Interface between knife and knife holder
09737942 · 2017-08-22
Assignee
Inventors
Cpc classification
Y10T83/9401
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T83/9464
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B26D2001/0046
PERFORMING OPERATIONS; TRANSPORTING
B26D2210/02
PERFORMING OPERATIONS; TRANSPORTING
B26D2003/286
PERFORMING OPERATIONS; TRANSPORTING
B23D61/10
PERFORMING OPERATIONS; TRANSPORTING
International classification
B23D61/10
PERFORMING OPERATIONS; TRANSPORTING
B26D7/26
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The invention relates to an interface between a knife and a knife holder, wherein the knife and the knife holder are designed such that the knife can be mounted on the knife holder in such a way that the knife is initially positioned on the knife holder in the axial direction, and then by rotating either the knife relative to the knife holder and/or the knife holder relative to the knife, the knife is locked on the knife holder with respect to the axial direction, wherein the knife has a single central fastening opening which is delimited by a knife edge region, and the knife holder has a fastening section for the fastening opening of the knife, which is delimited by a holder edge region.
Claims
1. A system comprising: a blade for a high-speed slicer, the blade being configured for rotation about a rotational axis and configured for attachment to a blade mount of the slicer by first moving the blade in an axial direction parallel to the rotational axis to place the blade on the blade mount and then securing the blade in the axial direction by rotating the blade about the rotational axis and relative to the blade mount and/or by rotating the blade mount about the rotational axis and relative to the blade, wherein: the blade has a single fastening opening defined by an opening edge for attachment to the blade mount; the opening edge has a non-circular shape; the opening edge defines a plurality of blade projections arranged in intervals along the fastening opening and extending radially inward toward the rotational axis; the plurality of blade projections have a uniform thickness in the axial direction; at least two adjacent ones of the plurality of blade projections each has an undercut, the undercuts forming a pocket that extends in a peripheral direction; the pocket is configured to receive a pair of pins on the blade mount and extend partially around a perimeter surface of the pins; and the blade mount, which is configured such that the blade is attachable thereto by first setting the blade is-onto the blade mount in the axial direction and subsequently locking the blade with respect to the axial direction at the blade mount by rotating the blade relative to the blade mount and/or by rotating the blade mount relative to the blade, wherein: the pins engage the undercuts in the two adjacent ones of the plurality of blade projections to prevent the blade from rotating relative to the blade mount; and at least one of the pins is preloaded by a spring that causes the pin to move upward into the pocket formed by the undercuts when the pocket is above the pin.
2. A system in accordance with claim 1, wherein the blade has the same axial thickness at the opening edge as in an inner blade region adjacent to the opening edge.
3. A system in accordance with claim 2, wherein the opening edge is flush with the inner blade region at a rear side of the blade and/or at a front side of the blade.
4. A system in accordance with claim 1, wherein the blade is configured to be locked to the blade mount via a bayonet fastening.
5. A system in accordance with claim 4, wherein the opening edge differs from a circular shape and is configured as a component of the bayonet fastening.
6. A system in accordance with claim 4, wherein the plurality of blade projections are configured as a component of the bayonet fastening.
7. A system in accordance with claim 1, wherein the blade has an anti-rotation mechanism.
8. A system in accordance with claim 7, wherein the anti-rotation mechanism comprises the undercut in each of the at least two adjacent ones of the plurality of blade projections.
9. A system in accordance with claim 1, wherein the plurality of blade projections are configured as a component of an attachment aid, with the opening edge having an asymmetrical portion that differs from a remaining extent of the opening edge.
10. A system in accordance with claim 9, wherein the opening edge has exactly one asymmetrical portion at which the opening edge differs from the remaining extent.
11. A system in accordance with claim 9, wherein the asymmetrical portion includes a blade tab which differs with respect to its shape and/or size from other blade projections of the opening edge.
12. A system in accordance with claim 1, wherein at least one of: a radius of a fastening opening amounts to at least 1/10 of a greatest radius of the blade; and an area of the fastening opening amounts to at least ⅙ of a total area of the blade.
13. A system in accordance with claim 1, wherein the blade mount has a fastening section for a fastening opening of the blade which is bounded by a marginal mount region.
14. A system in accordance with claim 1, wherein at least one of: a marginal mount region has a larger axial dimension than a marginal blade region; and a marginal blade region and a ring forming the marginal mount region cooperate with one another such that as the blade is set onto the blade mount in the axial direction, a rotation of the blade is suppressed until the marginal blade region has passed the ring.
15. A system in accordance with claim 1, wherein an axial spacing between a contact plane and a locking plane of the blade mount is larger in at least a release state of the blade mount than the axial thickness of a marginal blade region bounding a fastening opening.
16. A system in accordance with claim 15, wherein the axial spacing is smaller than 1 mm, or smaller than 0.5 mm, or smaller than 0.3 mm, or smaller than 0.1 mm.
17. A system in accordance with claim 1, wherein the entire opening edge has a uniform thickness in the axial direction.
18. A system in accordance with claim 1, wherein one of the pins is stationary and the other one of the pins is preloaded by the spring.
Description
DRAWINGS
(1) The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.
(2) The invention will be described in the following by way of example with reference to the drawings. There are shown:
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
(11)
DETAILED DESCRIPTION
(12) Example embodiments will now be described more fully with reference to the accompanying drawings.
(13)
(14) The margin of the fastening opening 12 is “frayed”. It in particular has a meandering shape. The margin of the fastening opening 12 can be of wave shape. Alternatively, it can be designed as star-shaped or, for example in the manner of a knurled-head screw. Other shapes are also conceivable.
(15) Sections which project further into the center of the scythe-like blade 10 thus alternate with sections which protrude less far into the center of the scythe-like blade 10. The blade 10 thus has an inwardly directed, non-circular contour. The sections, in particular blade projections 14, 14′, which project further into the center of the scythe-like blade 10, can be configured as lugs 14, 14′. They can, for example, be round or angled. The inwardly directed projections 14, 14′ can have the same axial thickness T1 (
(16) The blade projections 14, 14′ form a part of a bayonet fastening 16. It is also conceivable to arrange a plurality of bayonet fastenings 16.
(17) Two of the blade projections 14 form an anti-rotation mechanism 17. It has two cut-outs 18 which can also be considered as one cut-out 18 having two end regions in operative communication with one another.
(18) It is alternatively also conceivable only to use one cut-out 18 for the anti-rotation mechanism 17. A plurality of cut-outs 18 are also conceivable. While the remaining marginal region of the fastening opening 12, in particular the lugs 14, are symmetrical viewed in the peripheral direction, a lug 14′ is much larger. The lug 14′ so-to-say forms an open oval. At this point, the margin of the fastening opening 12 thus has an asymmetrical portion.
(19)
(20) The ring 22 in particular has recesses 24, 24′ and mount projections 26 (“teeth”) which alternate. They are shaped such that they correspond to the marginal blade region 13 in accordance with
(21) The ring 22 can in particular have at least one recess 24′ which extends over a longer section of the ring periphery than the remaining recesses 24. The recess 24′ can in particular receive the lug 14′. A plurality of recesses 24′ are also conceivable which can, for example, receive a plurality of lugs 14′. To set the blade 10 onto the blade mount 20, the blade 10 must thus be brought to the correct angular position.
(22) The blade mount 20 has at least one securing pin 28 which engages with shape matching into the anti-rotation mechanism 17. Two pins 28 are preferably provided of which, for example, one is movable and one is stationary. The pins 28 enter into engagement with the cut-outs 18 of the anti-rotation mechanism 17.
(23) The scythe-like blade 10 is therefore set onto the blade mount 20 by means of a handling apparatus, for example. The scythe-like blade 10 is in this respect rotated in such a manner until the lugs 14, 14′ correspond to the position of the recesses 24, 24′. The scythe-like blade 10 is now pushed over the ring 22 until it impacts the contact plane or section 30a of the second part 30 of the blade mount 20. After passing the ring 22, the scythe-like blade 10 can be rotated again. The scythe-like blade 10 is adjusted against the direction of rotation in cutting operation. Finally, the scythe-like blade 10 latches, for example via a securing pin 28, and is thus prevented from rotating. The scythe-like blade 10 is thus unambiguously positioned.
(24) The lugs 14, 14′ are now located beneath the projections 26 of the blade mount 20 due to the rotation. The inwardly directed contour of the blade 10 thus lies beneath the projections 26 and is prevented from an axial movement in this manner. Thus, the underside surfaces of the projections 26 are disposed within the locking plane or fastening section 22a of the ring 22. An axial spacing S1 (
(25) At least one of the pins 28 can in this respect be stationary, whereas the other can, for example, be preloaded via a spring and jumps upwardly when a cut-out 18 of the scythe-like blade 10 is located above it.
(26) The actuation of at least one of the pins 28 can e.g. take place via the mentioned handling apparatus of the blade 10.
(27) A counter-weight 32 is moreover shown in
(28) The shape of the counter-weight 32 can differ from the shape shown in
(29) Since the counter-weight 32 is not mounted at or in front of the scythe-like blade 10, the counter-weight does not have to be dismantled on a replacement of the scythe-like blade 10.
(30) The mass distribution can be set by the counter-weight 32. A balancing of the rotating total system is in particular thereby possible. A static balancing with respect to the axis of rotation is hereby generally ensured. A dynamic imbalance is also countered by the arrangement of the counter-weight 32 provided here.
(31)
(32) The blade mount 20 latches the contour, i.e. the lugs 14, 14′, of the blade 10 at its counter-contour, i.e. the projections 26. An axial movement of the scythe-like blade 10 is prevented by this bayonet fastening 16.
(33) For the final fastening of the scythe-like blade 10, the blade mount 20 can clamp the lugs 14, 14′ of the scythe-like blade 10. This is possible, for example, with the aid of screws within the blade mount 20. Alternatively, springs can also be used which are themselves tensioned by screws for clamping the lugs 14, 14′.
(34) For fastening the lugs 14, 14′, alternatively or additionally, a plate spring or a plate spring package 36 is also conceivable as the spring arrangement 36 which is shown in
(35) The blade 10 is thus clamped between the first part 23 and the second part 30 of the blade mount 20.
(36) The plate spring 36 can e.g. act directly on the lugs 14, 14′ of the scythe-like blade 10. The plate spring 36, however, preferably only acts indirectly via an inner side of the ring 22. This can have an inner projection 46 which is arranged between the plate spring 36 and the lugs 14, 14′ of the scythe-like blade 10. This is shown enlarged in
(37) Since the lugs 14, 14′ of the scythe-like blade 10 are acted on permanently due to the preload of the plate spring 36, the scythe-like blade 10 is permanently fixed.
(38) The clamping has to be actively overcome to remove the scythe-like blade 10 from the blade mount 20. If the actuation device used for this purpose fails, a secure clamping of the blade 10 is nevertheless ensured (safety clamping).
(39) It is moreover shown in
(40)
(41) A variant of the mentioned safety clamping is shown in
(42) A pneumatic device can, for example, be provided as the actuation device. In this respect, an inner space 44, 44′ is sealed and pressurized by the cover 50 which in particular simultaneously forms a part of the counter-weight 32, the ring 22 and the carrier 30. In this respect, the total inner space 44, 44′ containing the plate spring 36 is pressurized or is acted on by excess pressure. The plate spring 36 lies on an inner projection 46 of the ring 22. A membrane skin 48, which is also simply called a spring in the following, extends between the inner projection 46 and the carrier 30 and in particular connects these components in one piece. It seals the inner space 44, 44′ and in particular acts in the manner of a film hinge on an axial movement of the first part 23 relative to the second part 30. The ring 22, the inner projection 46, the membrane 48 and the carrier 30 can in particular be formed as a single-piece component.
(43) If the inner space 44, 44′ is pressurized, the cover 50 of the blade mount 20 moves upwardly. The ring 22 is in this respect taken along by the cover 50 and is likewise moved upwardly. The plate spring 36 is also moved upwardly radially outwardly against its preload by the inner projection 46 and is tensioned more in so doing. The plate spring 36 cannot move further upwardly radially inwardly since it contacts a stationary shoulder.
(44) The blade 10 thereby becomes free. The membrane 48 thus provides both a leak-tightness of the inner space 44, 44′ and the required relative movability of the components for cancelling the clamping state.
(45) Due to the use of a pneumatic system, screws are no longer required to fasten the blade 10.
(46) As an alternative to the pneumatic solution, a single screw 52 can also be used as the actuation device which is shown in
(47) The clamping of the blade can therefore be actively overcome purely mechanically and/or pneumatically.
(48) The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.