shaped concave portions (3) which do not contact the side wall surface of the annular groove are formed on at least one portion of an end of an inner diameter side of a side surface (2) of the seal ring (1).

It is an object of the present invention to provide a seal ring which has small oil leak and low torque generation performance for improving fuel consumption in a favorable balance as originally intended by the present invention. A seal ring (1) is mounted on an annular groove formed on one member consisting of either a housing having a shaft hole or a rotary shaft inserted into the shaft hole, contacts a surface of other member consisting of either the housing or the rotary shaft, and slidably contacts a side wall surface of the annular groove at a non-sealed fluid side thereof. V-shaped concave portions (3) which do not contact the side wall surface of the annular groove are formed on at least one portion of an end of an inner diameter side of a side surface (2) of the seal ring (1).

A hydraulic cylinder includes a cylinder tube, a piston, a piston rod, a bearing, and a seal, wherein the seal is configured to allow the flow of the operating liquid from the rod side chamber toward the anti-rode side chamber through the through passage when the pressure in the rod side chamber is higher than the pressure in the anti-rod side chamber.

A hydraulic cylinder includes a cylinder tube, a piston, a piston rod, a bearing, and a seal, wherein the seal is configured to allow the flow of the operating liquid from the rod side chamber toward the anti-rode side chamber through the through passage when the pressure in the rod side chamber is higher than the pressure in the anti-rod side chamber.

Seal systems for aircraft are disclosed. An example seal system includes a first seal to couple to a first thrust reverser portion, the first seal having a first cross-sectional shape. A second seal is to couple to a second thrust reverser portion opposite the first seal. The second seal having a second cross-sectional shape different than the first cross-sectional shape. The second seal is to receive at least a portion of the first seal in response to the first seal engaging the second seal.

An arrangement structure for a seal member includes: a first member having a first mating surface and provided with a groove portion; a second member having a second mating surface, and configured to move relatively to the first member; and an annular seal member fitted into the groove portion, providing sealing between the first member and the second member, and serving as a partition between an atmosphere-side space and a pressurized-side space. The seal member includes a plurality of first protruding portions protruding toward the second mating surface and aligned from the atmosphere-side space toward the pressurized-side space. The seal member has such a shape that, in a state of not being fitted into the groove portion, a protrusion height of the first protruding portion increases in stages from the first protruding portion arranged close to the pressurized-side space toward the first protruding portion arranged close to the atmosphere-side space.

A shockwave-inducing mechanical rotating shaft seal includes a seal face gap having at least one section of converging and then diverging gap width that supersonically accelerates compressible fluid escaping through the seal gap, thereby causing a shockwave that reduces the fluid pressure and provides a high pressure fluid seal with significantly reduced viscous heating and gap width. A plurality of the converging-diverging sections can be provided, having a combined width between 0.004 and 0.008 inches. The converging-diverging sections can be configured to accelerate the fluid to a Mach number less than 4. The gap can further include a section of flat, parallel seal faces that induce viscous stresses in the fluid, thereby further reducing the fluid pressure. The seal can be configured with axially directed seal faces or radially directed seal faces, and/or used as a pre-conditioner in combination with a conventional downstream mechanical fluid seal.