Hydraulic linear actuating drive
A hydraulic linear actuating drive includes a cylinder, a movable servo piston that can be pressure-loaded and that runs inside the cylinder, at least one piston rod attached to the servo piston, and at least one piston gasket having at least two sealing elements at a distance from each other. An intermediate sealing space is defined between the at least two sealing elements, an inner wall of the cylinder and an outer edge of the servo piston. The hydraulic linear actuating drive has at least one leakage channel that can move together with the servo piston. A first end of the channel opens into the intermediate sealing space and into a leakage fluid inlet opening located there, while the other, second end of the channel opens into a leakage fluid outlet opening arranged outside of the cylinder.
1. A hydraulic linear actuating drive for an aircraft arrangement comprising:
a cylinder with a first end and a second end, the first and the second ends opposing one another;
a movable servo piston capable of being pressure-loaded and running inside the cylinder, wherein the movable servo piston separates two operating chambers;
a hydraulic working fluid occupying both of the two operating chambers;
a first and a second piston rod attached to the servo piston, wherein the first piston rod protrudes from the first end, and wherein the second piston rod protrudes from the second end, and wherein the first piston rod is attached to an actuating element;
at least one piston gasket having at least two sealing elements disposed at a distance from each other, an intermediate space being defined between the at least two sealing elements, an inner wall of the cylinder and an outer edge of the servo piston;
at least one leakage channel moveable together with the servo piston and having a first end opening into a leakage fluid inlet opening located in the intermediate sealing space and a second end opening into a leakage fluid outlet opening arranged outside of the cylinder; and
a valve disposed outside of the cylinder on the leakage fluid outlet opening, the valve opening towards an outside of the leakage channel and closing towards an inside of the leakage channel.
2. The hydraulic linear actuating drive as recited in claim 1 , wherein the leakage channel has a first channel section extending in a radial direction from the leakage fluid inlet opening through the servo piston to a center area of the servo piston.
3. The hydraulic linear actuating drive as recited in claim 2 , wherein the leakage channel has a second channel section opening into the at least one first channel section and running through the at least one piston rod to the leakage fluid outlet opening along an entire maximum actuating distance of the servo piston outside of the cylinder.
4. The hydraulic linear actuating drive as recited in claim 3 , wherein the second channel section extends coaxially with the at least one piston rod.
5. The hydraulic linear actuating drive as recited in claim 3 , wherein the leakage fluid outlet opening is formed by at least one radial test bore starting from an outer circumference of the piston rod and opening into the second channel section.
6. The hydraulic linear actuating drive as recited in claim 1 , further comprising a leakage groove disposed on an outer circumference of the servo piston in the intermediate sealing space, and wherein the leakage fluid inlet opening opens into the leakage groove.