Reducing machine rotor assembly and inserts therefor and method of constructing the inserts
A comminuting machine rotor assembly comprising rotors carried by a shaft for conjoint rotation with the shaft, hammer heads carried by the rotors and extending radially outwardly from the shaft, and hammer inserts releasably attached to respective ones of the hammer heads. There is a wear material coating over at least a first cutting edge of an insert body of each insert. The first cutting edge of each insert body is defined by a front facet generally facing the direction of assembly rotation, a radially outer end facet adjacent the front facet, and an intervening radially distal corner of the hammer insert formed at the intersection of the front and end facets. The front and end facets are disposed at a relative angle of greater than 60 degrees to one another.
1. A rotor assembly for use in a comminuting machine for wood and the like, comprising;
a shaft arranged for driven rotation about an axis;
a plurality of rotors carried by the shaft in generally adjacent relation to one another for conjoint rotation with the shaft;
a plurality of hammer heads carried by the rotors and extending radially outwardly from the shaft; and
a plurality of hammer inserts releasably attached to respective ones of the hammer heads, each insert including an insert body and a welded-on abrasive wear material coating over at least a first cutting edge portion of the insert body of each hammer insert insert body, the first cutting edge of each insert body being defined by a front facet generally facing the direction of assembly rotation, a radially outer end facet adjacent the front facet, and an intervening radially distal corner of the hammer insert formed at the intersection of the front and end facets, the front facet being disposed at a relative included angle of greater than 60 degrees to the end facet.
2. The rotor assembly of claim 1 in which the relative included angle between the front facet and the adjacent end facet of each insert cutting edge is greater than or generally equal to 90 degrees.
3. The rotor assembly of claim 1 in which the front facet of each insert cutting edge is generally perpendicular to the end facet of each insert cutting edge.
4. The rotor assembly of claim 1 in which the front and end facets of each insert cutting edge are flat.
5. The rotor assembly of claim 1 in which the front facet of each insert cutting edge is generally parallel to a back surface of the insert.
6. The rotor assembly of claim 1 in which each insert includes a second cutting edge disposed opposite the first cutting edge, each insert being reversibly attachable to a hammer to interchangeably dispose the two cutting edges in either a radially-outward active cutting position or a radially-inward idle non-cutting position.
7. The rotor assembly of claim 6 in which the second cutting edge of each insert body is defined by a front facet generally facing the direction of assembly rotation, an end facet adjacent the front facet and opposite the end facet of the first cutting edge, and an intervening corner formed at the intersection of the front facet and the end facet, the front facet of the second cutting edge being disposed at a relative included angle of greater than 60 degrees to the end facet of the second cutting edge.
8. The rotor assembly of claim 7 in which the front facets of the opposite cutting edges are generally coplanar.