Bearing cage and bearing means having this type of bearing cage as well as method for designing, repairing and/or replacing such a bearing cage

1. A bearing cage ( 1 ) of a bearing, which is produced by means of a generative manufacturing method, comprising:

an outer flange ( 2 ) and a bearing seat ( 8 ), which are joined together via a plurality of spring beams ( 3 , 5 , 7 );

a first intermediate ring ( 4 ) joined to the outer flange ( 2 ) via first spring beams ( 3 );

a second intermediate ring ( 6 ) joined to the first intermediate ring ( 4 ) via second spring beams ( 5 ); and

the second intermediate ring ( 6 ) being joined to the bearing seat ( 8 ) via third spring beams ( 7 ).

2. The bearing cage according to claim 1 , wherein the second spring beams ( 5 ) are arranged offset with respect to the first spring beams ( 3 ) and/or the third spring beams ( 7 ) are arranged offset with respect to the second spring beams ( 5 ).

3. The bearing cage according to claim 1 , wherein the bearing seat ( 8 ) includes at least one pocket ( 11 ), which is connected to at least one oil line ( 12 ) for supplying an oil or squeeze film.

4. The bearing cage according to claim 3 , wherein the at least one oil line ( 12 ) is formed running in the bearing seat ( 8 ), in at least one spring beam ( 3 , 5 , 7 ), in at least one intermediate ring ( 4 , 6 ), and/or in the outer flange ( 2 ).

5. The bearing cage according to claim 1 , wherein a bearing ( 9 ) is taken up in the bearing seat ( 8 ) and the bearing ( 9 ) is fixed in place in an axial direction by a bearing fixation element ( 10 ).

6. The bearing cage according to claim 1 , wherein the bearing cage ( 1 ) is a multiply folded bearing cage ( 1 ).

7. The bearing cage according to claim 1 , wherein at least one spring beam ( 3 , 5 , 7 ) has a constant cross section.

8. The bearing cage according to claim 1 , wherein at least one spring beam ( 3 , 5 , 7 ) has a varying cross section, wherein the at least one spring beam ( 3 , 5 , 7 ) has a specifically adjusted, nonlinear spring characteristic.

9. The bearing cage according to claim 1 , wherein first spring beams ( 3 ), second spring beams ( 5 ), and/or third spring beams ( 7 ) have the same length and/or the same cross section or a different length and/or a different cross section.

10. The bearing cage according to claim 1 , wherein at least one stop element ( 14 ), which is formed integrally with or on the outer flange ( 2 ) or the second intermediate ring ( 6 ), or is arranged between the outer flange ( 2 ) and the second intermediate ring ( 6 ) of the bearing cage ( 1 ).

11. The bearing cage according to claim 10 , wherein the at least one stop element ( 14 ) has a stop surface that lies opposite a counter stop surface of one of the outer flange ( 2 ) and the second intermediate ring ( 6 ), with a surface contour of the stop surface being complementary to a surface contour of the counter stop surface.

12. The bearing cage according to claim 10 , wherein the at least one stop element ( 14 ) includes, above a defined load acting on the at least one stop element ( 14 ), a deformation of the stop element ( 14 ).

13. The bearing cage according to claim 12 , wherein the at least one stop element ( 14 ) is structurally less rigid in a middle region between its two end portions, each of which faces or is assigned to one of the two component segments ( 2 , 6 ), than at the two end portions.

14. The bearing cage according to claim 13 , wherein, after a plastic deformation, the two end portions of the at least one stop element ( 14 ) are still joined to each other in a form-fitting manner in the middle region between the two end portions of the stop element ( 14 ).

15. The bearing cage according to claim 1 , wherein the bearing is in an aircraft engine and bears a shaft, which joins a turbine section to a compressor section of the aircraft engine.

16. A method for designing, repairing, and/or replacing a bearing cage of a bearing having an outer flange ( 2 ) and a bearing seat ( 8 ), which are joined together via a plurality of spring beams ( 3 , 5 , 7 ), comprising the steps of:

applying a powder layer, which can be solidified by means of radiated energy, onto a support;

solidifying the powder layer by means of radiated energy from a source of radiated energy in a component region of the powder layer, wherein the component region is the bearing cage region;

moving the support by one layer thickness and application of the next powder layer;

solidifying the powder layer by radiated energy from a source of radiated energy in the component region of the powder layer;

repeating the preceding steps until a finished bearing cage has been constructed from the solidified component region; including the steps of:

forming a first intermediate ring ( 4 ) joined to the outer flange ( 2 ) via first spring beams ( 3 );

forming a second intermediate ring ( 6 ) joined to the first intermediate ring ( 4 ) via second spring beams ( 5 ); and

joining the second intermediate ring ( 6 ) to the bearing seat ( 8 ) via third spring beams ( 7 ).

17. A bearing cage of a bearing, which is produced by means of a generative manufacturing method, comprising:

a bearing seat, an outer flange and a plurality of component segments, which are joined together via a plurality of spring beams;

at least one stop element arranged between the plurality of component segments.