Divided stabilizer having an optimized spring rate
View Patent ↗It is a purpose in a divided stabilizer to increase the springy lengths of the two stabilizer components. The stabilizer components ( 1, 1′, 2, 2 ′) have respective rotary parts ( 4, 4′, 5, 5 ′) attached and the rotary parts in turn have respective rotary wings ( 14, 16 ) attached. A cover flange ( 8 ′) is formed at the outer rotary part ( 4 ′). An outer rotary wing ( 14 ) is radially inwardly directed and attached to the outer rotary part ( 4 ′). An inner rotary wing ( 16 ) is radially outwardly directed and is attached to the inner rotary part ( 5 ′). A second stabilizer part ( 2, 2 ′) is attached to the inner rotary part ( 5 ′), wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) moves relative to the liner rotary part ( 5 ′) with the inner rotary wing ( 16 ) up to the point where the outer rotary wing ( 14 ) contacts the inner rotary wing ( 16 ). The rotary wings ( 14, 16 ) are rotatable relative to each other up to a predetermined angle. The stabilizer is coordinated in parallel to an axle of a vehicle.
1. A subdivided stabilizer with optimized spring rate, comprising
a first stabilizer part ( 1 , 1 ′);
a second stabilizer part ( 2 , 2 ),
an outer rotary part ( 4 ′) with an outer rotary wing ( 14 ), wherein the outer rotary wing ( 14 ) is radially inwardly directed;
an inner rotary part ( 5 ′) with an inner rotary wing ( 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed,
wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) and the inner rotary part ( 5 ′) with the rotary wing ( 16 ) form a rotary clutch ( 13 ), and wherein the first stabilizer part ( 1 , 1 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the rotary clutch ( 13 ), wherein the inner rotary part ( 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) and wherein the outer rotary part ( 4 ′) is connected to the first stabilizer part ( 1 ′) through a second radial force transfer plane ( 10 ′) and wherein the inner rotary part ( 5 ′) is connected to the second stabilizer part ( 2 ′) through a first radial force transfer plane ( 7 ′);
a cover flange ( 8 ′) formed at the outer rotary part ( 4 ′) wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 ′) of the outer rotary part ( 4 ′) and the first stabilizer part ( 1 , 1 ′) extends up to the second radial force transfer plane ( 10 ′) with spring rate determining dimensions of the first stabilizer part ( 1 ′),
wherein the second stabilizer part ( 2 ′) is formed as a single piece with the inner rotary part ( 5 ′) and extends up to the first radial force transfer plane ( 7 ′) with spring rate determining dimensions of the second stabilizer part ( 2 ′), wherein a first force transferring axial length (x, y) is coordinated to the first radial force transfer plane ( 7 ′), wherein a second force transferring axial length (x, y) is coordinated to the second radial force transfer plane ( 10 ′), and wherein the first force transferring axial length (x, y) and the second force transferring axial length (x, y) are disposed immediately neighboring,
wherein the inner rotary wing ( 16 ) of the inner rotary part ( 5 ′) and the outer rotary wing ( 14 ) of the outer rotary part ( 4 ′) form a third radial force transfer plane ( 17 ) and wherein the third radial force transfer plane ( 17 ) is disposed on the side of the first radial force transfer plane ( 7 ′) located toward the second stabilizer part ( 2 ′),
wherein the outer rotary wing ( 14 ) is fixedly connected to the outer rotary part ( 4 ) over a certain force transferring axial length (x), and wherein the inner rotary wing ( 6 ) is fixedly connected to the inner rotary part ( 5 ) over the same force transferring axial length (x),
and wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) are freely rotatable relative to each other in a region of the free spaces ( 18 ) until the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) come to rest on a mutual stop,
wherein the force transferring axial length x of the attachment between the outer rotary part ( 4 ) and the outer rotary wing ( 14 ) or, respectively between the inner rotary part ( 5 ) and the inner rotary wing ( 6 ) is determined by the torque to be transferred, and
wherein a size of the outer rotary wing ( 14 ) and of the inner rotary wing ( 6 ) results from the torque to be generated by a hydraulic swivel motor ( 3 ), and
wherein the torque generating axial length is the basis of this size of the outer rotary wing ( 14 ) and of the inner rotary wing ( 6 ).
2. Subdivided stabilizer according to claim 1 , characterized in that the second stabilizer part ( 2 , 2 ′) with its inner rotary part ( 5 ′) is formed as a single piece and wherein the first stabilizer part ( 1 , 1 ′) with its cover flange ( 8 ′) is formed as a single piece.
3. The subdivided stabilizer according to claim 1 further comprising
a force transfer element ( 15 ) forming the first radial force transfer plane ( 7 ′) and wherein the force transfer element ( 15 ) is connected fixed against rotation to the inner rotary part ( 5 ), and wherein the force transfer element ( 15 ) is connected as a single part with the inner rotary wing ( 16 ).
4. The subdivided stabilizer according to claim 1 wherein
a torque generating axial length corresponds to the force transferring length x,
wherein
the torque is transferred from the first stabilizer part ( 1 , 1 ′) through the cover flange ( 8 , 8 ′) radially on the second radial force transferring plane ( 10 , 10 ′), then axially through the outer rotary part ( 4 , 4 ′) to the first force transferring plane ( 7 , 7 ′), then radially through the inner rotary wing ( 6 , 16 ) and through the inner rotary part ( 5 , 5 ′) to the second stabilizer part ( 2 , 2 ′).
5. The subdivided stabilizer according to claim 1 wherein
a torque transferring length x of the inner rotary wing ( 16 ) is smaller than a rotary torque generating length,
wherein
the torque is transferred in case of a different loading of the first stabilizer part ( 1 ′) and of the second stabilizer part ( 2 ′) from the first stabilizer part ( 1 ′) in axial direction to the second radial force transfer plane ( 10 ′), then through the cover flange ( 8 ′) radially on the second radial force transferring plane ( 10 ′), then in axial direction through the outer rotary part ( 15 ) to the third force transferring plane ( 17 ), then in axial direction back through the inner rotary wing ( 16 ) to the first force transferring plane ( 7 ′), then radially to the inner rotary part ( 5 ′), from where the force propagates in axial direction within the second stabilizer part ( 2 ′).
6. The subdivided stabilizer according to claim 1 wherein the outer rotary part ( 4 ) with its outer rotary wing ( 14 ) and the inner rotary part ( 5 ) with its inner rotary wing ( 6 ) find an axial closure through the cover flange ( 8 ) connected with the first stabilizer part ( 1 , 1 ′) and through a bearing cover ( 9 ), wherein the free spaces between the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) are formed as pressure chambers sealed toward the outside and inside in a corresponding way and connected to a hydraulic plant.
7. A subdivided stabilizer
with optimized spring rate, comprising
a first stabilizer part ( 1 , 1 ′);
a second stabilizer part ( 2 , 2 ),
an outer rotary part ( 4 ′) with an outer rotary wing ( 14 ), wherein the outer rotary wing ( 14 ) is radially inwardly directed;
an inner rotary part ( 5 ′) with an inner rotary wing ( 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed,
wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) and the inner rotary part ( 5 ′) with the rotary wing ( 16 ) form a rotary clutch ( 13 ), and wherein the first stabilizer part ( 1 , 1 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the rotary clutch ( 13 ), wherein the inner rotary part ( 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) and wherein the outer rotary part ( 4 ′) is connected to the first stabilizer part ( 1 ′) through a second radial force transfer plane ( 10 ′) and wherein the inner rotary part ( 5 ′) is connected to the second stabilizer part ( 2 ′) through a first radial force transfer plane ( 7 ′);
a cover flange ( 8 ′) formed at the outer rotary part ( 4 ′) wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 ′) of the outer rotary part ( 4 ′) and the first stabilizer part ( 1 , 1 ′) extends up to the second radial force transfer plane ( 10 ′) with spring rate determining dimensions of the first stabilizer part ( 1 ′),
wherein the second stabilizer part ( 2 ′) is formed as a single piece with the inner rotary part ( 5 ′) and extends up to the first radial force transfer plane ( 7 ′) with spring rate determining dimensions of the second stabilizer part ( 2 ′),
wherein a first force transferring axial length (x, y) is coordinated to the first radial force transfer plane ( 7 ′), wherein a second force transferring axial length (x, y) is coordinated to the second radial force transfer plane ( 10 ′), and wherein the first force transferring axial length (x, y) and the second force transferring axial length (x, y) are disposed immediately neighboring,
wherein the inner rotary wing ( 16 ) of the inner rotary part ( 5 ′) and the outer rotary wing ( 14 ) of the outer rotary part ( 4 ′) form a third radial force transfer plane ( 17 ) and wherein the third radial force transfer plane ( 17 ) is disposed on the side of the first radial force transfer plane ( 7 ′) located toward the second stabilizer part ( 2 ′),
wherein the outer rotary part ( 4 ) with its outer rotary wing ( 14 ) and the inner rotary part ( 5 ) with its inner rotary wing ( 6 ) find an axial closure through the cover flange ( 8 ) connected with the first stabilizer part ( 1 , 1 ′) and through a bearing cover ( 9 ), wherein the free spaces between the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) are formed as pressure chambers sealed toward the outside and inside in a corresponding way and connected to a hydraulic plant,
wherein the cover flange ( 8 ) performs a cover function at a hydraulic swivel motor ( 3 ) and a torque transferring function,
wherein
an axial length of the cover flange ( 8 ) represents a further force transferring length y for a force transfer from the first stabilizer part ( 1 ) to the outer rotary part ( 4 ) and backward on the second radial force transfer plane ( 10 ).
8. A subdivided stabilizer
with optimized spring rate, comprising
a first stabilizer part ( 1 , 1 ′);
a second stabilizer part ( 2 , 2 ),
an outer rotary part ( 4 ′) with an outer rotary wing ( 14 ), wherein the outer rotary wing ( 14 ) is radially inwardly directed;
an inner rotary part ( 5 ′) with an inner rotary wing ( 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed,
wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) and the inner rotary part ( 5 ′) with the rotary wing ( 16 ) form a rotary clutch ( 13 ), and wherein the first stabilizer part ( 1 , 2 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the rotary clutch ( 13 ), wherein the inner rotary part ( 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) and wherein the outer rotary part ( 4 ′) is connected to the first stabilizer part ( 2 ′) through a second radial force transfer plane ( 10 ′) and wherein the inner rotary part ( 5 ′) is connected to the second stabilizer part ( 2 ′) through a first radial force transfer plane ( 7 ′);
a cover flange ( 8 ′) formed at the outer rotary part ( 4 ′) wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 ′) of the outer rotary part ( 4 ′) and the first stabilizer part ( 1 , 1 ′) extends up to the second radial force transfer plane ( 10 ′) with spring rate determining dimensions of the first stabilizer part ( 1 ′),
wherein the second stabilizer part ( 2 ′) is formed as a single piece with the inner rotary part ( 5 ′) and extends up to the first radial force transfer plane ( 7 ′) with spring rate determining dimensions of the second stabilizer part ( 2 ′), wherein a first force transferring axial length (x, y) is coordinated to the first radial force transfer plane ( 7 ′), wherein a second force transferring axial length (x, y) is coordinated to the second radial force transfer plane ( 10 ′), and wherein the first force transferring axial length (x, y) and the second force transferring axial length (x, y) are disposed immediately neighboring,
wherein the inner rotary wing ( 16 ) of the inner rotary part ( 5 ′) and the outer rotary wing ( 14 ) of the outer rotary part ( 4 ′) form a third radial force transfer plane ( 17 ) and wherein the third radial force transfer plane ( 17 ) is disposed on the side of the first radial force transfer plane ( 7 ′) located toward the second stabilizer part ( 2 ′),
wherein the outer rotary part ( 4 ) with its outer rotary wing ( 14 ) and the inner rotary part ( 5 ) with its inner rotary wing ( 6 ) find an axial closure through the cover flange ( 8 ) connected with the first stabilizer part ( 1 , 1 ′) and through a bearing cover ( 9 ), wherein the free spaces between the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) are formed as pressure chambers sealed toward the outside and inside in a corresponding way and connected to a hydraulic plant,
wherein the cover flange ( 8 ) is furnished on an inner side in a finite bearing hole ( 11 ) for receiving the second stabilizing part ( 2 ) with its inner rotary part ( 5 ),
wherein
the bearing cover ( 9 ) comprises a passing through bearing bore ( 12 ) for receiving of the inner rotary part ( 5 ),
wherein
both the bearing cover ( 9 ) and the cover flange ( 8 ) are attached at the outer rotary part ( 4 ) with screws or by a welding connection,
wherein the inner rotary wing ( 6 ) is attached on the inner rotary part ( 5 ) by gear teeth or by clamping.
9. A subdivided stabilizer
with optimized spring rate, comprising
a first stabilizer part ( 1 , 1 ′);
a second stabilizer part ( 2 , 2 ),
an outer rotary part ( 4 ′) with an outer rotary wing ( 14 ), wherein the outer rotary wing ( 14 ) is radially inwardly directed;
an inner rotary part ( 5 ′) with an inner rotary wing ( 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed,
wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) and the inner rotary part ( 5 ′) with the rotary wing ( 16 ) form a rotary clutch ( 13 ), and wherein the first stabilizer part ( 1 , 1 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the rotary clutch ( 13 ), wherein the inner rotary part ( 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) and wherein the outer rotary part ( 4 ′) is connected to the first stabilizer part ( 1 ′) through a second radial force transfer plane ( 10 ′) and wherein the inner rotary part ( 5 ′) is connected to the second stabilizer part ( 2 ′) through a first radial force transfer plane ( 7 ′);
a cover flange ( 8 ′) formed at the outer rotary part ( 4 ′) wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 ′) of the outer rotary part ( 4 ′) and the first stabilizer part ( 1 , 1 ′) extends up to the second radial force transfer plane ( 10 ′) with spring rate determining dimensions of the first stabilizer part ( 2 ′),
wherein the second stabilizer part ( 2 ′) is formed as a single piece with the inner rotary part ( 5 ′) and extends up to the first radial force transfer plane ( 7 ′) with spring rate determining dimensions of the second stabilizer part ( 2 ′), wherein a first force transferring axial length (x, y) is coordinated to the first radial force transfer plane ( 7 ′), wherein a second force transferring axial length (x, y) is coordinated to the second radial force transfer plane ( 10 ′), and wherein the first force transferring axial length (x, y) and the second force transferring axial length (x, y) are disposed immediately neighboring,
wherein the inner rotary wing ( 16 ) of the inner rotary part ( 5 ′) and the outer rotary wing ( 14 ) of the outer rotary part ( 4 ′) form a third radial force transfer plane ( 17 ) and wherein the third radial force transfer plane ( 17 ) is disposed on the side of the first radial force transfer plane ( 7 ′) located toward the second stabilizer part ( 2 ′),
wherein the coupling piece ( 19 ) comprises
a guide part ( 20 ) and two equal and oppositely disposed coupling parts ( 21 ) equipped with side ways and conically extending guide faces, wherein the coupling parts ( 21 ) are capable of closing the free spaces ( 18 ) between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) without play, a compression spring ( 22 ) supported at a bearing cover ( 9 ′) and disposed in a spring chamber ( 23 ), wherein the spring chamber ( 23 ) is formed as a pressure space and connected to a hydraulic plant through an inlet connection piece ( 24 ),
wherein
the coupling piece ( 19 ) is loadable with a hydraulic pressure created in the spring chamber ( 23 ) opposing the compression spring ( 22 ) on the side disposed remote from the compression spring ( 22 ),
wherein the hydraulic pressure supports the force of the compression spring ( 22 ),
wherein a corresponding inlet opening ( 25 ) for a hydraulic pressure creation is disposed in the cover flange ( 8 ′).
10. A subdivided stabilizer
with optimized spring rate, comprising
a first stabilizer part ( 1 , 1 ′);
a second stabilizer part ( 2 , 2 ),
an outer rotary part ( 4 ′) with an outer rotary wing ( 14 ), wherein the outer rotary wing ( 14 )is radially inwardly directed;
an inner rotary part ( 5 ′) with an inner rotary wing ( 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed,
wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) and the inner rotary part ( 5 ′) with the rotary wing ( 16 ) form a rotary clutch ( 13 ), and wherein the first stabilizer part ( 1 , 1 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the rotary clutch ( 13 ), wherein the inner rotary part ( 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) and wherein the outer rotary part ( 4 ′) is connected to the first stabilizer part ( 1 ′) through a second radial force transfer plane ( 10 ′) and wherein the inner rotary part ( 5 ′) is connected to the second stabilizer part ( 2 ′) through a first radial force transfer plane ( 7 ′);
a cover flange ( 8 ′) formed at the outer rotary part ( 4 ′) wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 ′) of the outer rotary part ( 4 ′) and the first stabilizer part ( 1 , 1 ′) extends up to the second radial force transfer plane ( 10 ′) with spring rate determining dimensions of the first stabilizer part ( 1 ′),
wherein the second stabilizer part ( 2 ′) is formed as a single piece with the inner rotary part ( 5 ′) and extends up to the first radial force transfer plane ( 7 ′) with spring rate determining dimensions of the second stabilizer part ( 2 ′), wherein a first force transferring axial length (x, y) is coordinated to the first radial force transfer plane ( 7 ′), wherein a second force transferring axial length (x, y) is coordinated to the second radial force transfer plane ( 10 ′), and wherein the first force transferring axial length (x, y) and the second force transferring axial length (x, y) are disposed immediately neighboring,
wherein the inner rotary wing ( 16 ) of the inner rotary part ( 5 ′) and the outer rotary wing ( 14 ) of the outer rotary part ( 4 ′) form a third radial force transfer plane ( 17 ) and wherein the third radial force transfer plane ( 17 ) is disposed on the side of the first radial force transfer plane ( 7 ′) located toward the second stabilizer part ( 2 ′),
a sensor ( 26 ) for determining a position of a movable coupling piece ( 19 ) disposed in the outer rotary part ( 4 ′).
11. A subdivided stabilizer
with optimized spring rate,
comprising
a first stabilizer part ( 1 , 1 ′);
a cover flange ( 8 , 8 ′), wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 , 8 ′);
an outer rotary part ( 4 ′), wherein the cover flange ( 8 , 8 ′) is formed at the outer rotary part ( 4 ′);
an outer rotary wing ( 14 ) attached to the outer rotary part ( 4 ′), wherein the outer rotary wing ( 14 ) is radially inwardly directed;
an inner rotary wing ( 6 , 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed;
an inner rotary part ( 5 ′), wherein the inner rotary wing ( 6 , 16 ) is attached to the inner rotary part ( 5 ′);
a second stabilizer part ( 2 , 2 ′), wherein the second stabilizer part ( 2 , 2 ′) is attached to the inner rotary part ( 5 ′), wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) moves relative the inner rotary part ( 5 ′) with the inner rotary wing ( 6 , 16 ) up to a point where the outer rotary wing ( 14 ) contacts the inner rotary wing ( 6 , 16 ), and wherein the first stabilizer part ( 1 , 1 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the outer rotary wing ( 14 ) and the inner rotary wing ( 6 , 16 ), wherein the inner rotary part ( 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a movable coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 6 , 16 ); wherein the second stabilizer part ( 2 , 2 ′) is formed as a single piece with the inner rotary part ( 5 ′),
wherein the movable coupling piece ( 19 ) comprises
two equal and oppositely disposed coupling parts ( 21 ) equipped with side ways and conically extending guide faces, wherein the coupling parts ( 21 ) are capable of closing the free spaces ( 18 ) between the outer rotary wing ( 14 ) and the inner rotary wing ( 6 , 16 ) without play;
wherein the coupling parts ( 21 ) are disengaged in the decoupled state from the outer rotary wing ( 14 ) and from the inner rotary wing ( 6 , 16 ) such that initially a free angle of rotation has to be overcome for each direction in case of a different load of the first stabilizer part ( 1 , 1 ′) and of the second stabilizer part ( 2 , 2 ′) before the outer rotary wing ( 14 ) and the inner rotary wing ( 6 , 16 ) come to rest.
12. The subdivided stabilizer according to claim 11 further comprising
a force transfer element ( 15 ) connected fixed against rotation to the inner rotary part ( 5 ), wherein the force transfer element ( 15 ) forms a single part with the inner rotary wing ( 6 , 16 ).
13. The subdivided stabilizer according to claim 11 wherein the inner rotary wing ( 16 ) is disposed an a radial plane together with the outer rotary wing ( 14 ) of the outer rotary part ( 4 ′), wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) extend over a certain axial length, wherein the inner rotary wing ( 16 ) and the outer rotary wing are of such dimensions and disposed such to each other that the inner rotary wing ( 16 ) and the outer rotary ring ( 14 ) form two radially and oppositely disposed free spaces ( 18 ) between themselves.
14. The subdivided stabilizer according to claim 11 wherein the cover flange ( 8 , 8 ′) is furnished on an inner side in a finite bearing hole ( 11 ) for receiving the second stabilizing part ( 2 , 2 ′) with its inner rotary part ( 5 ),
wherein
a bearing cover ( 9 ) comprises a passing through bearing bore ( 12 ) for receiving of the inner rotary part ( 5 ),
wherein
both the bearing cover ( 9 ) and the cover flange ( 8 , 8 ′) are attached at the outer rotary part ( 4 ) with screws or by a welding connection,
wherein the inner rotary wing ( 6 ) is attached at the inner rotary part ( 5 ) by gear teeth or by clamping.
15. A subdivided stabilizer
with optimized spring rate,
comprising
a first stabilizer part ( 1 , 1 ′);
a cover flange ( 8 ′), wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 ′);
an outer rotary part ( 4 ′), wherein the cover flange ( 8 ′) is formed at the outer rotary part ( 4 ′);
an outer rotary wing ( 14 ) attached to the outer rotary part ( 4 ′), wherein the outer rotary wing ( 14 ) is radially inwardly directed;
an inner rotary wing ( 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed;
an inner rotary part ( 5 ′), wherein the inner rotary wing ( 6 , 16 ) is attached to the inner rotary part ( 5 ′);
a second stabilizer part ( 2 , 2 ′), wherein the second stabilizer part ( 2 , 2 ′) is attached to the inner rotary part ( 5 ′), wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) moves relative the inner rotary part ( 5 ′) with the inner rotary wing ( 16 ) up to a point where the outer rotary wing ( 14 ) contacts the inner rotary wing ( 16 ), and wherein the first stabilizer part ( 1 , 1 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ), wherein the inner rotary part ( 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a movable coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ); wherein the second stabilizer part ( 2 ′) is formed as a single piece with the inner rotary part ( 5 ′),
wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) are freely rotatable relative to each other in a region of the free spaces ( 18 ) until the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) come to rest at a mutual stop.
16. The subdivided stabilizer according to claim 15
wherein the second stabilizer part ( 2 , 2 ′) and the inner rotary part ( 5 , 5 ′)are furnished by a round rod; and
wherein the first stabilizer part ( 1 , 1 ′) is at its end axially aligned attached to the cover flange ( 8 , 8 ′).
17. The subdivided stabilizer according to claim 15 further comprising
a bearing cover ( 9 ) attached to the outer rotary part ( 4 , 4 ′),
wherein the outer rotary part ( 4 ) with its outer rotary wing ( 14 ) and the inner rotary part ( 5 ) with its inner rotary wing ( 6 ) find an axial closure through the cover flange ( 8 ) connected with the first stabilizer part ( 1 , 1 ′) and through the bearing cover ( 9 ), wherein the free spaces between the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) are formed as pressure chambers sealed toward the outside and inside in a corresponding way and connected to a hydraulic plant.
18. The subdivided stabilizer according to claim 15 further comprising
a bearing cover ( 9 , 9 ′), wherein the outer rotary part has the shape of a cylindrical casing, wherein the outer rotary part ( 4 , 4 ′) is covered on a front side through a cover flange ( 8 ′), wherein the cover flange ( 8 ′) is connected fixedly against rotation to the first stabilizer part ( 1 , 1 ′), wherein the outer rotary part ( 4 , 4 ′) is delimited an a second front side with the bearing cover ( 9 , 9 ′), wherein the inner rotary part ( 5 , 5 ′) is supported in a bore hole of the bearing cover ( 9 , 9 ′) and in a recess of the cover flange ( 8 , 8 ′).
19. The subdivided stabilizer according to claim 15 wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) are intersected by a common radial plane.
20. The subdivided stabilizer according to claim 15 wherein the movable coupling piece ( 19 ) comprises
two equal and oppositely disposed coupling parts ( 21 ) equipped with side ways and conically extending guide faces, wherein the coupling parts ( 21 ) are capable of closing the free spaces ( 18 ) between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) without play;
wherein the coupling parts ( 21 ) are disengaged in the decoupled state from the outer rotary wing ( 14 ) and from the inner rotary wing ( 16 ) such that initially a free angle of rotation has to be overcome for each direction in case of a different load of the first stabilizer part ( 1 , 1 ′) and of the second stabilizer part ( 2 , 2 ′) before the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) come to rest.
21. A subdivided stabilizer
with optimized spring rate,
comprising
a first stabilizer part ( 1 , 1 ′);
a cover flange ( 8 ′), wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 ′);
an outer rotary part ( 4 ′), wherein the cover flange ( 8 ′) is formed at the outer rotary part ( 4 ′);
an outer rotary wing ( 14 ) attached to the outer rotary part ( 4 ′), wherein the outer rotary wing ( 14 ) is radially inwardly directed;
an inner rotary wing ( 6 , 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed;
an inner rotary part ( 5 ′), wherein the inner rotary wing ( 6 , 16 ) is attached to the inner rotary part ( 5 ′);
a second stabilizer part ( 2 , 2 ′), wherein the second stabilizer part ( 2 , 2 ′) is attached to the inner rotary part ( 5 , 5 ′), wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) moves relative the inner rotary part ( 5 , 5 ′) with the inner rotary wing ( 6 , 16 ) up to a point where the outer rotary wing ( 14 ) contacts the inner rotary wing ( 6 , 16 ), and wherein the first stabilizer part ( 1 , 1 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the outer rotary wing ( 14 ) and the inner rotary wing ( 6 , 16 ), wherein the inner rotary part ( 5 , 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a movable coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 6 , 16 ); wherein the second stabilizer part ( 2 ′) is formed as a single piece with the inner rotary part ( 5 , 5 ′),
a bearing cover ( 9 ) attached to the outer rotary part ( 4 , 4 ′),
wherein the outer rotary part ( 4 ) with its outer rotary wing ( 14 ) and the inner rotary part ( 5 , 5 ) with its inner rotary wing ( 6 , 16 ) find an axial closure through the cover flange ( 8 ) connected with the first stabilizer part ( 1 , 1 ′) and through the bearing cover ( 9 ), wherein the free spaces between the outer rotary wing ( 14 ) and the inner rotary wing ( 6 , 16 ) are formed as pressure chambers sealed toward the outside and inside in a corresponding way and connected to a hydraulic plant,
wherein the cover flange ( 8 ) is furnished on an inner side in a finite bearing hole ( 11 ) for receiving the second stabilizing part ( 2 ) with its inner rotary part ( 5 , 5 ′),
wherein
the bearing cover ( 9 ) comprises a passing through bearing bore ( 12 ) for receiving of the inner rotary part ( 5 , 5 ′),
wherein
both the bearing cover ( 9 ) and the cover flange ( 8 ) are attached at the outer rotary part ( 4 ) with screws or by a welding connection,
wherein the inner rotary wing ( 6 ) is attached an the inner rotary part ( 5 , 5 ′) by gear teeth or by clamping.
22. The subdivided stabilizer according to claim 21 wherein the inner rotary part ( 5 ) forms one part with the second stabilizer ( 2 , 2 ′) and is supported by the bearing cover ( 9 ) and the cover flange ( 8 ).
23. The subdivided stabilizer according to claim 21 wherein the movable coupling piece ( 19 ) comprises
two equal and oppositely disposed coupling parts ( 21 ) equipped with side ways and conically extending guide faces, wherein the coupling parts ( 21 ) are capable of closing the free spaces ( 18 ) between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) without play;
wherein the coupling parts ( 21 ) are disengaged in the decoupled state from the outer rotary wing ( 14 ) and from the inner rotary wing ( 16 ) such that initially a free angle of rotation has to be overcome for each direction in case of a different load of the first stabilizer part ( 1 , 1 ′) and of the second stabilizer part ( 2 , 2 ′) before the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) come to rest.
24. The subdivided stabilizer according to claim 21 wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) are freely rotatable relative to each other in a region of the free spaces ( 18 ) until the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) come to rest at a mutual stop.
25. The subdivided stabilizer with optimized spring rate,
comprising
a first stabilizer part ( 1 , 1 ′);
a cover flange ( 8 ′), wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 ′);
an outer rotary part ( 4 ′), wherein the cover flange ( 8 ′) is formed at the outer rotary part ( 4 ′);
an outer rotary wing ( 14 ) attached to the outer rotary part ( 4 ′), wherein the outer rotary wing ( 14 ) is radially inwardly directed;
an inner rotary wing ( 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed;
an inner rotary part ( 5 ′), wherein the inner rotary wing ( 6 , 16 ) is attached to the inner rotary part ( 5 ′);
a second stabilizer part ( 2 , 2 ′), wherein the second stabilizer part ( 2 , 2 ′) is attached to the inner rotary part ( 5 ′), wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) moves relative the inner rotary part ( 5 ′) with the inner rotary wing ( 16 ) up to a point where the outer rotary wing ( 14 ) contacts the inner rotary wing ( 16 ), and wherein the first stabilizer part ( 1 , 1 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ), wherein the inner rotary part ( 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a movable coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ); wherein the second stabilizer part ( 2 ′) is formed as a single piece with the inner rotary part ( 5 ′),
a bearing cover ( 9 ) attached to the outer rotary part ( 4 , 4 ′),
wherein the outer rotary part ( 4 ) with its outer rotary wing ( 14 ) and the inner rotary part ( 5 ) with its inner rotary wing ( 6 ) find an axial closure through the cover flange ( 8 ) connected with the first stabilizer part ( 1 , 1 ′) and through the bearing cover ( 9 ), wherein the free spaces between the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) are formed as pressure chambers sealed toward the outside and inside in a corresponding way and connected to a hydraulic plant,
a compression spring ( 22 ) supported at the bearing cover ( 9 ′) and disposed in a spring chamber ( 23 ), wherein the spring chamber ( 23 ) is formed as a pressure space and connected to a hydraulic plant through an inlet connection piece ( 24 ),
wherein
the coupling piece ( 19 ) is loadable with a hydraulic pressure created in the spring chamber ( 23 ) opposing the compression spring ( 22 ) on the side disposed remote from the compression spring ( 22 ),
wherein the hydraulic pressure supports the force of the compression spring ( 22 ),
wherein a corresponding inlet opening ( 25 ) for a hydraulic pressure creation is disposed in the cover flange ( 8 ′).
26. The subdivided stabilizer according to claim 25 wherein the movable coupling piece ( 19 ) comprises
two equal and oppositely disposed coupling parts ( 21 ) equipped with side ways and conically extending guide faces, wherein the coupling parts ( 21 ) are capable of closing the free spaces ( 18 ) between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) without play;
wherein the coupling parts ( 21 ) are disengaged in the decoupled state from the outer rotary wing ( 14 ) and from the inner rotary wing ( 16 ) such that initially a free angle of rotation has to be overcome for each direction in case of a different load of the first stabilizer part ( 1 , 1 ′) and of the second stabilizer part ( 2 , 2 ′) before the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) come to rest.
27. The subdivided stabilizer according to claim 25 wherein the second stabilizer part ( 2 , 2 ′) and the inner rotary part ( 5 , 5 ′)are furnished by a round rod; and
wherein the first stabilizer part ( 1 , 1 ′) is at its end axially aligned attached to the cover flange ( 8 , 8 ′).
28. The subdivided stabilizer according to claim 25 wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) are freely rotatable relative to each other in a region of the free spaces ( 18 ) until the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) come to rest at a mutual stop.
29. The subdivided stabilizer according to claim 25 wherein the inner rotary part ( 5 ) forms one part with the second stabilizer ( 2 , 2 ′) and is supported by the bearing cover ( 9 ) and the cover flange ( 8 ).
30. The subdivided stabilizer according to claim 25 wherein the inner rotary wing ( 16 ) is disposed an a radial plane together with the outer rotary wing ( 14 ) of the outer rotary part ( 4 ′), wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) extend over a certain axial length, wherein the inner rotary wing ( 16 ) and the outer rotary wing are of such dimensions and disposed such to each other that the inner rotary wing ( 16 ) and the outer rotary ring ( 14 ) form two radially and oppositely disposed free spaces ( 18 ) between themselves.
31. A subdivided stabilizer
with optimized spring rate,
comprising
a first stabilizer part ( 1 , 1 ′);
a cover flange ( 8 ′), wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 ′);
an outer rotary part ( 4 ′), wherein the cover flange ( 8 ′) is formed at the outer rotary part ( 4 ′);
an outer rotary wing ( 14 ) attached to the outer rotary part ( 4 ′), wherein the outer rotary wing ( 14 ) is radially inwardly directed;
an inner rotary wing ( 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed;
an inner rotary part ( 5 ′), wherein the inner rotary wing ( 6 , 16 ) is attached to the inner rotary part ( 5 ′);
a second stabilizer part ( 2 , 2 ′), wherein the second stabilizer part ( 2 , 2 ′) is attached to the inner rotary part ( 5 ′), wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) moves relative the inner rotary part ( 5 ′) with the inner rotary wing ( 16 ) up to a point where the outer rotary wing ( 14 ) contacts the inner rotary wing ( 16 ), and wherein the first stabilizer part ( 1 , 1 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ), wherein the inner rotary part ( 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a movable coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ); wherein the second stabilizer part ( 2 ′) is formed as a single piece with the inner rotary part ( 5 ′),
wherein the movable coupling piece ( 19 ) comprises
a guide part ( 20 ) and two equal and oppositely disposed coupling parts ( 21 ) equipped with side ways and conically extending guide faces, wherein the coupling parts ( 21 ) are capable of closing the free spaces ( 18 ) between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) without play.
32. The subdivided stabilizer according to claim 27 further comprising
a force transfer element ( 15 ) connected fixed against rotation to the inner rotary part ( 5 ), wherein the force transfer element ( 15 ) forms a single part with the inner rotary wing ( 16 ).
33. The subdivided stabilizer according to claim 31 wherein the movable coupling piece ( 19 ) comprises
two equal and oppositely disposed coupling parts ( 21 ) equipped with side ways and conically extending guide faces, wherein the coupling parts ( 21 ) are capable of closing the free spaces ( 18 ) between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) without play;
wherein the coupling parts ( 21 ) are disengaged in the decoupled state from the outer rotary wing ( 14 ) and from the inner rotary wing ( 16 ) such that initially a free angle of rotation has to be overcome for each direction in case of a different load of the first stabilizer part ( 1 , 1 ′) and of the second stabilizer part ( 2 , 2 ′) before the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) come to rest.
34. The subdivided stabilizer according to claim 31 wherein the cover flange ( 8 ) is furnished on an inner side in a finite bearing hole ( 11 ) for receiving the second stabilizing part ( 2 ) with its inner rotary part ( 5 ),
wherein
a bearing cover ( 9 ) comprises a passing through bearing bore ( 12 ) for receiving of the inner rotary part ( 5 ),
wherein
both the bearing cover ( 9 ) and the cover flange ( 8 ) are attached at the outer rotary part ( 4 ) with screws or by a welding connection,
wherein the inner rotary wing ( 6 ) is attached an the inner rotary part ( 5 ) by gear teeth or by clamping.
35. The subdivided stabilizer according to claim 27 further comprising
a compression spring ( 22 ) supported at a bearing cover ( 9 ′) and disposed in a spring chamber ( 23 ), wherein the spring chamber ( 23 ) is formed as a pressure space and connected to a hydraulic plant through an inlet connection piece ( 24 ),
wherein
the coupling piece ( 19 ) is loadable with a hydraulic pressure created in the spring chamber ( 23 ) opposing the compression spring ( 22 ) an the side disposed remote from the compression spring ( 22 ),
wherein the hydraulic pressure supports the force of the compression spring ( 22 ),
wherein a corresponding inlet opening ( 25 ) for a hydraulic pressure creation is disposed in the cover flange ( 8 ′).
36. The subdivided stabilizer according to claim 27 further comprising
a bearing cover ( 9 , 9 ′), wherein the outer rotary part has the shape of a cylindrical casing, wherein the outer rotary part ( 4 , 4 ′) is covered an a front side through a cover flange ( 8 ′), wherein the cover flange ( 8 ′) is connected fixedly against rotation to the first stabilizer part ( 1 , 1 ′), wherein the outer rotary part ( 4 , 4 ′) is delimited an a second front side with the bearing cover ( 9 , 9 ′), wherein the inner rotary part ( 5 , 5 ′) is supported in a bore hole of the bearing cover ( 9 , 9 ′) and in a recess of the cover flange ( 8 , 8 ′).
37. The subdivided stabilizer according to claim 31 wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) are intersected by a common radial plane.
38. A subdivided stabilizer
with optimized spring rate,
comprising
a first stabilizer part ( 1 , 1 ′);
a cover flange ( 8 ′), wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 ′);
an outer rotary part ( 4 ′), wherein the cover flange ( 8 ′) is formed at the outer rotary part ( 4 ′);
an outer rotary wing ( 14 ) attached to the outer rotary part ( 4 ′), wherein the outer rotary wing ( 14 ) is radially inwardly directed;
an inner rotary wing ( 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed;
an inner rotary part ( 5 ′), wherein the inner rotary wing ( 6 , 16 ) is attached to the inner rotary part ( 5 ′);
a second stabilizer part ( 2 , 2 ′), wherein the second stabilizer part ( 2 , 2 ′) is attached to the inner rotary part ( 5 ′), wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) moves relative the inner rotary part ( 5 ′) with the inner rotary wing ( 16 ) up to a point where the outer rotary wing ( 14 ) contacts the inner rotary wing ( 16 ), and wherein the first stabilizer part ( 1 , 1 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ), wherein the inner rotary part ( 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a movable coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ); wherein the second stabilizer part ( 2 ′) is formed as a single piece with the inner rotary part ( 5 ′),
a sensor ( 26 ) for determining a position of the movable coupling piece ( 19 ) disposed in the outer rotary part ( 4 ′).
39. The subdivided stabilizer according to claim 38 further comprising
a force transfer element ( 15 ) connected fixed against rotation to the inner rotary part ( 5 ), wherein the force transfer element ( 15 ) forms a single part with the inner rotary wing ( 16 ).
40. The subdivided stabilizer according to claim 38 wherein the movable coupling piece ( 19 ) comprises
two equal and oppositely disposed coupling parts ( 21 ) equipped with side ways and conically extending guide faces, wherein the coupling parts ( 21 ) are capable of closing the free spaces ( 18 ) between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) without play;
wherein the coupling parts ( 21 ) are disengaged in the decoupled state from the outer rotary wing ( 14 ) and from the inner rotary wing ( 16 ) such that initially a free angle of rotation has to be overcome for each direction in case of a different load of the first stabilizer part ( 1 , 1 ′) and of the second stabilizer part ( 2 , 2 ′) before the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) come to rest.
41. The subdivided stabilizer according to claim 38 wherein the second stabilizer part ( 2 , 2 ′) and the inner rotary part ( 5 , 5 ′) are furnished by a round rod; and
wherein the first stabilizer part ( 1 , 2 ′) is at its end axially aligned attached to the cover flange ( 8 , 8 ′).
42. The subdivided stabilizer according to claim 38 wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) are freely rotatable relative to each other in a region of the free spaces ( 18 ) until the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) come to rest at a mutual stop.
43. The subdivided stabilizer according to claim 38 further comprising
a bearing cover ( 9 ) attached to the outer rotary part ( 4 , 4 ′),
wherein the outer rotary part ( 4 ) with its outer rotary wing ( 14 ) and the inner rotary part ( 5 ) with its inner rotary wing ( 6 ) find an axial closure through the cover flange ( 8 ) connected with the first stabilizer part ( 1 , 1 ′) and through the bearing cover ( 9 ), wherein the free spaces between the outer rotary wing ( 14 ) and the inner rotary wing ( 6 ) are formed as pressure chambers sealed toward the outside and inside in a corresponding way and connected to a hydraulic plant.
44. The subdivided stabilizer according to claim 38 wherein the cover flange ( 8 ) is furnished on an inner side in a finite bearing hole ( 11 ) for receiving the second stabilizing part ( 2 ) with its inner rotary part ( 5 ),
wherein
a bearing cover ( 9 ) comprises a passing through bearing bore ( 12 ) for receiving of the inner rotary part ( 5 ),
wherein
both the bearing cover ( 9 ) and the cover flange ( 8 ) are attached at the outer rotary part ( 4 ) with screws or by a welding connection,
wherein the inner rotary wing ( 6 ) is attached an the inner rotary part ( 5 ) by gear teeth or by clamping.
45. The subdivided stabilizer according to claim 38 further comprising
a compression spring ( 22 ) supported at a bearing cover ( 9 ′) and disposed in a spring chamber ( 23 ), wherein the spring chamber ( 23 ) is formed as a pressure space and connected to a hydraulic plant through an inlet connection piece ( 24 ),
wherein
the coupling piece ( 19 ) is loadable with a hydraulic pressure created in the spring chamber ( 23 ) opposing the compression spring ( 22 ) an the side disposed remote from the compression spring ( 22 ),
wherein the hydraulic pressure supports the force of the compression spring ( 22 ),
wherein a corresponding inlet opening ( 25 ) for a hydraulic pressure creation is disposed in the cover flange ( 8 ′).
46. The subdivided stabilizer according to claim 38 wherein the movable coupling piece ( 19 ) comprises
a guide part ( 20 ) and two equal and oppositely disposed coupling parts ( 21 ) equipped with side ways and conically extending guide faces, wherein the coupling parts ( 21 ) are capable of closing the free spaces ( 18 ) between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) without play.
47. The subdivided stabilizer according to claim 38 further comprising
a bearing cover ( 9 , 9 ′), wherein the outer rotary part has the shape of a cylindrical casing, wherein the outer rotary part ( 4 , 4 ′) is covered an a front side through a cover flange ( 8 ′), wherein the cover flange ( 8 ′) is connected fixedly against rotation to the first stabilizer part ( 1 , 1 ′), wherein the outer rotary part ( 4 , 4 ′) is delimited an a second front side with the bearing cover ( 9 , 9 ′), wherein the inner rotary part ( 5 , 5 ′) is supported in a bore hole of the bearing cover ( 9 , 9 ′) and in a recess of the cover flange ( 8 , 8 ′).
48. The subdivided stabilizer according to claim 38 wherein the inner rotary wing ( 16 ) is disposed an a radial plane together with the outer rotary wing ( 14 ) of the outer rotary part ( 4 ′), wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) extend over a certain axial length, wherein the inner rotary wing ( 16 ) and the outer rotary wing are of such dimensions and disposed such to each other that the inner rotary wing ( 16 ) and the outer rotary ring ( 14 ) form two radially and oppositely disposed free spaces ( 18 ) between themselves.
49. The subdivided stabilizer according to claim 38 wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) are intersected by a common radial plane.
50. A subdivided stabilizer
with optimized spring rate,
comprising
a first stabilizer part ( 1 , 1 ′);
a cover flange ( 8 ′), wherein the first stabilizer part ( 1 , 1 ′) is formed as a single piece with the cover flange ( 8 ′);
an outer rotary part ( 4 ′), wherein the cover flange ( 8 ′) is formed at the outer rotary part ( 4 ′);
an outer rotary wing ( 14 ) attached to the outer rotary part ( 4 ′), wherein the outer rotary wing ( 14 ) is radially inwardly directed;
an inner rotary wing ( 16 ), wherein the inner rotary wing ( 6 , 16 ) is radially outwardly directed;
an inner rotary part ( 5 ′), wherein the inner rotary wing ( 6 , 16 ) is attached to the inner rotary part ( 5 ′);
a second stabilizer part ( 2 , 2 ′), wherein the second stabilizer part ( 2 , 2 ′) is attached to the inner rotary part ( 5 ′), wherein the outer rotary part ( 4 ′) with the outer rotary wing ( 14 ) moves relative the inner rotary part ( 5 ′) with the inner rotary wing ( 16 ) up to a point where the outer rotary wing ( 14 ) contacts the inner rotary wing ( 16 ), and wherein the first stabilizer part ( 1 , 1 ′) and the second stabilizer part ( 2 , 2 ′) are connected to each other with the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ), wherein the inner rotary part ( 5 ′) is rotatable relative to the outer rotary part ( 4 ′) to a predetermined extent, wherein free spaces ( 18 ) for a movable coupling piece ( 19 ) exist between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ); wherein the second stabilizer part ( 2 ′) is formed as a single piece with the inner rotary part ( 5 ′),
wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) come to rest on a mutual stop.
51. The subdivided stabilizer according to claim 50 further comprising
a force transfer element ( 15 ) connected fixed against rotation to the inner rotary part ( 5 ), wherein the force transfer element ( 15 ) forms a single part with the inner rotary wing ( 16 ).
52. The subdivided stabilizer according to claim 50 wherein the cover flange ( 8 ) is furnished on an inner side in a finite bearing hole ( 11 ) for receiving the second stabilizing part ( 2 ) with its inner rotary part ( 5 ),
wherein
a bearing cover ( 9 ) comprises a passing through bearing bore ( 12 ) for receiving of the inner rotary part ( 5 ),
wherein
both the bearing cover ( 9 ) and the cover flange ( 8 ) are attached at the outer rotary part ( 4 ) with screws or by a welding connection,
wherein the inner rotary wing ( 6 ) is attached an the inner rotary part ( 5 ) by gear teeth or by clamping.
53. The subdivided stabilizer according to claim 50 further comprising
a compression spring ( 22 ) supported at a bearing cover ( 9 ′) and disposed in a spring chamber ( 23 ), wherein the spring chamber ( 23 ) is formed as a pressure space and connected to a hydraulic plant through an inlet connection piece ( 24 ),
wherein
the coupling piece ( 19 ) is loadable with a hydraulic pressure created in the spring chamber ( 23 ) opposing the compression spring ( 22 ) an the side disposed remote from the compression spring ( 22 ),
wherein the hydraulic pressure supports the force of the compression spring ( 22 ),
wherein a corresponding inlet opening ( 25 ) for a hydraulic pressure creation is disposed in the cover flange ( 8 ′).
54. The subdivided stabilizer according to claim 50 wherein the inner rotary part ( 5 ) forms one part with the second stabilizer ( 2 , 2 ′) and is supported by a bearing cover ( 9 ) and the cover flange ( 8 ).
55. The subdivided stabilizer according to claim 50 wherein the movable coupling piece ( 19 ) comprises
a guide part ( 20 ) and two equal and oppositely disposed coupling parts ( 21 ) equipped with side ways and conically extending guide faces, wherein the coupling parts ( 21 ) are capable of closing the free spaces ( 18 ) between the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) without play.
56. The subdivided stabilizer according to claim 50 further comprising
a sensor ( 26 ) for determining a position of the movable coupling piece ( 19 ) disposed in the outer rotary part ( 4 ′).
57. The subdivided stabilizer according to claim 50 wherein the inner rotary wing ( 16 ) is disposed an a radial plane together with the outer rotary wing ( 14 ) of the outer rotary part ( 4 ′), wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) extend over a certain axial length, wherein the inner rotary wing ( 16 ) and the outer rotary wing are of such dimensions and disposed such to each other that the inner rotary wing ( 16 ) and the outer rotary ring ( 14 ) form two radially and oppositely disposed free spaces ( 18 ) between themselves.
58. The subdivided stabilizer according to claim 50 wherein the outer rotary wing ( 14 ) and the inner rotary wing ( 16 ) are intersected by a common radial plane.