Mechanism and method for automatically transversely positioning the pinch-point of a concave

1. A transverse pivot assembly mechanism for automatically positioning a pinch-point of a concave relative to a rotor of a combine, the mechanism comprising:

a remotely operative adjustment mechanism coupled to one end of said concave; and

a linking assembly pivotally coupling another end of said concave to said combine, said linking assembly defining at least one transverse pivot axis, said transverse pivot axis allowing automatic remotely operative adjustment mechanism providing selective transverse pivoting of said concave along said transverse pivot axis and relative to said rotor in accordance with selectively defined clearance spacing between said concave and said rotor, wherein said linking assembly includes at least a first linking member and a second linking member, said first linking member and said second linking member substantially similar in shape, said first linking member being positioned substantially angular relative to said second linking member, wherein said substantially angular positioning of said first linking member relative to said second linking member defines a generally “X-shaped” configuration.

2. The transverse pivot assembly mechanism of claim 1 , wherein at least one of said first linking member and said second linking member is rigid.

3. The transverse pivot assembly mechanism of claim 1 , wherein at least one of said first linking member and said second linking member is flexible.

4. The transverse pivot assembly mechanism of claim 1 , wherein one of said first linking member and said second linking member has a greater length dimension than the other of said first linking member and said second linking member.

5. The transverse pivot assembly mechanism of claim 1 , wherein said linking assembly further includes at least a third linking member and a fourth linking member, said third linking member and said fourth linking member being substantially similar in shape, said third linking member being positioned substantially angular relative to said fourth linking member.

6. The transverse pivot assembly mechanism of claim 5 , wherein one of said third linking member and said fourth linking member has a greater length dimension than the other of said third linking member and said fourth linking member.

7. The transverse pivot assembly mechanism of claim 5 , wherein said substantially angular positioning of said third linking member relative to said fourth linking member defines a generally “X-shaped” configuration.

8. The transverse pivot assembly mechanism of claim 5 , wherein said linking assembly further includes at least a fifth linking member and a sixth linking member, said fifth linking member and said sixth linking member being substantially similar in shape, said fifth linking member being positioned substantially angular relative to said sixth linking member.

9. The transverse pivot assembly mechanism of claim 8 , wherein one of said fifth linking member and said sixth linking member has a greater length dimension than the other of said fifth linking member and said sixth linking member.

10. The transverse pivot assembly mechanism of claim 8 , wherein said substantially angular positioning of said fifth linking member relative to said sixth linking member defines a generally “X-shaped” configuration.

11. The transverse pivot assembly mechanism of claim 8 , wherein said first linking member, said third linking member, and said fifth linking member have substantially similar length dimensions, and wherein said second linking member, said fourth linking member, and said sixth linking member have substantially similar length dimensions.

12. The transverse pivot assembly mechanism of claim 11 , wherein said substantially angular positioning of said first linking member relative to said second linking member, said third linking member relative to said fourth linking member, and said fifth linking member relative to said sixth linking member define generally “X-shaped” configurations.

13. The transverse pivot assembly mechanism of claim 1 , wherein said first linking member includes a first end and a second end and said second linking member includes a First end and a second end, said first end of said first linking member being pivotally coupled to said concave and said second end of said first linking member being pivotally coupled to said combine, said first end of said second linking member being pivotally coupled to said concave and said second end of said second linking member being pivotally coupled to said combine.

14. The transverse pivot assembly mechanism of claim 13 , wherein said substaiitially angular positioning of said first linking member relative to said second linking member defines a generally “X-shaped” configuration.

15. The transverse pivot assembly mechanism of claim 13 , wherein said pivotal coupling of said first end of said first linking member to said concave is located in a diferent horizontal plane than said pivotal coupling of said first end of said second linking member to said concave.

16. The transverse pivot assembly mechanism of claim 13 , wherein said pivotal coupling of said second end of said first linking member to said combine is located in a different horizontal plane than said pivotal coupling of said second end of said second linking member to said combine.

17. The transverse pivot assembly mechanism of claim 13 , wherein said pivotal coupling of said first end of said first linking member to said concave is located in a different horizontal plane than said pivotal coupling of said first end of said second linking member to said concave, and wherein said pivotal coupling of said second end of said first linking member to said combine is located in a different horizontal plane than said pivotal coupling of said second end of said second linking member to said combine.

18. The transverse pivot assembly mechanism of claim 1 , wherein said linking assembly further includes at least a first mounting bracket mounted to said combine.

19. The transverse pivot assembly mechanism of claim 18 , wherein said first mounting bracket includes a plurality of mounting apertures said mounting apertures allowing accommodation of varying dimensions of linking members, concaves, and rotors.

20. The transverse pivot assembly mechanism of claim 18 , wherein said first linking member includes a first end and a second end and said second linking member includes a first end and a second end, said first end of said first linking member being pivotally coupled to said concave and said second end of said first linking member being pivotally coupled to said mounting bracket, said first end of said second linking member being pivotally coupled to said concave and said second end of said second linking member being pivotally coupled to said mounting bracket.

21. The transverse pivot assembly mechanism of claim 20 , wherein said substantially angular positioning of said first linking member relative to said second linking member defines a generally “X-shaped” configuration.

22. The transverse pivot assembly mechanism of claim 20 , wherein said pivotal coupling of said first end of said first linking member to said concave is located in a different horizontal plane than said pivotal coupling of said first end of said second linking member to said concave.

23. The transverse pivot assembly mechanism of claim 20 , wherein said pivotal coupling of said second end of said first linking member to said first mounting bracket is located in a different horizontal plane than said pivotal coupling of said second end of said second linking member to said first mounting bracket.

24. The transverse pivot assembly mechanism of claim 20 , wherein said pivotal coupling of said first end of said first linking member to said concave is located in a different horizontal plane than said pivotal coupling of said first end of said second linking member to said concave, and wherein said pivotal coupling of said second end of said first linking member to said first mounting bracket is located in a different horizontal plane than said pivotal coupling of said second end of said second linking member to said first mounting bracket.

25. A transverse pivot assembly mechanism for automatically positioning a pinch-point of a concave relative to a rotor of a combine, the mechanism comprising:

a linking assembly pivotally coupling said concave to said combine, said linking assembly defining at least one transverse pivot axis, said transverse pivot axis allowing automatic transverse pivot of said concave relative to said rotor in accordance with adjustably set clearance spacing between said concave and said rotor, said linking assembly including at least a first linking member and a second linking member, said first linking member and said second linking member being substantially similar in shape, said first linking member including a first end and a second end and said second linking member including a first end and a second end, at least a first mounting bracket mounted to said combine, said first mounting bracket including a plurality of mounting apertures, said mounting apertures allowing accommodation of varying dimensions of linking members, concaves, and rotors, wherein said first end of said first linking member is pivotally coupled to said concave and said second end of said first linking member is pivotally coupled to said first mounting bracket, and wherein said first end of said second linking member is pivotally coupled to said concave and said second end of said second linking member is pivotally coupled to said first mounting bracket, said first linking member being positioned substantially angular relative to said second linking member, wherein said substantially angular positioning of said first linking member relative to said second linking menber defines a generally “X-shaped” configuration.

26. The transverse pivot assembly mechanism of claim 25 , wherein said pivotal coupling of said first end of said first linking member to said concave is located in a different horizontal plane than said pivotal coupling of said first end of said second linking member to said concave, and wherein said pivotal coupling of said second end of said first linking member to said first mounting bracket is located in a different horizontal plane than said pivotal coupling of said second end of said second linking member to said first mounting bracket.

27. The transverse pivot assembly mechanism of claim 25 , wherein one of said first linking member and said second linking member has a greater length dimension than the other of said first linking member and said second linking member.

28. A transverse pivot assembly mechanism for automatically positioning a pinch-point of a concave relative to a rotor of a combine, the mechanism comprising:

a linking assembly pivotally coupling said concave to said combine, said linking assembly defining at least one transverse pivot axis, said transverse pivot axis allowing automatic transverse pivot of said concave relative to said rotor in accordance with adjustably set clearance spacing between said concave and said rotor, said linking assembly including at least a first linking member and a second linking member, said first linking member and said second linking member being substantially similar in shape, said first linking member including a first end and a second end and said second linking member including a first end and a second end, at least a first mounting bracket mounted to said combine, said first mounting bracket including a plurality of mounting apertures, said mounting apertures allowing accommodation of varying dimensions of linking members, concaves, and rotors, wherein said first end of said first linking member is pivotally coupled to said concave and said second end of said first linking member is pivotally coupled to said first mounting bracket, and wherein said first end of said second linking member is pivotally coupled to said concave and said second end of said second linking member is pivotally coupled to said first mounting bracket, said pivotal coupling of said first end of said first linking member to said concave being located in a different horizontal plane than said pivotal coupling of said first end of said second linking member to said concave, said pivotal coupling of said second end of said first linking member to said first mounting bracket being located in a different horizontal plane than said pivotal coupling of said second end of said second linking member to said first mounting bracket, said first linking member being positioned substantially angular relative to said second linking member, said substantially angular positioning of said first linking member relative to said second linking member defining a generally “X-shaped” configuration.

29. A rotary combine comprising:

a rotor having a longitudinal axis of rotation;

a concave including a first side and a second side, said concave spaced circumferentially around said rotor and comprising a plurality of concave inserts outwardly removable away from said rotor in a direction transverse to said longitudinal axis of said rotor;

a transverse pivot assembly mechanism coupling said first side of said concave to said combine, said transverse pivot assembly mechanism comprising:

a linking assembly pivotally coupling said concave to said combine, said linking assembly defining at least one transverse pivot axis, said transverse pivot axis allowing automatic transverse pivot of said concave relative to said rotor in accordance with adjustably set clearance spacing between said concave and said rotor, said linking assembly including at least a first linking member and a second linking member, said first linking member and said second linking member being substantially similar in shape, said first linking member being positioned substantially angular relative to said second linking member, wherein said substantially angular positioning of said first linking member relative to said second linking member defines a generally “X-shaped” configuration; and

an adjustment mechanism coupling said second side of said concave to said combine, said adjustment mechanism allowing adjustment of clearance spacing between said concave and said rotor.

30. The rotary combine of claim 29 , wherein one of said first linking member and said second linking member has a greater length dimension than the other of said first linking member and said second linking member.

31. The rotary combine of claim 29 , wherein said first linking member includes a first end and a second end and said second linking member includes a first end and a second end, said first end of said first linking member being pivotally coupled to said first side of said concave and said second end of said first linking member being pivotally coupled to said combine, said first end of said second linking member being pivotally coupled to said first side of said concave and said second end of said second linking member being pivotally coupled to said combine.

32. The rotary combine of claim 31 , wherein said substantially angular positioning of said first linking member relative to said second linking member defines a generally “X-shaped” configuration.

33. The rotary combine of claim 31 , wherein said pivotal coupling of said first end of said first linking member to said first side of said concave is located in a different horizontal plane than said pivotal coupling of said first end of said second linking member to said first side of said concave.

34. The rotary combine of claim 31 , wherein said pivotal coupling of said second end of said first linking member to said combine is located in a different horizontal plane than said pivotal coupling of said second end of said second linking member to said combine.

35. The rotary combine of claim 31 , wherein said pivotal coupling of said first end of said first linking member to said first side of said concave is located in a different horizontal plane than said pivotal coupling of said first end of said second linking member to said first side of said concave, and wherein said pivotal coupling of said second end of said first linking member to said combine is located in a different horizontal plane than said pivotal coupling of said second end of said second linking member to said combine.

36. The rotary combine of claim 29 , wherein said linking assembly further includes at least a first mounting bracket mounted to said combine, and wherein said first linking member includes a first end and a second end and said second linking member includes a first end and a second end, said first end of said first linking member being pivotally coupled to said first side of said concave and said second end of said first linking member being pivotally coupled to said first mounting bracket, said first end of said second linking member being pivotally coupled to said first side of said concave and said second end of said second linking member being pivotally coupled to said first mounting bracket.

37. The rotary combine of claim 36 , wherein said first mounting bracket includes a plurality of mounting apertures, said mounting apertures allowing accommodation of varying dimensions of linking members, concaves, and rotors.

38. The rotary combine of claim 36 , wherein said substantially angular positioning of said first linking member relative to said second linking member defines a generally “X-shaped” configuration.

39. The rotary combine of claim 36 , wherein said pivotal coupling of said first end of said first linking member to said first side of said concave is located in a different horizontal plane than said pivotal coupling of said first end of said second linking member to said first side of said concave.

40. The rotary combine of claim 36 , wherein said pivotal coupling of said second end of said first linking member to said first mounting bracket is located in a different horizontal plane than said pivotal coupling of said second end of said second linking member to said first mounting bracket.

41. The rotary combine of claim 36 , wherein said pivotal coupling of said first end of said first linking member to said first side of said concave is located in a different horizontal plane than said pivotal coupling of said first end of said second linking member to said first side of said concave, and wherein said pivotal coupling of said second end of said first linking member to said first mounting bracket is located in a different horizontal plane than said pivotal coupling of said second end of said second linking member to said first mounting bracket.

42. A method for automatically transversely pivoting and positioning a pinch-point of a concave relative to a rotor of a combine, the method comprising the steps of:

providing a rotor having a longitudinal axis of rotation;

providing at least one concave, said concave including a first side and a second side spaced circumferentially around said rotor and including a plurality of concave inserts outwardly removable away from said rotor in a direction transverse to said longitudinal axis of said rotor;

providing a transverse pivot assembly mechanism, said transverse pivot assembly mechanism coupling said first side of said concave to said combine, said transverse pivot assembly mechanism comprising:

a linking assembly pivotally coupling said first side of said concave to said combine, said linking assembly defining at least one transverse pivot axis, said transverse pivot axis allowing automatic transverse pivot of said concave relative to said rotor in accordance with adjustably set clearance spacing between said concave and said rotor, said linking assembly including at least a first linking member and a second linking member, said first linking member and said second linking member being substantially similar in shape, said first linking member being positioned substantially angular relative to said second linking member, wherein said substantially angular positioning of said first linking member relative to said second linking member defines a generally “X-shaped” configuration;

providing a remotely operative adjustment mechanism, said remotely operative adjustment mechanism adjustably coupling said second side of said concave to said combine for effecting movement and clearance spacing of said concave relative to said rotor of said combine; and

selectively actuating said remotely operative adjustment mechanism to effect movement and clearance spacing of said concave relative to said rotor of said combine.