A sealing arrangement for a hydrodynamic machine BAKGROUND OF THE INVENTION AND PRIOR ART The present invention relates to a sealing arrangement for a hydrodynamic machine according to the preamble of claim 1.

A hydrodynamic machine such as a hydrodynamic retarder comprises a stator and a rotor arranged in a housing. The stator and rotor may have a substantially corresponding design with a multiplicity of blades arranged in a respective annular shell The stator and the rotor are arranged such that the annular shells together form a toroidal space. During activation of the retarder a working medium is supplied to the toroidal space, A rotary shaft which extends through an opening of the housing transfers a rotary motion from a drive line of the vehicle to the rotor. A mechanical face seal is usually arranged in the space between the opening of the housing and the rotary shaft in order to prevent leakage of the working medium out of the housing. A mechanical taco seal comprises a sealing ring connected to the housing and a sealing ring rotating with the shaft. The sealing rings comprise sealing surfaces of a high degree of flatness abutting against each other. During operation, the sealing surfaces of the sealing rings slide in relation to each other. The working medium may be oil, water or a water mixture. It has been found that the scaling surfaces is worn out relatively fast when water or a water mixture are used as working medium.

WO 2011/082759 shows a hydrodynamic retarder comprising a stator and a rotor arranged inside a casing. A drive shaft drives the rotor. The drive shaft being sealed off with respect to the casing by means of a sliding ring seal in order to prevent any escape of working medium between the drive shaft, and the casing. The sliding ring seal has a scaling liquid supply in order to cool and/or to lubricate the sliding ring seal. The sliding ring seal has a first sliding ring and a second sliding ring which are arranged to enclose one another concentrically in the radial direction and each have a sealing surface, and which, together with a mating element, seal off a sealing gap running in the radial direction with respect to the drive shaft. A sealing liquid channel opens into the sliding ring seal in the radial direction between the two sealing surfaces in order to cool and/or to lubricate the two sealing surfaces with sealing liquid, SUMMARY OF THE IN VENTION The object of the present invention is to provide a sealing arrangement for a hydrodynamic machine where the sealing surfaces achieve a cooling and lubrication which prevent wear of the sealing surfaces substantially independent of the working medium used in the hydrodynamic machine.

The above mentioned objects are achieved by the sealing arrangement according to the characterizing portion, of claim 1. The sealing arrangement seals a space between a surface defining an opening of a housing and a rotary shaft having an extension through the opening. The: sealing arrangement comprises a first sealing ring connected to the housing ha ving an annular sealing surface and a second sealing ring connected to the rotary component having an annular sealing surface configured to seaiing!y abut against the sealing surface of the first sealing ring. Even if the sealing surfaces have a very high degree of flatness and smoothness, they are heated when the sealing rings slides in contact with each other. In order to cool the sealing surfaces and reduce the wear between the sealing surfaces, lubricant is supplied to a lubrication channel formed in a space between a radially ou ter part of the annular sealing surfaces and a radiall y inner part of the annular seali ng surfaces. The supply of lubrican t to the lubricant channel cools the radially outer part of the sealing surfaces as well as the radially inner part of the sealing surfaces in a very effective manner substantially independent of the working medium used in the hydrodynamic machine.

According to an embodiment of the invention, said lubrication channel is formed as a circular arc. in this ease, the lubrication channel is located at a constant radial distance from a rotational axis of the rotary shafi. As a consequence, the radial extension of the radially outer part of the sealing surfaces as well as the radially inner part of the sealing surfaces will be constant. However, it is possible to give the lubrication channel a substantially arbitrary shape along the sealing surfaces where the lubricant cools and lubrica t es the radiall y outer part of the sealing surfaces as well as the radially Inner part of the sealing surfaces in a favorable manner.

According to an embodiment of the invention, said lubrication channel extends almost completely around the annular sealing surfaces. In this case, it is possible to cool and lubricate all areas around the annular sealing surfaces in a favorable manner. The lubrication channel may extend at least 350º around the annular sealing surfaces. Alternatively, It Is possible to use two of more separate lubricant channels extending along different parts of the annular sealing surfaces.

According to an embodiment of the invention, the lubrication channel comprises an end portion provided with an inlet hole where the lubricant enters the lubrication channel and an opposite end portion with an outlet hole where the lubricant leaves the lubrication channel. Such a positioning of the inlet hole and the outlet hole ensure a lubricant flow along the whole lubrication channel. However, it is possible to provide the lubrication channel with several inlet holes and several outlet holes. The inlet hole and/or the outlet hole may extend through the first sealing ring. It is practical and relatively easy to arrange the inlet hole and the outlet hole of the lubricant channel in the form of through holes extending through the first non-rotatable sealing ring.

According to an embodiment of the invention, the end portions of the lubrication channel is connected to each other via a lubrication passage having a smaller cross section area than the lubrication channel. In this case, the lubrication channel and the lubrication passage form together a continuous annular lubrication groove. Such, a lubrication groove divides completely a radial outer sealing portion from a radially inner sealing portion. The lubrication passage is designed with a flow areas of a size such that it does not significantly influence on the lubricant flow through the lubrication channel.

According to an embodimen t of the invention, the second sealing ring rotates in a specific direction of ro tation around an axis of rotation of the rotary shaft, w herein t he lubrication channel is designed such that the lubricant flows in the same direction of rotation around said axis of rotation in the lubrication channel. Thereby, the rotational movement of the second scaling ring helps to drive the lubricant flow in the lubricant channel from the inlet hole to the outlet hole.

According to an embodiment of the invention, said lubrication channel is defined by a groove in at least one of the sealing surfaces. The annular sealing surfaces of the firstsealing ring and the second sealing ring are fiat, in order to provide a lubrication channel between the radially outer part and the radially inner part of the seating surfaces, it is necessary to provide a groove in at least one of the seating surfaces. Preferably, said lubrication channel is defined by a groove in the sealing surfaces of the first seating ring and a flat portion of the sealing surface of the second sealing ring, Both sealing ri ngs are manufactured of hard materials.

According to an embodiment of the invention, the sealing arrangement comprises a power member configured to press the sealing surfaces of the sealing rings against each other. It is necessary to press the sealing surfaces against each other with, a certain force for providing a tight sealing between the sealing surfaces. The power member may be a spring member. By means a suitably dimensioned spring member it is possible to provide a force of a suitable size pressing the sealing surfaces together. Furthermore, with a suitable design of the sealing arrangement, the pressure inside the housing may help to press the sealing surfaces of t he seating rings against each other, According to an embodim ent of the invention, the stationary part of the sealing arrangement comprises said spring member and an annular mounting unit by which the stationary part is releasably mounted in the housing. Such a stationary part of the sealing arrangement includes few components. The annular mounting unit may comprises an inlet channel receiving lubricant from a lubrication inlet line in the housing and an outlet channel delivering lubricant to a lubrication outlet line in the housing. Thus, the mounting unit and the first scaling ring of the stationary part of the sealing arrangement comprises parts of the lubrication passage supplying lubricant to and from the lubrication channel where the lubricant lubricates and cools the sealing surfaces.

According to an embodiment of the invention, the rotatable part of the sealing arrangement comprises an annular support member which is fixedly arranged on the rotary component and which supports the second sealing ring. By means of such a support member it is possible to support the second sealing ring in a corresponding radial position radial position in relation to the rotary shaft as the first scaling ring. The second sealing ring may be supported on the annular support member via a rubber sealing. The rubber sealing provides a tight connection between the second sealing ring and the annular support member. Furthermore, it provides a somewhat resilient support of the second sealing ring in relation to the first sealing ring which facilitate a tight abutment between the annular sealing surfaces of the sealing rings.

According to an embodiment of the invention, the lubricant is coolant, in certain hydrodynamic apparatus such as hydrodynamic retarders, coolant is used as working medium Instead of oil. In this case, it is a higher risk that the sealing surfaces are worn out In view of this fact, it. is especially appropriate to use the sealing arrangement according to the invention in hydrodynamic machines using other mediums than oil.

BRIEF DESCRIPTION OF THE DRAWINGS in the following a preferred embodiment of the invention is described, as an example, with reference to the attached drawings, on which: Fig. 1 shows a cross section view of a hydrodynamic retarder with a sealing arrangement according to the invention, fig. 2 shows the first sealing ring in Fig. 1 more in detail.

Fig. 3 shows a cross section view of an inlet hole to the sealing arrangement. Fig; 4 shows a cross section view of a resilient portion of the sealing arrangement and Fig. 5 shows a cross section view of an outlet hole of the sealing arrangement.

DETAILED DESCRIPTION OF A PREFERRED EMBODIMENT OF THE INVENTION Figure 1 shows a hydrodynamic brake in the form of a retarder of a vehicle powered by a combustion engine or an electric engine. The retarder comprises a stator 1 and a rotor 1. The stator 1 has an annular shell 3 with a multiplicity of blades 4. The blades 4 are usually arranged at equal spacing along the annular shell 3. The rotor 2 is of corresponding design and it comprises an annular shell 5 which incorporates a multiplicity of blades b, The blades 6 are usually arranged at equal spacing. The shells 3, 5 of the stator 1 and rotor 2 are arranged so that they together form a toroidal space 7. The stator I is arranged firmly on a stationary surface of the vehicle. A housing 8 encloses the stator 1 and the rotor 2. The rotor 2 incorporates a shaft, portion 2a which is connected firmly to a rotary shaft 9 extending through an. opening 8a of th e housing 8. The rotary shaft 9 is rotatably arranged around a rotary axis A. An outer portion of the rotary shaft 9 is engaged by a drive line of the vehicle. Thus, the rotor 2 will thus rotate with the drive line of the vehicle.

To exert a braking action on the hydrodynamic brake, a working medium is supplied to the toroidal space 7. In this ease, the working medium is coolant which is supplied from a cooling system cooling the engine of the vehicle. The coolant is supplied, via a coolant passage 10 and a multiplicity of apertures 11 in the stator 1 to the toroidal space 7, During the braking process, the kinetic energy of the coolant is converted to thermal energy in the toroidal space ?. The coolant leaves the toroidal space 7 via a multiplicity of apertures 19 at high pressure, The high, pressure is created by the high medium flow in the toroidal space 7. The multiplicity of apertures 19 lead the coolant to a coolant passage 20 and then to the cooling system. The coolant is also connected to a circular groove 13 via a circular aperture 12 between the radially outer parts of the stator 1 and rotor 2. The groove circular aperture 13 is connected to a space 14 located between the housing 8 and an outer surface of the rotor 2, As a consequence, coolant with a corresponding high pressure enters info the space 14, A sealing arrangement is configured to prevent leakage of coolant from the space 14 to the ambient via the opening 8a of the housing 8, The sealing arrangement comprises a stationary part 15 connected to the housing 8 and a rotatable part 16 firmly connected to the rotary shaft 9. The stationary part 15 comprises a first scaling ring 15a which is shown more in detail in Figs. 2-5. The rotatable part 16 comprises a second sealing ring 16a which is shown more in detail in Figs. 3-5, Fig, 2 shows the first sealing ring 15a in a separated state. The first sealing ring 15a may consist of carbon or another hard material. The first scaling ring 15a comprises at one side a flat annular sealing surface 15b provided with a circular arcshaped groove 15c. The arc-shaped groove 15c extends nearly one lap around the annular sealing surface 15b. An inlet hole 15d is located at one end of the arc-shaped groove 15c and an outlet hole 15e is located at an opposite end of the arc-shaped groove 15c. The inlet hole 1 Sd and the outlet hole 15c arc through holes extending through the first sealing ring 15a. The inlet hole 15d and the outlet hole 1 Se arc located at a relatively short distance .from each other. The coolant enters the arc-shaped groove 15c via the inlet hole 15d and it leaves the arc-shaped groove 15c via the outlet hole 15e. A lubricant passage 18 is arranged between the end portions of the lubrication channel 15c, The lubrication passage 18 has a smaller flow area than the lubrication channel 15c. Thus, the lubricant flow through the lubrication passage is smaller than the lubricant flow through the lubrication channel 15c, The lubrication passage 18 and the lubrication channel 15c separate a radially outer sealing surface 15b1and a radially inner sealing surface 15b2of the first sealing ring 15 from each other. A number of spring members 17, which are indicated with doted lines in Fig 2, are arranged at equal or almost equal spacing on an opposite side to the side including the sealing surface 15b and the arc-shaped groove 15c, Fig. 3 shows a cross section view through the inlet hole 15d of the first sealing ring 15a when it is in a mounted state. The stationary part 15 of the sealing arrangement comprises an annular stationary unit 15f. The annular stationary unit 15f is releasably mounted in an annular recess of the housing 8 by means of suitable mounting elements 15g. The annular stationary unit 15f includes the spring members 17 and the first sealing ring 15a, The housing 8 comprises a coolant inlet, line 8a directing coolant at pressure p1to an inlet channel 15h of the stationary unit 15f. The inlet channel 15h directs the coolant, via the inlethole 15d, to inlet portion of the arc-shaped, groove 15c, The sealing surface 15b of the first sealing ring 15a comprises a radially outer part 15b1arranged radially outside of the arc-shaped groove 15c where it is in contact with a radially outer part 16b1of the second sealing surface 16b. The sealing surface 15b comprises a radially inner part 15b2arranged radially inside of the groove 15c where it is in contact with a radially inner part 16b2of the second sealing surface 16b. The first seali ng ring 15a and the second sealing ring 16a may be manufactured of carbon*silicon carbide, ceramic or tungsten carbide or equal hard materials. The second sealing ring 16a comprises an annular support member 16c fixedly arranged on the shaft portion 2a of the rotor 2. The support member 16c supports the second sealing ring 16a by means of a rubber sealing 16d or similar material to assure a tight connection.

Fig. 4 shows a cross section view of a part of the first sealing ring 15a including one of the spring members 17. The spring members 17 is a compression spring arranged in a recess of the stationary unity. The spring member 17 acts between a botom surface in the recess and a surface of the first sealing ring 15a located on opposite side to the sealing surface 15b and the are-shaped groove 15c. Consequently the spring members 17 act with a spring force on the first sealing ring 15a pressing the sealing surface 15b of the first sealing ring 15a against the sealing surface 16b of the second sealing ring 16a.

Fig. 5 shows a cross section view through the outlet hole 15e of the first sealing ring 15a. When the coolant has flown through lubrication channel framed by the arc-shaped groove 15c in the first sealing ring 15a and a flat surface of the second sealing ring 16a, it leaves the lubrication channel and enters the outlet hole 15c. The outlet hole 15e directs the coolant to an outlet channel 15e in the stationary unit 15f whereupon the coolant is directed back to the cooling system via an outlet line 8b in the housing 8 at the pressure pi which is slightly lower than the pressure p1due to flow pressure drop.

Ambient air pressure p0prevails on the outside of the housing 8, The coolant is continuously supplied to the arc-shaped groove 15c with a certain positive pressure p; corresponding to the pressure of the coolant in die cooling system. When the retarder is activated coolant is let into the toroidal space 7 and into the space 14 between the housing 8 and the rotor 2. At high braking torque the pressure p2is higher than the pressure p1and p3. At low braking torque the pressure p2may be lower than the pressure p1and p3. The radially outer sealing surface 15b1of the first sealing ring 15 a and the radially outer seal ing surface 16b1of the second sealing ring 16a provides a tight sealing between the coolant with the pressure p2in the bousing 8 and the coolant with, the pressure p5in the groove 15c close to the inlet hole 15d and the pressure p3close to the outlet hole 15e when the retarder is activated. The inner radially sealing surface 15b2of the first sealing ring 15a and the inner radially sealing surface 16b2of the second sealing ring 16a provides a tight sealing between the coolant with the pressure ps in the groove 15c close to the inlet hole at 15d and the pressure p3close to the outlet hole 15e and the ambient air pressure p0on the outside of the housing 8. As a consequence, the sealing arrangement provides a scaling acting in two steps between the high coolant pressure ps in the space 14 in the housing 8 and the ambient air pressure p0. Such a sealing arrangement prevents leakage of coolant to the ambient air in a very effective manner.

When the vehicle runs, the power train of the vehicle provides a rotary movement of the rotor 2. As a consequence, the sealing surface 16b of the second sealing ring 16a slides in contact with the sealing surface 15b of the first sealing ring 15a. Inevitably, the friction between the sealing surfaces 15b, 16b generates heat. In order to cool the sealing surfaces 15b, 16b and reduce wear of the sealing surfaces 15b, 16b, coolant is continuously supplied from the cooling system, via the inlet line 8a in the housing 8, the inlet channel 15d and the inlet hole 15c, to the arc-shaped groove 15c of the first scaling ring 15a. In the arc-shaped groove 15c, the coolant comes in contact with a flat part 16bs of the sealing surface 16b located between the radially outer part 16b1and the radially inner part 16b2of the second sealing surface 16b. When the coolant flows along the arc-shaped groove 15c, it cools and lubricates the radially outwardly located parts 15b1, 16b2of the sealing surfaces 15b, 16b and as well the radially inwardly located parts 15b2, 16b2of the sealing surfaces 15b, 16b in a very effective manner. Since the arc-shaped grove 15c nearly extends one lap around the first sealing ring 15a, the coolant cools and lubricates the entire sealing surfaces 15b, 16b. Furthermore, the second sealing ring 16a rotates in a direction such that it promotes the coolant flow along the circular are-shaped groove 15c from, the end portion comprising the inlet hole 15d to the end portion comprising the outlet hole 15e.

The invention is not restricted to the described embodiment but may he varied freely within the scope of the claims.