Cutting Blade and Method for Producing Such a Blade
US-2021291285-A1 · Sep 23, 2021 · US
US9676044B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9676044-B2 |
| Application number | US-201314135164-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 19, 2013 |
| Priority date | Dec 19, 2013 |
| Publication date | Jun 13, 2017 |
| Grant date | Jun 13, 2017 |
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A cutting tool and cutter body assembly, including a disk-shaped cutter body and a plurality of support pads removably retained therein, the cutter body having an axis of rotation, two opposing end surfaces and a body peripheral surface extending therebetween. Each support pad intersects one of two annular-shaped planes equidistantly offset from opposite sides of a median plane perpendicular to the axis of rotation, and the cutter body intersects neither of the two annular-shaped planes. Each support pad is configured to make operative contact with a machined surface of a workpiece perpendicular to the axis of rotation. Each support pad has opposing upper and lower surfaces and a pad peripheral surface extending therebetween, the pad peripheral surface having an upper portion intersecting the upper surface, and the upper portion exhibiting N-fold rotational symmetry about a pad axis non-perpendicular to the lower surface.
Opening claim text (preview).
What is claimed is: 1. A cutter body assembly ( 20 , 20 ′) comprising: a disk-shaped cutter body ( 22 ) and a plurality of support pads ( 24 , 24 ′) removably retained therein, the cutter body ( 22 ) having an axis of rotation (R), a direction of rotation (DR) about the axis of rotation (R), two opposing end surfaces ( 26 a , 26 b ) and a body peripheral surface ( 28 ) extending therebetween, and each of the plurality of support pads ( 24 , 24 ′) protruding from one of the two opposing end surfaces ( 26 a , 26 b ), wherein a median plane (M) perpendicular to the axis of rotation (R) intersects the body peripheral surface ( 28 ), and two annular-shaped planes (P 1 ) are equidistantly offset from opposite sides of the median plane (M) by a first distance (D 1 ), wherein each of the plurality of support pads ( 24 , 24 ′) intersects one of the two annular-shaped planes (P 1 ), and the cutter body ( 22 ) intersects neither of the two annular-shaped planes (P 1 ); and wherein not all of the plurality of support pads ( 24 , 24 ′) intersect the same annular-shaped plane (P 1 ). 2. The cutter body assembly ( 20 , 20 ′) according to claim 1 , wherein the median plane (M) intersects the body peripheral surface ( 28 ) along its entire circumference. 3. The cutter body assembly ( 20 , 20 ′) according to claim 1 , wherein the body peripheral surface ( 28 ) has a plurality of circumferentially spaced apart body recesses ( 30 ) equal in number to the plurality of support pads ( 24 , 24 ′), and wherein the median plane (M) intersects each of the plurality of body recesses ( 30 ). 4. The cutter body assembly ( 20 , 20 ′) according to claim 3 , wherein each of the plurality of body recesses ( 30 ) opens out to at least one of the two opposing end surfaces ( 26 a , 26 b ). 5. The cutter body assembly ( 20 , 20 ′) according to claim 3 , wherein each of the plurality of body recesses ( 30 ) opens out to both opposing end surfaces ( 26 a , 26 b ). 6. The cutter body assembly ( 20 , 20 ′) according to claim 3 , wherein the body peripheral surface ( 28 ) has a plurality of outer peripheral portions ( 34 ) circumferentially alternating with the plurality of body recesses ( 30 ), and each outer peripheral portion ( 34 ) intersects the median plane (M) to define the arc of a first pie-shaped sector (S 1 ) having a first center point (C 1 ) contained in the axis of rotation (R), and wherein each first pie-shaped sector (S 1 ) at least partially contains the axial projection of a single support pad ( 24 , 24 ′). 7. The cutter body assembly ( 20 , 20 ′) according to claim 6 , wherein the plurality of first pie-shaped sectors (S 1 ) are identical to each other. 8. The cutter body assembly ( 20 , 20 ′) according to claim 1 , wherein the plurality of support pads ( 24 , 24 ′) are identical to each other, and wherein an equal number of support pads ( 24 , 24 ′) intersect each of the two annular-shaped planes (P 1 ). 9. The cutter body assembly ( 20 , 20 ′) according to claim 1 , wherein two circumferentially adjacent support pads ( 24 , 24 ′) intersect different annular-shaped planes (P 1 ). 10. The cutter body assembly ( 20 , 20 ′) according to claim 1 , wherein the cutter body ( 22 ) has a plurality of pad pockets ( 40 ) for mounting and indexing the plurality of support pads ( 24 , 24 ′), and each support pad ( 24 , 24 ′) has an axially outermost point (NO) located a second distance (D 2 ) from the median plane (M), and wherein each support pad ( 24 , 24 ′) is indexable in its associated pad pocket ( 40 ) to increase or decrease the second distance (D 2 ). 11. The cutter body assembly ( 20 , 20 ′) according to claim 10 , wherein the second distance (D 2 ) is equal to or greater than the first distance (D 1 ). 12. The cutter body assembly ( 20 , 20 ′) according to claim 10 , wherein each pad pocket ( 40 ) has a planar seat surface ( 42 ) non-parallel to the median plane (M), and each support pad ( 24 ) has opposing upper and lower surfaces ( 44 , 46 ) and a pad peripheral surface ( 48 ) extending therebetween, and wherein each lower surface ( 46 ) abuts its associated seat surface ( 42 ) in each index position of the support pad ( 24 , 24 ′). 13. The cutter body assembly ( 20 , 20 ′) according to claim 12 , wherein each support pad ( 24 , 24 ′) is indexable about a pocket axis (A 1 ) perpendicular to its associated seat surface ( 42 ). 14. The cutter body assembly ( 20 , 20 ′) according to claim 13 , wherein each support pad ( 24 , 24 ′) is removably fastened in its associated pad pocket ( 40 ) by means of a fastening screw ( 58 ). 15. The cutter body assembly ( 20 ) according to claim 14 , wherein each support pad ( 24 ) has a protuberance ( 60 ) extending away from its lower surface ( 46 ), and wherein the fastening screw ( 58 ) threadingly engages a first threaded bore ( 60 ) in a distal surface ( 64 ) of the protuberance ( 60 ). 16. The cutter body assembly ( 20 ) according to claim 15 , wherein the first threaded bore ( 60 ) is coaxial with the pocket axis (A 1 ). 17. The cutter body assembly ( 20 , 20 ′) according to claim 12 , wherein each seat surface ( 42 ) forms an acute first inclination angle (α 1 ) with the median plane (M), and wherein the first inclination angle (α 1 ) has a value of less than 20 degrees. 18. The cutter body assembly ( 20 , 20 ′) according to claim 12 , wherein each pad peripheral surface ( 48 ) has an upper portion ( 50 ) intersecting its associated upper surface ( 44 ), and each upper portion ( 50 ) exhibits N-fold rotational symmetry about a pad axis (A 2 ), wherein each support pad ( 24 , 24 ′) has N index positions in its associated pad pocket ( 40 ), and wherein the pad axis (A 2 ) is non-perpendicular to its associated seat surface ( 42 ). 19. The cutter body assembly ( 20 , 20 ′) according to claim 18 , wherein each pad axis (A 2 ) forms an acute second inclination angle (α 2 ) with its associated seat surface ( 42 ), and wherein the second inclination angle (α 2 ) has a value of greater than 80 degrees. 20. The cutter body assembly ( 20 , 20 ′) according to claim 18 , wherein: said each upper portion ( 50 ) has N planar facets ( 50 ), and wherein at least three consecutive planar facets ( 54 ) about the pad axis (A 2 ) face an equal number of corresponding planar walls ( 56 ) in the associated pad pocket ( 40 ). 21. The cutter body assembly ( 20 , 20 ′) according to claim 12 , wherein the axially outermost point (NO) of each support pad ( 24 , 24 ′) is formed on its upper surface ( 44 ), and wherein each upper surface ( 44 ) is convexly shaped. 22. A cutting tool ( 70 ) comprising: a cutter body assembly ( 20 ) according to claim 1 ; and a plurality of cutting inserts ( 32 ) removably retained in the cutter body ( 22 ) and circumferentially spaced about the body peripheral surface ( 28 ), wherein each of the plurality of support pads ( 24 ) is configured to make operative contact with a machined surface ( 76 a , 76 b ) of a workpiece ( 78 ), and wherein the machined surface ( 76 a , 76 b ) is perpendicular to the axis of rotation (R). 23. The cutting tool ( 70 ) according to claim 22 , wherein the total number of support pads ( 24 ) and the total number of cutting inserts ( 32 ) are equal. 24. The cutting tool ( 70 ) according to claim 22 , wherein not all of the plurality of support pads ( 24 ) intersect the same annular-shaped
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