U.S. patent application number 11/514098 was filed with the patent office on 2007-01-04 for method of adjusting an anti-wind wiper assembly.
Invention is credited to Craig E. Murray, Mark J. Svitak, Dale R. Tanis.
Application Number | 20070004478 11/514098 |
Document ID | / |
Family ID | 37071278 |
Filed Date | 2007-01-04 |
United States Patent
Application |
20070004478 |
Kind Code |
A1 |
Tanis; Dale R. ; et
al. |
January 4, 2007 |
Method of adjusting an anti-wind wiper assembly
Abstract
An anti-wind wiper including an extension adjustably mountable
in a desired spaced relation and angular orientation relative to a
leading edge of a flight of a front rotor inlet section of a
combine, for interaction with the flight during rotation of the
rotor, for directing and guiding crop material, particularly long
strand-like elements of crop material, away from a shaft and
bearing supporting the inlet section.
Inventors: |
Tanis; Dale R.; (Geneseo,
IL) ; Murray; Craig E.; (Geneseo, IL) ;
Svitak; Mark J.; (Colona, IL) |
Correspondence
Address: |
CNH AMERICA LLC
INTELLECTUAL PROPERTY LAW DEPARTMENT
PO BOX 1895, M.S. 641
NEW HOLLAND
PA
17557
US
|
Family ID: |
37071278 |
Appl. No.: |
11/514098 |
Filed: |
August 31, 2006 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
|
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11097899 |
Apr 1, 2005 |
|
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11514098 |
Aug 31, 2006 |
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Current U.S.
Class: |
460/68 |
Current CPC
Class: |
A01F 7/06 20130101; A01F
12/10 20130101 |
Class at
Publication: |
460/068 |
International
Class: |
A01F 12/00 20060101
A01F012/00 |
Claims
1-28. (canceled)
29. A method of adjusting an anti-wind wiper assembly for
preventing winding of plant material around structure supporting a
front inlet section of a rotor of an agricultural combine,
comprising the steps of: orienting the extension on the structure
so as to extend in a direction of rotation of the rotor in a
predetermined axially spaced position in relation to a radially
outwardly extending leading edge of at least one helical flight of
the inlet end; and fixedly mounting the extension on the structure
in the position.
30. The method of claim 29, comprising the further step of
adjustably positioning the extension in a predetermined angular
orientation in relation to the leading edge and mounting the
extension to the structure in the predetermined angular
orientation.
31. The method of claim 29, wherein the structure comprises a
shroud extending at least partially around the axis and including a
radially outwardly facing wiper surface, and the extension is
mounted on the wiper surface.
Description
[0001] This divisional application claims priority under 35 U.S.C.
.sctn. 120 from co-pending U.S. patent application Ser. No.
11/097,899 filed on Apr. 1, 2005 by Dale R. Tanis et al. with the
same title, the full disclosure of which is hereby incorporated by
reference.
TECHNICAL FIELD
[0002] The present invention relates generally to an agricultural
combine rotor, and more particularly, to an adjustable extension
for an anti-wind wiper for a support for a front rotor inlet
section, for interaction with flights on the front rotor inlet
section, for directing crop material, and particularly long strand
like elements of crop material, away from a shaft and bearing
supporting the inlet section.
BACKGROUND ART
[0003] A well-known form of harvesting machine is a rotary combine.
A typical combine includes a crop harvesting apparatus which reaps
grain stalks and other plant materials and feeds them to a
separating or threshing apparatus. The grain stalks or other crop
and plant materials harvested in the field are moved rearwardly
from a crop harvesting header assembly and introduced for threshing
to the rotor assembly by a crop feeder assembly.
[0004] In a rotary combine, the rotor assembly includes a generally
tubular rotor housing mounted in the combine body. A driven rotor
is coaxially mounted within the housing. The rotor comprises an
infeed or inlet section and a cylindrical threshing section, and is
supported at opposite ends by front and rear bearing
assemblies.
[0005] The cylindrical threshing section of the rotor and the rotor
housing mount cooperating threshing elements, which separate grain
from other material in a threshing zone. The crop material is
threshed as it spirals around the rotor threshing section and
passes through openings in the rotor housing.
[0006] As discussed in Tanis U.S. Pat. No. 5,387,153, assigned to
the same assignee as the present invention, the ability to transfer
crop materials from the feeder assembly to the threshing zone of
the rotor assembly is a key to efficient combine operations. Most
rotary combine rotors include an infeed or inlet section impeller
comprised of a series of impeller blades or flights arranged at a
forward end of the rotor. The impeller flights rotate within a
housing which is a part of the rotor housing. During harvesting
operations, the generally linear movement of the crop materials
received from the feeder assembly is converted by the rotating
impeller flights into a rotating, circulatory movement, in a
rearward and outward direction.
[0007] When rotary combines are used on certain long-stemmed
leguminous or grassy crops, such as windrowed perennial or annual
rye grass, clover, and bent grass, and oats, there is a potential
for portions of such grassy crops and other plant materials such as
weeds to extend into the impeller flights while other portions
remain partially engaged with the feeder assembly. The latter
portions tend to move toward the axis of rotation of the rotor
assembly, and may wrap about the front rotor bearing or shaft. This
can rob power and cause damaging heat build up around the bearing,
potentially causing premature failure thereof.
[0008] Long-stemmed leguminous or grassy crops also have a tendency
to wrap around or "hairpin" about the leading edge of the impeller
blades or flights. This hairpinning action can create a buildup of
crop materials on the aforementioned leading edge, which reduces
the effectiveness of the impeller and further reduces combine
efficiency.
[0009] Numerous front rotor inlet and bearing housing designs,
including that disclosed in the above referenced Tanis patent, have
been proposed to prevent crop materials from becoming entangled
with the front rotor bearing and prevent hairpinning about the
impeller blades' leading edges. None has been thoroughly successful
in doing so, however.
[0010] Tanis U.S. Pat. No. 6,296,566, also assigned to the same
assignee as the present invention, discloses an infeed impeller for
a rotary combine which utilizes anti-winding vanes on the rotor
which cooperate with vanes on the front bearing assembly to force
debris radially outwardly away from the axis of the rotor. However,
this combination has been found to also suffer from the
above-discussed shortcomings, more particularly, that long,
particularly wet, crop material winds onto the rotor shaft which
creates heat, consumes power, and causes early bearing failures.
Additionally, hairpinning of such long grassy crop material about
the leading edges of the impeller blades or flights can result in
irregular wear in the form of scalloping of the leading edges,
which can impede smooth flow of crop material radially outwardly
along the leading edges.
[0011] Accordingly, what is sought is a front bearing housing
anti-wind element and/or front rotor inlet section which provides
improved anti-wind characteristics, particularly with regard to
long, wet straw and other crop material.
SUMMARY OF THE INVENTION
[0012] What is disclosed is a front bearing housing anti-wind
element which provides improved anti-wind characteristics,
particularly with regard to long, wet straw and other crop
material.
[0013] According to a preferred aspect of the invention, an
adjustable anti-wind wiper is disclosed, including an elongate
wiper extension having a first longitudinal end portion adjustably
mountable on structure supporting an inlet end of a rotor of a
combine for rotation about a rotational axis, such that the wiper
extension will extend generally radially outwardly in relation to
the axis, to an opposite second end portion of the wiper extension.
When so mounted, the extension is in predetermined axially spaced
relation to a radially outwardly extending leading edge of an inlet
flight of the rotor, and can optionally also be oriented at a
desired angle in relation thereto. The preferred wiper extension
has a longitudinal edge extending between the longitudinal end
portions of the extension, the extension being adjustably movable
during the mounting thereof, for positioning the longitudinal edge,
and also a wiper surface of the extension, in a desired axially
spaced relation to the leading edge of the inlet flight, and
optionally, in a desired angular orientation in relation thereto,
the extension then being fixedly securable to the structure.
[0014] As a result, the relationship, both axially spaced, and
angular, of the extension to a leading edge of one or more inlet
flights of a rotor can be customized and adjusted for such
conditions as manufacturing tolerances and wear. The wiper
extension also allows making adjustments to the spacing between the
extension and an inlet flight as required or desired, and
replacement of the extension when worn and/or damaged.
BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Preferred aspects of the invention, including of its
construction and method of operation, are illustrated more or less
diagrammatically in the drawings, in which:
[0016] FIG. 1 is a side elevational view of a portion of a rotary
combine, showing in partial section a crop feeder assembly, and a
threshing rotor including a front inlet section thereof and a front
bearing housing shroud assembly, including an adjustable anti-wind
wiper extension according to preferred aspects of the
invention;
[0017] FIG. 2 is an enlarged fragmentary side view of the rotor and
front inlet section of FIG. 1;
[0018] FIG. 3 is a perspective view of the wiper extension of FIG.
1, showing elements for installation on the shroud assembly, shown
in dotted lines;
[0019] FIG. 4 is a side view of the front rotor inlet section of
FIG. 1, showing the wiper extension in relation thereto;
[0020] FIG. 5 is another perspective view of the rotor, shroud
assembly and wiper extension of FIG. 1;
[0021] FIG. 6 is a front view of the front rotor inlet section and
the front bearing housing and shroud of FIG. 1, illustrating a
relationship between the extension and a flight of the rotor in one
rotational position;
[0022] FIG. 7 is another front view of the front rotor inlet
section and the front bearing housing and shroud of FIG. 1, showing
a relationship between the extension and a flight of the rotor in
another rotational position;
[0023] FIG. 8 is another front view of the front rotor inlet
section and the front bearing housing and shroud of FIG. 1, showing
a relationship between the extension and a flight of the rotor in
another rotational position;
[0024] FIG. 9 is another front view of the front rotor inlet
section and the front bearing housing and shroud of FIG. 1, showing
a relationship between the extension and a flight of the rotor in
still another rotational position; and
[0025] FIG. 10 is a high level flow diagram of steps of a method of
the invention.
DETAILED DESCRIPTION OF THE INVENTION
[0026] Referring now to the drawings, in FIG. 1 a self-propelled
rotary combine is seen generally at 10. Combine 10 includes a front
portion 12 including front wheels 14, an operator cab 16, and an
engine (not shown) suitably supported within a body 18. The
transfer of power from the engine to various driven components of
combine 10 is effected conventionally.
[0027] Combine 10 is provided with a crop harvesting header
assembly 20 for cutting and gathering crop materials. Header
assembly 20 cuts and directs the crop material into a crop feeder
assembly 22 including a conveyor 24. Conveyor 24 carries the crop
material upwardly toward a rotor assembly 26, which threshes grain
from material other than the grain. Rot or assembly 26 is supported
in a conventional manner inside body 18. Rotor assembly 26 includes
a tubular rotor housing 28 mounted in a front to rear orientation
in body 18. A rotor 30 is mounted in housing 28 for rotation
therein in a predetermined rotational direction about a rotational
axis 32 through rotor 30 oriented at an acute angle to horizontal
as shown.
[0028] Referring also to FIG. 2, rotor 30 is a hollow drum
including a threshing section 34 and a front inlet section 36.
Front inlet section 36 includes two helical impeller auger flights
38 extending therearound in a rearward direction from a front
center portion 40 to threshing section 34. Front inlet section 36
has a conical shape, extending radially outwardly relative to axis
32 rearwardly from adjacent to front center portion 40 to threshing
section 34. Rotor 30 is rotatable in rotor housing 28 in a
rotational direction denoted by arrow A, which is a
counterclockwise direction when viewed from the front. Each
impeller auger flight 38 includes a leading edge 42 which extends
radially outwardly with respect to axis 32 from a radial outer
circumferential edge of front center portion 40 having a
predetermined radial extent, and terminating at a radial outer edge
44. Edges 42 are raked or swept back in relation to rotational
direction A. Each impeller auger has a helical pitch that increases
in the rearward direction along the length thereof, which enables
auger flight 38 to aggressively move plant material rearwardly from
feeder assembly 22 during rotation of rotor 30, while leading edges
42 are disposed and rotate in closely axially spaced relation to a
shroud 46 which extends around and protects a front bearing housing
48 (FIGS. 3 and 5) carrying a front bearing 50 (FIG. 5) for
supporting a shaft 52, which, in turn, supports inlet section 36
and flights 38 of rotor 30 for rotation.
[0029] More particularly referring to FIGS. 3, 4 and 5, shroud 46
is mounted on a support arm 54 frontwardly of inlet section 36 of
rotor 30, and is preferably integrally formed or cast with front
bearing housing 48. Front bearing housing 48 contains and carries
conventional bearing 50 for rotatably supporting shaft 52 for
rotation about axis 32, shaft 52 being affixed to and rotatably
carrying and supporting inlet section 36 in the conventional
manner. Shroud 46 has a curved radial outer wiper surface 56
extending at least partially therearound, and a rearwardmost curved
anti-wind wiper edge 58 disposed so as to be spaced just marginally
frontwardly of front center portion 40 and leading edges 42 of
flights 38. Radial outer wiper surface 56 includes an elongate
adjustable anti-wind wiper extension member 60 according to the
invention, that extends generally radially outwardly preferably at
least generally tangentially from surface 56 in the rotational
direction denoted by arrows A and includes a longitudinally
extending wiper edge 62 which partially overlays or forms an
extension of anti-wind wiper edge 58.
[0030] Extension member 60 of the invention includes a
longitudinally extending radial outer wiper surface 64 having a
convex, curved shape which overlays a portion of wiper surface 56
of shroud 46, and extends generally radially outwardly in direction
of rotation A beyond wiper surface 56, effectively forming an
extension thereof. Wiper surface 56 and wiper edge 58 of shroud 46,
and wiper edge 62 and wiper surface 64 of extension member 60 are
preferably curved so as to extend gradually radially outwardly in
rotational direction A about axis 32, so as to be capable of
smoothly guiding crop material brought into contact therewith by
rotation of auger flights 38, particularly long crop material such
as grassy strands of crop material hairpinned about leading edges
42, radially outwardly and away from the vicinity of front bearing
housing 48 and shaft 32, preferably to radial outer edge 44, where
the crop material will be released from leading edges 42, so as to
be carried rearwardly by flights 38. As a result of the radial
outward movement of the crop material along leading edges 42 to the
radial outer ends thereof, the crop material is not concentrated at
any one location therealong, such that occurrences of sawing or
abrading of any one portion, or location along, leading edges 42 by
the crop material is eliminated. Here, it should be understood that
by the term "hairpinning", what is meant is that the long strands
or other elements of the crop material bend about leading edges 42
of flights 38, such that a portion of the long element is in front
of the flight, and a portion is rearward of the flight.
[0031] This is best illustrated in reference to FIGS. 6, 7, 8 and
9, wherein the relative rotational positions of an auger flight 38
and shroud 46 about axis 32 is shown. The view in each of FIGS. 6,
7, 8 and 9 is looking rearward. In FIG. 6, flight 38 is shown at a
lower rotational position wherein leading edge 42 thereof is spaced
below shroud 46 and is rotating in direction A toward wiper surface
64 of extension member 60. Long crop material, denoted collectively
by B, is shown hairpinned about leading edge 42. In FIG. 7, leading
edge 42 of flight 38 is rotating in direction A about axis 32,
along wiper surface 64 of extension 60, such that more radially
inwardly located elements of the crop material B are in contact
with, and moving in direction A with flight 38 along wiper surface
64. Because wiper surface 64 extends radially outwardly in
direction A, the crop material in contact therewith is being urged
radially outwardly thereby, along leading edge 42, as denoted by
arrow C. Here, it should be noted that the included angle between
leading edge 42 and surface 64 is greater than 90.degree. such that
radial outward movement of the crop material B along edge 42 is not
impeded, and scissoring action is not occurring. In FIG. 8, flight
38 is shown rotated to a more upwardly oriented position along
surface 64 of extension 60, leading edge 42 still being oriented at
at least a 90.degree. angle to surface 64. Here, it can be observed
that crop material B is still being moved radially outwardly along
leading edge 42, as denoted by arrow C. And, in FIG. 9, flight 38
is shown at a rotational position wherein surface 64 of extension
member 60 has reached a radial outermost end of leading edge 42
adjacent to radial outer edge 44, such that crop material B will be
released from leading edge 42 so as to be carried rearwardly by the
flight. From a sequential review of FIGS. 6, 7, 8 and 9, it should
be evident that crop material carried into contact with extension
member 60 and carried along surface 64 thereof by leading edge 42
of flight 38 will be progressively urged radially outwardly toward
radial outer edge 44, as denoted by arrows C, so as to be released
from leading edge 42 and carried rearwardly on the oppositely
facing surface of flight 38, toward threshing section 34. Here, it
can also be observed that extension member 60 has a first
longitudinal end portion 66 mounted in overlaying relation to wiper
surface 56 of shroud 46, relatively close to axis 32, and that
extension member 60, edge 62 and wiper surface 64 extend generally
progressively radially outwardly in rotational direction A along
wiper surface 56 to a second longitudinal end portion 68 of member
60 which is located radially outwardly of a radial outermost
portion of shroud 46 in rotational direction A. Thus, a significant
extension of shroud 46 is provided, which, in relation to the
radial outward extent of leading edge 42 of each flight 38,
provides a capability of guiding and urging crop material radially
outwardly along leading edge 42 of each flight during the rotation
thereof, sufficiently so as to be released therefrom, particularly
if bent or hairpinned thereover.
[0032] Ref erring more particularly to FIGS. 1, 2 and 4, it is
evident that some axial space or gap must exist between wiper edges
58 and 62 of shroud 46 and extension member 60, and leading edges
42 of flights 38, such that there is no contact therebetween. As a
result of manufacturing and assembly tolerances when installing a
rotor 30 in the support structure therefor, namely, shroud 46 and
bearing housing 48 on support arm 54, variances in such axial space
or gap can exist. Additionally, as a result of use, particularly
with more abrasive varieties of crops, leading edges 42 can be
abraded away to some extent, as can wiper edge 58 and other
surfaces of shroud 46, and the corresponding surfaces on extension
member 60 when used. Thus, both at installation, and subsequently
after periods of use, the gap and angular relationship between
leading edges 42 and edge 58 of shroud 46, and edge 62 of extension
member 60, when used, can change. Additionally, shroud 46, surface
56 and edge 58 thereof can be damaged from contact with other
material which may be inadvertently inducted with the harvested
crop materials, such as rocks, fence posts, animal carcasses and
skeletal remains, and the like which may be fed by feeder assembly
22 into rotor housing 28. Accordingly, for the above reasons, it
has been found that it is desirable to provide an extension member
60 for shrouds such as shroud 46, and further, for such an
extension member 60 to be adjustably mountable in relation to
shroud 46 to achieve desired performance, and/or to compensate for
the above-described variances, wear and possible damage, and it is
replaceable if required, by a duplicate extension member, or one
that has one or more different characteristics or properties.
Additionally, by usage of an extension member installable in the
manner as described herein, such installation, and adjustment can
be achieved without major disassembly of the support structure for
the inlet end of the rotor.
[0033] Referring more particularly to FIGS. 2, 3 and 4, another
advantage of extension member 60 is that it can be installed at or
in a desired or required position and/or angular orientation in
relation to a desired or required reference, such as in a desired
or required position and/or orientation in relation to fixed
structure such as a reference on support arm 54 or shroud 46, or,
more preferably, in a desired or required axially spaced relation
and/or orientation in relation to a leading edge 42 of one or more
of inlet flights 38. In particular, it is anticipated that utility
would be achieved by positioning wiper edge 62 at a predetermined
distance, denoted by distance D in FIG. 4, from the leading edge 42
of one or both flights 38, which distance have a nominal value, for
instance, of about 2.3 millimeters, or a range of distances, for
instance, from about 2.0 to about 3.0 millimeters. An angular
orientation of wiper edge 62 in relation to a reference such as
leading edge 42, as illustrated by angle E in relation to leading
edge 42 in FIG. 2, or a line transverse or perpendicular to axis
32, can also be specified, as desired or required for a particular
application. For instance, angle E can have a nominal value of 0
degrees, and a predetermined range or tolerance of 1 or 2 degrees
therefrom. Here, it should be noted that the values set forth for
distance D and angle E are not limiting, and may differ for
different applications. To facilitate and enable such variable
mountability of extension member 60 on shroud 46, first end portion
66 of member 60 is preferably mounted on surface 56 of shroud using
suitable mounting elements, such as, but not limited to fasteners
70 which here are shown as bolts, which extend through washers 72,
and axially elongate holes 74 through first end portion 66, and are
threadedly received in threaded holes 76 in surface 56 of shroud
46.
[0034] In FIG. 10, steps of installation of extension member 60 are
illustrated. In step 78, the extension is loosely installed, for
instance using fasteners 70, to allow adjusting the position of the
extension in relation to a selected reference, such as a leading
edge 42 of a flight 38 as discussed above. In step 80, the position
of the extension is adjusted, for instance, such that a clearance
value, (distance D in FIG. 4) is the desired amount. In Step 82,
the extension is secured in position, for instance, by tightening
fasteners 70. In step 84, a test is performed, for instance, by
spinning rotor 30, to ensure the desired position of extension is
achieved. If it is, the installation is coomplete.
[0035] Here, it should also be noted that the terms "rearward" and
"rearwardly" are used in respect to rotor 30, as denoting toward
the threshing end thereof, and not with respect to the rearward end
of combine 10, as it is recognized that rotor 30 could be oriented
otherwise than front to rearwardly with respect to combine 10, such
as in a side to side orientation therein. Additionally, it should
be noted that the terms "radial" and "radially" are used with
respect to axis 32.
[0036] It will be understood that changes in the details,
materials, steps, and arrangements of parts which have been
described and illustrated to explain the nature of the invention
will occur to and may be made by those skilled in the art upon a
reading of this disclosure within the principles and scope of the
invention. The foregoing description illustrates the preferred
embodiment of the invention; however, concepts, as based upon the
description, may be employed in other embodiments without departing
from the scope of the invention. Accordingly, the following claims
are intended to protect the invention broadly as well as in the
specific form shown.
* * * * *