CA2550141C - Differential connecting rod and draft cable for agricultural tillage device - Google Patents

Abstract

The invention discloses a differential connecting rod and draft cable for an agricultural tillage device. The invention consists of a differential connecting rod which is positioned parallel to the center frame. The center frame is connected to the inner wing frame by a universal joint. The universal joint has a spherical bearing and a pivot. The pivot is positioned in a slot. The differential control rod positions the pivot in the slot. An 'L'- shaped linkage and a spring assembly pivotally support the rod. The draft cable is attached to the center frame hitch and outer wing. It is supported in the center by a folding support arm. This allows the wire to be moved when the cultivator is being transported. The draft cable transfers the draft force exerted on the outer wing to the center frame hitch.

Description

DIFFERENTIAL CONNECTING ROD AND
DRAFT CABLE FOR AGRICULTURAL TILLAGE DEVICE
This is a divisional of application serial number 2,287,627 filed October 26, 1999.
Field of the Invention This invention relates to the improvement of an agricultural ground-working cultivator.
More specifically it relates to an improvement of the centre frame of a cultivator and support for a pair of opposing wings on the said cultivator.

Background of the Invention The need to till and cultivate soil for the planting of crops has been accomplished since the earliest days of civilisation. More recently, tillage devices have increased in complexity and size, depending on the type of crops, quantity and soil being tilled. There has also been an increased emphasis on conserving natural resources resulting in these concerns being integrated in modern tillage systems. These concerns have resulted in larger and more complex tillage systems that assist in achieving these goals.
A larger tillage system allows a single operator to perform tillage operations on a greater area.
More sophisticated tillage systems further allow for the accomplishment of low till and no till farming techniques. Low till and no till farming encourages tilling, planting and fertilising in a single pass of the tillage device or cultivator through the field. By only disturbing the soil a single time, there is less soil compaction, less moisture loss, less pesticides and herbicides needed and less fertiliser required. However, these larger and more complex tillage systems create complexities that were previously unknown in the art.

Previously, an agricultural tractor could pull a relatively small tillage device or cultivator.
As the tillage device or cultivator moved over hills and similar undulations in the terrain all the ground-working implements maintained contact with the soil. The width of the tillage device was sufficiently small for it generally not to have problems maintaining ground contact. However, as the tillage devices were increased in width, so as to be able to till a greater area in a single pass, the undulations in the ground resulted in the ground-working tools failing always to contact the earth.

Furthermore, to transport the tillage device or cultivator for the farming operations it was necessary for the device to be capable of being collapsed to a width sufficient to be moved. To accomplish these goals, a centre section with. a set of pivotable wings was designed. The wings could pivot horizontally relative to the centre section allowing the tillage device to accommodate some undulations in the ground. The wings could also be folded into the centre section allowing for easy transport before and after farming operations. Eventually, an outer set of wings was added increasing the width of the tillage device.

Figure 1 illustrates the general configuration of a tillage device or cultivator. Specifically, there is a centre section directly behind the tractor. There is a set of inner wings and outer wings respectively surrounding the centre section. Some cultivators are folded into the transport position along an axis along the direction of travel; other cultivators are folded along a diagonal axis.

In prior art cultivators, the wings can rotate on an axis in the direction of travel, the wings generally cannot rotate, flex or bend on an axis perpendicular to travel.
Finally, the additional inner wings and outer wings create large additional draft forces on the frame of the cultivator, draft forces being those created when the ground-working tool is pulled through the soil.

These are complex problems to overcome, especially when considering the need for the tillage device to be a collapsed from its field operation mode to the compact transportation mode.

Consequently, the need exists for a linkage, which allows for the inner wings to move transversely to the centre section of a tillage device. The need also exists for a means to help distribute the draft load generated by the outer wings.

Summary of the Invention The present invention relates to an agricultural cultivator having a central section flanked by wings which are connected to the centre section in such a manner that in addition to being able to pivot relative the centre section about an axis parallel to the direction of travel of the cultivator may pivot relative to the centre section about a horizontal axis transverse to the direction of travel of the cultivator.

The invention provides an agricultural cultivator coniprising: a. a hitch frame and a drawbar frame including a drawbar center frame and a drawbar wing frame; b.
said drawbar center frame pivotally attached to the hitch frame on a transverse axis for rotation between a downward working position and an upward transport position;
and c. said drawbar wing frame being attached to a side of the drawbar center frame by a multi-joint assembly whereby: i. the multi-joint assembly is attached to the drawbar center frame defining a first axis perpendicular to the drawbar center frame;
ii. the multi-joint assembly is attached to the drawbar wing frame defining a second axis perpendicular to the first axis and perpendicular to the drawbar wing frame; and iii. the multi-joint assembly includes a third axis generally longitudinal to the drawbar wing frame.

In a preferred embodiment a folding draft support wire acts as a means by which the draft force on the outer wings is transferred to the centre hitch frame. The wire is pivotally attached to the outer wing and wing hitch frame. Supporting the wire is a folding support arm. The arm has an outer arm pivotally attached to an inner arm. The inner arm is attached to the wing hitch frame. Controlling the outer arm is a chain that is attached to the wing hitch frame by a chain arm. The chain is also attached to an elongated plate on the outer arm. This design allows the support arm to be folded when the cultivator is in the transportation mode.

The disclosure also describes connecting rods and draft cables as hereinafter set forth.
Brief Description of the Drawings The invention will now be described further, by way of example, with reference to the accompanying drawings, in which:

Figure 1 is an overhead schematic view of an agricultural cultivator, Figure 2 is a side, overhead view of the differential connecting rod in the field mode, Figure 3 is a side, overhead view of the differential connecting rod in the transport mode, Figure 4A is a side view of the cultivator in the headland mode, Figure 4B is a rear view of the cultivator in the field mode, Figure 4C is a rear view of the cultivator in the transportation mode, Figure 4D is a side, front view of the transport assembly, Figure 4E is a side, front view of the differential rod while the cultivator is in field operating mode, Figure 4F is a view of the folding support wire when the cultivator is in the transportation mode, Figure 5 is a front view of the differential connecting rod, showing both spring assemblies, and Figure 6 is a front view of the left side of the differential connecting rod showing a single spring assembly.

Detailed Description of the Preferred Embodiments Referring to the drawings, it is possible to observe the major elements and general operation of the present invention. The terms "left" and "right" are used as a matter of convenience and are determined by standing at the rear of the tillage device or cultivator and facing the forward end in the normal direction of travel when the tillage device or cultivator is operating in the field (field mode, see figure 4B). Likewise, forward and rearward are determined by normal direction of travel in the field mode of the tillage device or cultivator. Upward or downward orientations are relative to the ground or operating surface. Horizontal or vertical planes are also relative to ground.

Figure 1 illustrates a general overhead view of a pull-type tillage device or cultivator. A
conventional tillage device or cultivator consists of a centre section 2 with two inner wings 3 positioned next to the centre section 2. Next to the inner wings 3 are two outer wings 4. The tillage device or cultivator 1 has a triangular shaped centre frame hitch 9.
The base of this hitch 9 is attached to the centre section 2 and the front of the hitch 9 is attached to a tractor mount 8. The tractor mount 8 is attached to a conventional agricultural tractor. The tractor pulls the tillage device or cultivator 2 and also supplies hydraulic power or mechanical power via the power-take-off (PTO) to the various implements on the cultivator 2.

Supplementing the centre frame hitch 9 is the wing hitch frame 10 that provides draft support to the inner wings 3. Supporting the entire cultivator 2 are a series of castor wheels 5 located towards the front of the cultivator 2 and a series of packing or rear supporting wheels 7 located towards the rear of the cultivator 2.

The centre section 2 has a centre frame 22 and a toolbar 6 which supports various ground-working implements. Such implements are well known in the art and include ploughs, coulters, discs as well as other implements. Each inner wing 3 and outer wing 4 also possesses a tool bar 6. The inner wing 3 also has an inner wing frame 13. The centre frame 22 and inner wing frame 13 are connected by means of a universal joint assembly 21 that can best be seen in figures 2 and 3.

Figure 1 shows the cultivator 2 in the field mode. In the field mode, the inner and outer wings 3 and 4 are fully extended horizontally across the field. There is also a headland mode (see figure 4A) where the wings (2 and 3) are still extended, but the tool bars 6 are raised out of the soil. The headland mode is used at the end of a crop row when an operator wishes to turn the tractor and cultivator 2 around and partially raise the ground working implements. The transportation mode (see figure 4C) involves rotating the centre frame 22 and inner wing frame 13 upwards through 900 This raises the toolbars 6 and packing wheels 6 up into the air. The wings 3 and 4 are then rotated rearwards. This results in a cultivator that is narrow and may be transported to another field.

The draft support wire 50 can best be seen in figure 1 and extends from the wing hitch frame 10 to the outer wing 4. During field operations, this wire can transfer some of the draft force in the outer wing 4 to the centre hitch frame 9.

As seen in figures 2 and 3, the differential connecting rod 20 is located parallel to the centre frame 22. It controls the movement of the universal joint assembly 21.
There are two, identical connecting rods 20 which control respective universal joint assemblies 21 located on the left and right sides of the centre frame 22. For purposes of brevity, only the right side is illustrated and discussed. However, the left side works in an analogous fashion.

The universal joint assembly consists of a universal joint 25 with a centre frame attach 27 and a wing attach 26. Generally speaking, the centre frame 22 is connected to the centre frame attach 27 and the wing frame is connected to the wing attach 26. Figure 2 shows the centre frame 22 and universal joint assembly 21 oriented in the field mode. Figure 3 illustrates the centre frame 22 and universal joint assembly 21 rotated forward 90 into the transportation mode.

Connecting the universal joint assembly 21 to the centre frame 22 is bracket 23 with a slot 24. At the other end of the universal joint 25 there is a conventional spherical bearing 28 which allows for a full range of motion and permits the universal joint 25 to move in the slot 24. This allows the wing section a full range of motion about the universal joint.

In the prior art, the wing section could only rotate about an axis parallel to the direction of travel. By contrast, in the present invention, the wing section can rotate upwards or downwards on an axis perpendicular to the direction of travel and about a vertical axis.
However, to control the movement of the universal joint 25 within the slot 24, there is the differential connecting rod 20.

The universal joint assembly 21 has three axes of motion. The three-axes joint consists of a universal joint with one joint pin connected to a yoke on the centre frame 22 at bearing 28 at one end and constrained in the slot 24 at the other end, defining a first axis longitudinal to the pin and a second axis perpendicular to the pin through the bearing 28.
The pin 28 is allowed freedom to rotate about the second axis within the limits of the slot 24 of the bracket 23. The second axis is therefor generally transverse. A
third axis is defined by the joint pin connected to a yoke on the wing frame, which is perpendicular to the first axis and is a pivot for inner wings 3 to follow ground elevations when in transport.

The first axis in the transport position allows rear folding of the wing frames and in the field position is a pivot allowing wings to follow ground elevations as shown in figure 2.
The first axis allows rear folding of the wing frames. The second axis allows the drawbar to rotate relative to the centre section so that the attached gangs are on average, aligned with the pitch of the ground (rising or falling slope in the direction of travel). The range of the second axis rotation is limited by the ends of the slot 24.

In figure 2, the differential connecting rod 20 is attached towards the centre of the centre frame 22 by means of the spring assembly 40. The spring assembly 40 will be described in greater detail below. At the end of the centre frame 22, the connecting rod is pivotally attached to an 'L'-shaped linkage 30. The 'L'-shaped linkage is pivotally attached to the centre frame 22 at the linkage pivot 31. The end of the 'L'-shaped linkage 30 is attached to the universal joint assembly 21 at the pivot 29.

Turning to figures 5 and 6, it is possible to observe both spring assemblies 40. As previously indicated both spring assemblies 40 are identical in construction and operation.
Figure 6 illustrates a single spring assembly 40 viewed overhead. Each spring assembly 40 consists of a co-axial spring 41 held in a slightly compressed positioned by a pair of threaded tie rods 42. The differential connecting rod 20 is in two parts that, in field operation abut each other at the centre of the centre frame section. Each part of the connecting rod 20 is slidably supported by a inner stop block 46 which is attached to the frame 22. The differential connecting rod 20 is biased to a central position as shown by the spring assembly 40.

The spring assembly 40 is attached at one end to the inner stop block 46 by tie rods 42.
The spring is co-axial with the differential connecting rod 20. It is constrained between two abutment inner sliding blocks 44a and 44b. Inner sliding block 44a is constrained by nuts 45 at the end of tie rods 42. A pair of outer sliding blocks 43a are attached to the differential connecting rod 20 (secured by bolt shown) and are in abutment with an inner sliding block 44a. Another pair of outer sliding blocks 43b are welded to the differential tie rod 20 and are in abutment with inner sliding block 44b, passing through the inner stop block 46.

In operation, when a wing rotates about the second axis in direction 66a, driven to an average position between the attached gangs as the ground slope varies, then it drives the L-shape lever and then the connecting rod 20 in direction 66. The spring is compressed between the outer sliding blocks 43a and the inner stop block 46, between which are also pressed inner sliding block 44a and 44b. The motion is directed onto the other abutting connecting rod and causes the opposite wing to rotate about its second axis in an equal amount in the opposite direction. Therefor the centre section is suspended at an average height between the two adjacent wing sections.

When being driven from the other wing section, the connecting rod 20 is forced in the other direction 67. Outer sliding blocks 44b abut onto the inner sliding block 43b. The spring shown in figure 6 is then compressed between the outer sliding blocks 43b and nuts 45, between which again pressed the inner sliding blocks 44b and 44a are again pressed. The spring works in both directions to bias the half of the connecting rod assembly to a central position. The other half works the same way. The height of centre section is driven by the three axes joints attaching the wing frames on either side. The differential connecting rod assembly keeps it at an average position between the two wing frames and biases the wing frames into rotational alignment with the centre frame about the second axis. It also distributes weight transfer force that may be optionally applied to the centre frame onto each of the wing frames. It should be noted that there are several possible secondary embodiments involving the connecting rods.

When the cultivator 2 is in the transportation mode, as seen in figure 3, it is important the pivot 29 be fixed in the slot 24. Because the wing section's weight is supported partially by the universal assembly 21, it is important that the pivot 29 should not impact the slot 24. To achieve that goal, a transport assembly 47 has been included to prevent translation of the differential rod. The transport assembly 47 has a tongue 48 attached to the centre frame 22. A tongue spring 49 is biased between the differential connecting rods 20 as seen in figure 3. During the transition from the field mode (as seen in figure 2) to the transportation mode (as seen in figure 3), the wings are folded upwards 90 and the ends of the wings are folded rearwards. This places a force similar to 67a on the pivot 29.
These forces pull both differential connecting rods 20 away from the centre of the centre frame 22. The spring-biased tongue 49 is inserted between the rods when the centre frame 22 is rotated forward 90 . This locks the rods and holds the pivot 29 at one end of the slot 24 during transport (as seen in figure 4D). Conversely, the tongue 48 is removed from the between the rods when the centre frame 22 is rotated into the field position.

The folding draft support wire 50 can be seen in figures 1 and 4F. The wire 50 is attached to the cultivator 2 at three points. The wire 50 is pivotally attached to the inner hitch 52.
At the opposite end, the wire 50 is pivotally attached to the outer wing hitch 51 (see figure 4F). Supporting the wire 50 in the middle is the folding support arm 53. The folding draft support wire 50 is designed to transfer the draft force created by the outer wings to the centre hitch frame. Failure to transfer the draft force could result in the outer wings twisting behind the centre section. As seen in figure 4F, the support wire 50 is lifted towards the centre frame and wing sections during the transportation mode. The folding support arm 53 accomplishes this. The folding support arm 53 consists of an inner arm 54 attached to the wing hitch frame 10. A hinge 56 pivotally attaches the outer arm 55. To ensure that the support arm 53 remains fully extended during the field mode, the outer arm 55 has an elongated plate 55a. Attached to the elongated plate 53a is a chain 57.
The chain is connected to the wing hitch frame 10 by a pivotally mounted chain arm 58.
The support wire 50 is attached to the top of the outer arm 55.

During the field mode, the wing hitch frame 10 is rotated 90 downwards. The chain arm 58 pulls the elongated plate 55a and outer arm 55 away and downwards. This extends the draft wire 50. Conversely, when converting the cultivator from the field mode to the transport mode, the wing hitch frame 10 rotates upwards 90 . This allows the outer arm to pivot about the hinge 56. The wire is moved towards the hitch frame as seen in figure 4F.
It is the tension in the wire as the wing frames are folded rearwardly that causes the wire to be pulled in close to the frame in the transport position. The outer arm 55 guides the position of the wire up and over the wheel 5 so that it does not rub on the wheel or the ground in transport.

Claims (7)

Claims

1. An agricultural cultivator comprising:
a. a hitch frame and a drawbar frame including a drawbar center frame and a drawbar wing frame;
b. said drawbar center frame pivotally attached to the hitch frame on a transverse axis for rotation between a downward working position and an upward transport position;
and c. said drawbar wing frame being attached to a side of the drawbar center frame by a multi-joint assembly whereby:
i. the multi-joint assembly is attached to the drawbar center frame defining a first axis perpendicular to the drawbar center frame;
ii. the multi-joint assembly is attached to the drawbar wing frame defining a second axis perpendicular to the first axis and perpendicular to the drawbar wing frame;
and iii. the multi-joint assembly includes a third axis generally longitudinal to the drawbar wing frame.

2. The cultivator as in claim 1, in which the multi-joint assembly is pivotally attached to the drawbar center frame at a first end, and at a second end constrained within a slotted end of the drawbar center frame, so that the third axis is at the first end and movement of the multi-joint assembly is about the third axis is limited by the second end which is constrained within the slotted end, thereby allowing relative rotation between the drawbar center frame and drawbar wing frame about the third axis.

3. The cultivator as in claim 1, in which the multi-joint assembly is attached to the drawbar center frame at one end pivotally, and at a second end to a first end of a differential lever, and the lever being pivotally attached to the drawbar center frame for pivotal movement, allowing movement of the multi-joint assembly about the third axis thereby allowing relative rotation between the drawbar center frame and drawbar wing frame about the third axis.

4. The cultivator as in claim 3 in which the pivotal movement of the differential lever is limited.

5. The cultivator as in claim 4 in which the pivotal movement of the differential lever is biased.

6. The cultivator as in claim 3 in which a second end of the differential lever is connected to one end of a differential control rod, and the other end of the differential control rod is connected to a similar differential lever at an opposite end of the drawbar center frame for controlling relative rotation of the drawbar wing frame about the third axis differentially with a second drawbar wing frame.

7. The cultivator as in claim 6 in which the differential control rod is split in two parts which are guided on the drawbar center frame so that inner ends of the two parts abut each other, the implement further comprising:
a. limits to limit the range of pivotal movement of the differential levers;
and b. a transport assembly which can be placed between the inner ends thereby maintaining the position of the differential levers at their respective limit.