Hydrodynamic brake

• US 6,923,301 B2
• Filed: 06/28/2001
• Issued: 08/02/2005
• Est. Priority Date: 07/07/2000
• Status: Expired due to Fees

• Current Assignee: Scania CV AB (Volkswagen AG)
• Original Assignee: Scania CV AB (Volkswagen AG)
• Inventors: Hagen, Torger, Arne, Johnny, Jönsson, Hans, Kjell, Anders
• Primary Examiner(s): SICONOLFI, ROBERT
• Application Number:
  US10/332,420
• Publication Number:
  US 20030188940A1
• Time in Patent Office: 1,496 Days
• Field of Search: 188/296, 188/301, 188/269, 192/3.34, 192/3.32
• US Class Current: 188/296
• CPC Class Codes: F16D 57/005 Details of blades, e.g. shape
• CPC Class Codes: F16D 57/04 with blades causing a directed flow, e.g. Föttinger type

Abstract

A hydrodynamic brake, which comprises a stator and a rotor which are coaxial and have respective opposed annular recesses which open toward each other to form a toroid-shaped space. A first medium is supplied to the space for providing braking action during rotation of the rotor. At least one injection member is arranged to supply a second medium to the toroid-shaped space for reducing the circulation of air in the toroid-shaped space when no brake action is desired. The second medium is supplied at at least one location to the toroid-shaped space with a pressure and in a direction which at least partly is directed towards the principal flow direction of the circulating air.

Claims

1. A hydrodynamic brake comprising:

a stator having an axis, a coaxial rotor for cooperating with the stator and rotatable around the axis, the stator being shaped to define an annular recess opening toward the rotor and a plurality of stator vanes extending toward the rotor, the annular recess of the stator has a bottom surface defining the annular recess thereof, the rotor being shaped to define an annular recess opening toward the recess of the stator and the rotor having a plurality of rotor vanes extending toward the stator, both the stator recess and the rotor recess together define a toroid-shaped space;

a supply of a first medium to the toroid-shaped space for providing a brake action during rotation of the rotor by the first medium cooperating with the vanes of the stator and the rotor during rotation of the rotor;

at least one inlet for supplying a second medium to the toroid-shaped space such that the second medium reduces circulation of air in the toroid-shaped space during rotation of the rotor with respect to the stator, wherein the second medium inlet is arranged to supply the second medium at at least one location in the toroid-shaped space and with a pressure and in a supply direction into the space which is at least partly directed toward the principal flow direction of air circulating in the toroid-shaped space during rotation of the rotor;

the at least one inlet for supplying the second medium includes at least one inlet jet for supplying a jet of the medium into the toroid-shaped space, the inlet jet includes an injection portion shaped and positioned to inject the second medium into the toroid-shaped space, the injection portion for the second medium comprises an orifice arranged in the bottom surface of the recess of the stator so as to supply the second medium at an injection angle between 15° and

45°

to a radius that extends from the orifice to a center of the toroid-shaped space.

2. The hydrodynamic brake of claim 1, wherein the second medium supplied by the jet is the same as the first medium supplied to the toroid-shaped space for braking action on the vanes.

3. The hydrodynamic brake of claim 1, wherein the toroid-shaped space has a radially inward portion, and the injection portion is positioned to inject a second medium from the radially inward portion of the toroid-shaped space.

4. The hydrodynamic brake of claim 1, wherein the toroid-shaped space has a radially outward portion, and the injection portion is shaped, oriented and positioned to supply second medium in the radially outward portion of the toroid-shaped space.

5. The hydrodynamic brake of claim 1, wherein the rotor has a shaft portion about which the rotor rotates around the axis, the rotor recess has a bottom surface defining the recess, the injection portion is defined in the shaft portion of the rotor.

6. The hydrodynamic brake of claim 1, wherein the rotor has a shaft portion about which the rotor rotates around the axis, the rotor recess has a bottom surface defining the recess, and further including a second inlet jet for supplying the medium into the toroid-shaped space, the second inlet jet including a further injection portion defined in the shaft portion of the rotor, which further injection portion comprises an orifice in the bottom surface of the recess of the rotor.

7. The hydrodynamic brake of claim 6, wherein the further injection portion is shaped and positioned to supply second medium in a direction having an angle of between 15°

to 45°

to a radial direction and which extends from the orifice of the injection member and through a center in the toroid-shaped space.

8. The hydrodynamic brake of claim 7, wherein the stator recess, the rotor recess and the vanes therein arc shaped to drive circulating air in a pathway around and between the recesses;

the inlet for supplying second medium is directed to supply the second medium in a direction which tends to change the direction of flow of around the toroid-shaped space air around the recesses thereby to reduce the braking effect of the circulating air on the rotor.

9. The hydrodynamic brake of claim 1, wherein the stator recess, the rotor recess and the vanes therein are shaped to drive circulating air in a pathway around and between the recesses;

the inlet for supplying second medium is directed to supply the second medium in a direction which tends to change the direction of flow of around the toroid-shaped space air around the recesses thereby to reduce the braking effect of the circulating air on the rotor.