Claims
- 1. A method for replacing a concave insert in a rotary combine, said method comprising:providing a rotor having a longitudinal extent and a longitudinal axis of rotation; providing a support structure disposed adjacent said rotor; providing a longitudinally extending frame comprising first and second sides spaced circumferentially around said rotor and at least a first and second rib member extending transversely between said first and second sides of said frame, said first and second rib members longitudinally spaced apart and defining an opening therebetween; providing at least a first and second concave insert, each of said first and second concave inserts comprising a first and second end spaced circumferentially around said rotor, said first end of said first concave insert releasably secured to said first side of said frame and said first end of said second concave insert releasably secured to said second side of said frame, said each of said first and second concave inserts dimensioned to pass through said opening in an outwardly, transverse direction relative to said rotor; removing said first concave insert through said opening; providing a replacement concave insert having a first and second end; inserting said replacement concave insert through said opening.
- 2. The invention of claim 1 wherein said second ends of said first and second concave inserts are abuttingly engaged.
- 3. The invention of claim 1 wherein said frame further comprises a longitudinally extending frame member connecting said first and second rib members intermediate said first and second sides of said frame, wherein said second ends of said first and second concave inserts abut opposite sides of said frame member.
- 4. The invention of claim 1 wherein said first side comprises a longitudinally extending support shaft, and wherein said first end of said first concave insert is releasably and pivotally engaged with said support shaft on said first side of said frame, wherein said step of removing said first concave insert comprises pivoting said first concave insert through said opening about said support shaft on said first side of said frame.
- 5. The invention of claim 4 wherein said first end of said first concave insert and said replacement concave insert comprises a hook dimensioned to pivotally engage said shaft on said first side of said frame.
- 6. The invention, of claim 4 wherein said first and second rib members each have a first and second end, said first and second sides of said frame comprising said first and second ends of said first and second ribs respectively, wherein said shaft on said first side of said frame connects said first ends of said first and second rib members.
- 7. A method for replacing a concave insert in a rotary combine, said method comprising:providing a rotor having a longitudinal extent and a longitudinal axis of rotation; providing at least a first and second concave, each of said first and second concave comprising a first and second end spaced circumferentially around said rotor, said first end of said first concave releasably, pivotally mounted about a first pivot axis, said first pivot axis substantially parallel to said axis of rotation of said rotor, and said first end of said second concave releasably, pivotally mounted about a second pivot axis substantially parallel to said axis of rotation of said rotor, said second pivot axis circumferentially spaced around said rotor from said first pivot axis; pivoting said second end of said first concave around said first pivot axis in an outwardly, transverse direction relative to said rotor; disengaging said first end of said first concave from said structure at said first pivot axis; providing a replacement concave having a first and second end; engaging said first end of said replacement concave with said structure at said first pivot axis; pivoting said second end of said replacement concave about said first pivot axis in an inwardly transverse direction relative to said rotor.
Parent Case Info
This is a divisional of application Ser. No. 09/503,512 filed on Feb. 14, 2000, now U.S. Pat. No. 6.358,142.
US Referenced Citations (7)
Foreign Referenced Citations (1)
Number |
Date |
Country |
55153846 |
Nov 1991 |
JP |