• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    A star sensor arrangement for weeding a field, which comprises a star sensor arrangement - a tool frame comprising a plurality of star cleaners along the tool frame, two foldable wing sections divided by a center boom, each wing section comprising an inner wing connected to an outer wing with a distal blade end, - the tool frame has an operating position where the center boom, inner wings and outer wings define a straight line of work, and a folded position where the wing sections are folded, - each inner wing rotatably engages the center boom and each inner wing rotates in an inner plane between an inner operating position where the inner wing extends along the line of work, and an inner folded position where the inner wing extends upward and substantially perpendicular to the straight line - each outer wing rotatably engages the corresponding inner wing and each outer wing rotates in a outer plane tilted in relation to it corresponding inner plane, between an outer operating position where the outer wing extends along the work line, and an outer folded position, with the distal wing end substantially facing the center boom, and the outer wing parallel to the corresponding inner wing and positioned upward in the outer plane .
    公开号:DK201900096U1
    申请号:DK201900096U
    申请日:2019-11-28
    公开日:2020-01-15
    发明作者:Lindholm Gubi Jacob；Holm Jan；Jensen Bent
    申请人:GAMMELSKOV SERVICE TEKNIK ApS；Farmer Power Pack ApS；
    IPC主号:
    专利说明:

    Star cleaning arrangement and use of a star cleaning arrangement for weeding
    FIELD OF THE INVENTION
    The present invention relates to a star sensor arrangement and the use of a star sensor arrangement for weeding.
    BACKGROUND OF THE INVENTION
    Star cleaners are well known in the art. Star cleaners are versatile and come in many sizes and with a wide range of features depending on the intended use.
    One use of the star cleaner is to remove weeds that come into the field. For this purpose, farmers prefer long-wing star cleaners that can extend over much of the field, thus reducing the time spent on field work.
    The problem with today's star cleaners is that the long wingspan of the star cleaner complicates storage and transport of the machine from one location to another.
    Thus, solutions are needed that can reduce the time needed for weeding and seeding a field.
    The object of the invention
    It is an object of the invention to overcome the limitations of the prior art by providing a stellar sensor arrangement capable of reducing the time to be spent on weeding.
    Description of the Invention
    An object of the invention is achieved by a star cleaning arrangement for weeding a field. The star cleaning arrangement may include a tool frame.
    The tool frame may comprise a plurality of star cleaners along the tool frame.
    The tool frame may further comprise a stationary center boom dividing the tool frame into two foldable blade sections, each blade section may comprise an inner wing connected to an outer wing with a distal wing end.
    DK 2019 00096 U1
    The tool frame may have an operating position where the center boom, inner wings and outer wings define a straight line of work, and a collapsed position where the wing sections are folded.
    The person skilled in the art will understand the width of the stellar arrangement as the maximum extent of the stellar arrangement along the proper line of work.
    The star cleaner arrangement will be able to hatch a field when in the operating position as the width of the star cleaner arrangement is maximized in the operating position.
    The star cleaner arrangement can be transported to and from a field when in the collapsed position because the width of the star cleaner arrangement is minimized in the operating position.
    Each inner wing can rotatably engage the center boom. Each inner wing rotates in an inner plane between an inner operating position and an inner folded position. Each inner wing can extend along the proper working line when positioned in the operating position. Each inner wing may extend upward and substantially perpendicular to the proper working line when in the inner folded position.
    Those skilled in the art will recognize that the outer wing associated with the inner wing will rotate parallel to the inner plane as one of the inner wings rotates between the inner operating position and the inner folded position.
    Each wing section may be 6 m long and the star sensor arrangement will be too high to be transportable if each outer wing simply rotated with the corresponding inner wing.
    Each outer wing can rotatably engage the corresponding inner wing. Each outer wing can rotate in an outer plane, which outer plane can be inclined with respect to the corresponding inner plane between an outer operating position and an outer folded position.
    Each outer wing may extend along the work line when positioned in the outer operating position. The distal wing end of each outer wing faces substantially towards the center boom 201 and the outer wing is parallel to the corresponding inner wing, and upwards in the outer plane when the outer wing is positioned in the outer folded position.
    If each wing section of a star sensor arrangement has an inner wing in an inner operating position and an outer wing positioned in an outer folded position, and both inner wings are rotated from the inner operating position to the inner folded position, the overall height of the star sensor arrangement will be substantially lower. than if the outer wings were not rotatable.
    This allows the star detector arrangement to have longer wing sections while still being transportable, increasing the area weighed per unit area. passage, thus increasing efficiency.
    Each outer wing is rotatable in the outer plane, which outer plane is inclined with respect to the corresponding inner plane, causing a displacement between the inner and outer wings of a wing section when the outer wing is in the outer folded form, thus reducing the width of the stellar array.
    The transport of star sensor arrangement is facilitated with decreasing width.
    In one aspect of the invention, the center beam has a center beam width adapted to form an equipment space between the wing sections.
    An increase in the center boom width will cause the stellar array arrangement width in the collapsed position, which will make transporting the stellar array arrangement more difficult, but this will allow the stellar array arrangement to carry optional equipment.
    This enhancement space makes the star sensor arrangement more versatile as it can solve two tasks at once.
    Those skilled in the art will recognize that the equipment space is possible due to the blade sections, with each outer wing rotatable in the outer plane, causing a reduction in the width of the star sensor arrangement in the collapsed position. The reduction allows that the center boom
    GB 2019 00096 U1 width can be increased, thus creating the equipment space between the wing sections and the stars.
    In one aspect of the invention, the star sensor arrangement comprises a drill positioned in the equipment room.
    Normally it will be very time-consuming and expensive to sow after weeding, as the farmer has to drive all the passes once more. However, the drill positioned in the equipment room enables the farmer to hatch and then simultaneously. This reduces costs and time consumption.
    The above situation is especially advantageous in winter weeding. If the farmer at the same time sow grass or similar, the farmer will reduce the amount of weeds in the field. Furthermore, the grass is excellent for holding (i.e., storing) nitrates, which is favorable for the crop to be sown in the spring.
    The inner wing can rotatably engage the center boom using a 90-degree folding joint.
    Opposite to the center boom, the inner wing can rotatably engage the outer wing by means of a 180-degree folding joint.
    In one aspect of the invention, each outer plane forms a 38-48 degree angle with the corresponding inner plane.
    The angle between the outer plane and the corresponding inner plane allows a reduction in the width of the stellar arrangement when in a collapsed position, and / or an increase in the width of the center boom.
    In one aspect of the invention, each outer plane forms a 41-45 degree angle with the corresponding inner plane.
    DK 2019 00096 U1
    The angle between the outer plane and the corresponding inner plane allows a reduction in the width of the stellar arrangement when in a collapsed position, and / or an increase in the width of the center boom.
    In one aspect of the invention, each outer plane forms a 43 degree angle with the corresponding inner plane.
    The angle between the outer plane and the corresponding inner plane allows a reduction in the width of the stellar arrangement when in a collapsed position, and / or an increase in the width of the center boom.
    An object of the invention is achieved by connecting a vehicle to a star sensor arrangement.
    An object of the invention is achieved by using a star sensor arrangement for weeding a field.
    An object of the invention is achieved by the use of a star sensor arrangement comprising a seed drill for weeding and sowing a field simultaneously.
    An object of the invention is achieved by using a vehicle for weeding a field.
    Although well described above, one skilled in the art may understand a corresponding description, which description may be an equivalent description. In such aspects, the following description may serve to support the description or serve as an example. Structural features mentioned below can be found to be supported in the figures as needed. One skilled in the art will be able to easily identify technical features of the figures.
    One aspect of the object can be achieved with a star sensor arrangement comprising a blade arrangement comprising at least two blade sections, each blade section configured to support several star sensor arms each with a rotor element. The vane arrangement may be configured with a vane pin between two vane sections disposed so that the vane portions can rotate relative to one another in a plane of section around a vane vane angle and collapse the vane portions. The section plane can be seen in the figures as an outer plane. Wing turning pin 201 20100096 U1 pen may be implemented as seen in the attached figures. The pivot pin can be as described in Figure 6. The pivot pin can be operated as shown in Figure 7.
    One skilled in the art will experiment with surfaces and angles to improve the folding of blade sections, which includes the possibility of squeezing rotating stars, either without overlap or with partial overlap, and to optimize the weight distribution and design moments. The swivel pin may be a collapsible joint that folds two sections at an angle of e.g. 180 degrees.
    The star cleaning arrangement may further comprise a support wing pivot in one of the two blade sections and configured to rotate one wing portion relative to a support in a support plane at a support angle. The support wing pivot pin can bend the blade arrangement relative to the support. The support plane can be seen in the figures as an inner plane. The support wing pivot pin may be a flexible connection which bends the wing arrangement into e.g. 90 degrees.
    The rotor arrangement may be configured where the support wing pivot pin and the sectional dowel pin are disposed at an angle to each other such that the section plane and the support plane intersect at an angle of cut. The angle between the planes can be 35-55 degrees, 40-50 degrees or e.g. ca. 43-47 degrees. An exit angle can be 43 degrees.
    The star cleaning arrangement may further comprise a support configured with connecting means for connecting to a vehicle. The star cleaning arrangement may be arranged in which the support supports the support pivot pin attached to one end of an inner wing section and configured for an operating position relative to the vehicle at an operating support angle and to a transport position relative to the vehicle at a transport support angle.
    The vehicle is not part of the star sensor arrangement, however, configured to operate in conjunction with a vehicle such as a tractor.
    In one aspect, the support and at least two wing sections are disposed with the wing pivot at the opposite end of the inner wing section, and wherein the wing pivot is configured for an operating position 2019 00096 U1 position relative to the vehicle at an operating section angle and to a transport position relative to the vehicle section at a transport angle. .
    In one aspect, the support wing pivot and wing pivot pin are arranged such that the operating support angle and the operating section angle in the operating position align with the wing portions and extend from the support in a substantially linear manner and with an operating extent of the support. The operating range can be 9 m or more, 10 m or more or 12 m or more.
    In one aspect, the support wing pivot and wing pivot pin are arranged such that the operating support angle and the operating section angle in the transport position collapse the wing portions with a height and a width from the support.
    In one aspect, the support has a center section and supports in one direction a first blade arrangement configured to extend in a first direction when in the operating position, and a second wing arrangement configured to extend in a second direction. and opposite direction of the first direction when in the operating position. The star cleaning arrangement is configured such that the center section has a void when the first wing arrangement and the second wing arrangement are in the transport position.
    The shape of the void is complementary to the shape of a wound arrangement so that the wound arrangement can fit into the void.
    In one aspect, the support further supports a center section configured to support multiple star detector arms each with a rotor element that aligns with the wing sections when in the operating position.
    The star cleaning arrangement, where the support is configured with a platform, the platform is designed to support a wound arrangement.
    An object is achieved by an agricultural arrangement comprising a star sensor arrangement and a sowing arrangement. In such an agricultural arrangement, the star sensor arrangement may be as described or according to the figures. In such an agricultural arrangement, the wound arrangement may be any standard wound arrangement or according to the figures.
    DK 2019 00096 U1
    An object can be achieved by the use of a vehicle comprising a star cleaning arrangement and a wound arrangement.
    In a particular application, the vehicle comprises a star cleaning arrangement as described or according to the figures. Such use may involve placing a wound arrangement in front of the vehicle. In one aspect, the wound arrangement is arranged in conjunction with the star cleaning arrangement. In a particular aspect, the wound arrangement is located in a void in the star cleaning arrangement in a transport position, i.e. when the sections of the star cleaning arrangement are bent or folded.
    An object can be achieved by using a vehicle comprising a star cleaning arrangement in a transport position, the star cleaning arrangement surrounding a sow arrangement in a transport position, the use in the transport position in a transport direction having a width of less than 4 meters, less than 3.2 m or less 3 meters and a height of less than 4 meters or less than 3 meters.
    An object can be achieved by using a vehicle comprising a star cleaning arrangement in an operating position, where, using the vehicle in an operating direction with the star cleaning arrangement in the operating position, the star cleaning arrangement extends more than 10 meters or approx. 12 meters or more.
    Description of the drawing
    Embodiments of the invention will be described in the figures wherein:
    FIG. 1 illustrates a vehicle having a star cleaning arrangement and a drill;
    FIG. 2 illustrates a star cleaning arrangement in an operating position and a folded position;
    FIG. 3 illustrates a star cleaning arrangement in a collapsed position;
    FIG. 4 illustrates a top view of a star cleaning arrangement in a collapsed position;
    FIG. 5 illustrates a wing section;
    FIG. 6 illustrates a link between an inner wing and an outer wing; and
    FIG. 7 illustrates an unfolding of an outer wing.
    DK 2019 00096 U1
    Detailed description of the invention
    Element No. Manage Nero Cleaner Arrangement 10 Equipment Frame 20 operating Position 22 Folded position 24 Midterbom 25 stars Sere 30 Wing Section 40I, 40II 90-degree folding joint 41I, 41II Inner Wing 42I, 42II 180-degree folding joint 43I, 43II Outer Wing 44I, 44II Distal wing end 45I, 45II straight line of work 50 Drills 80 equipment rooms 90 Vehicle 100
    FIG. 1 illustrates a vehicle 100 with a star sensor arrangement 10 and a drill 90.
    The star cleaning arrangement 10 is positioned in an operating position 22 and will be ready to hatch and then if the vehicle 100 was in a field.
    The star cleaner arrangement 10 comprises a tool frame 20 with a center boom 25 and a first and second wing sections 40I, 40II extending along a straight line of work 50 when the star cleaner arrangement 10 is positioned in an operating position 22. The middle boom 25 is connected on both sides thereof. first and second wing sections 40I, 40II.
    Each wing section 40I, 40II includes an inner wing 42I, 42II that rotatably engages the center boom 25 by a 90-degree folding joint 411, 41II.
    DK 2019 00096 U1
    Opposite the center boom 25, the inner wing 42I, 42II is rotatably engaged with an outer wing 44I, 44II by a 180-degree folding link 43I, 43II.
    Each outer wing 44I, 44II has a distal wing end 45I, 45II which, when the star sensor arrangement 10 is positioned in an operating position 22, defines a maximum width of the star sensor arrangement 10.
    The drill 90 is positioned in the equipment room 90.
    FIG. 2 illustrates a star sensor arrangement 10 in an operating position 22 and a collapsed position 24.
    Those skilled in the art will know that the star sensor arrangement 10 cannot be in both the operating position 22 and the collapsed position 24 simultaneously, but FIG. 2 illustrates the differences between the two positions, such as a maximum and a minimum width for the star sensor arrangement
    10th
    The star cleaner arrangement 10 comprises a tool frame 20 with a center boom 25 and a first and second wing sections 40I, 40II extending along a straight line of work 50 when the star cleaner arrangement 10 is positioned in an operating position 22. The center boom 25 is connected on both sides to the first and the second wing section 40I, 40II.
    Each blade section 40I, 40II includes an inner wing 42I, 42II that rotatably engages the center boom 25 by a 90-degree folding link 41I, 41II.
    Opposite the center boom 25, the inner wing 42I, 42II is rotatably engaged with an outer wing 44I, 44II by a 180-degree folding link 43I, 43II.
    Each outer wing 44I, 44II has a distal wing end 45I, 45II which, when the star sensor arrangement 10 is positioned in an operating position 22, defines a maximum width of the star sensor arrangement 10.
    The star cleaning arrangement 10 is special in that it has an equipment room 90 in the collapsed position 24 and in the operating position 22.
    DK 2019 00096 U1
    This allows the star sensor arrangement 10 to have more functions than weeding.
    Furthermore, the enhancement can be carried with the star sensor arrangement 10 as a single unit, since the equipment space 90 is also available in the collapsed position.
    FIG. 3 illustrates a star sensor arrangement 10 in a collapsed position 24.
    The star cleaning arrangement 10 is shown with only a few star cleaners 30, but the tool frame 25 would have star cleaners 30 along its entire width for the intended use.
    The star cleaner arrangement 10 comprises a tool frame 20 with a center boom 25 and a first and second wing sections 40I, 40II extending along a straight line of work 50 when the star cleaner arrangement 10 is positioned in an operating position 22. The center boom 25 is connected on both sides to the first and the second wing section 40I, 40II.
    Each wing section 40I, 40II includes an inner wing 42I, 42II that rotatably engages the center boom 25 by a 90-degree folding joint 411, 41II.
    Opposite the center boom 25, the inner wing 42I, 42II is rotatably engaged with an outer wing 44I, 44II by a 180-degree folding link 43I, 43II.
    Each outer wing 44I, 44II has a distal wing end 45I, 45II which, when the star sensor arrangement 10 is positioned in an operating position 22, defines a maximum width of the star sensor arrangement 10.
    FIG. 4 illustrates a top view of a star sensor arrangement 10 in a collapsed position 24. FIG. 4 describes how star sensors 30 are positioned relative to each other and that there is equipment space 90.
    FIG. 5 illustrates a wing section 40.
    The wing section 40 comprises an inner wing 42 which rotatably engages the center boom 25 by means of a 90-degree folding joint 41.
    DK 2019 00096 U1
    Opposite to the center boom 25, the inner wing 42 is rotatably engaged with an outer wing 44 by means of a 180-degree folding joint 43.
    The outer wing 44 has a distal wing end 45 which, when the star sensor arrangement 10 is positioned in an operating position 22, defines a maximum width of the star sensor arrangement
    10th
    FIG. 6 illustrates a link between an inner wing 42 and an outer wing 43.
    The joint is a 180-degree folding joint 43.
    FIG. 6A and 6B show two different perspectives.
    FIG. 7 illustrates the unfolding of an outer wing 44.
    权利要求:
    Claims (9)
    [1]
    A star cleaning arrangement (10) for weeding a field, comprising a star cleaning arrangement (10)
    - a tool frame (20) comprising a plurality of star cleaners (30) along the tool frame (20), two foldable wing sections (40I, 40II) divided by a center boom (25), each wing section (40I, 40II) comprising a inner wing (42I, 42II) connected to an outer wing (44I, 44II) with a distal wing end (45I, 45II),
    - the tool frame (20) has an operating position (22) where the center boom (25), the inner wings (42) and the outer wings (44) define a straight working line (50) and a folded position (24) where the blade sections (40I, 40II) is collapsed,
    - each inner wing (42I, 42II) rotates in engagement with the center boom (25), each inner wing (42I, 42II) rotates in an inner plane between an inner operating position, with the inner wing (42I, 42II) extending along the proper working line (50 ), and an inner folded position where the inner wing (42I, 42II) extends upward and substantially perpendicular to the proper working line (50),
    - each outer wing (44I, 44II) rotates in engagement with the corresponding inner wing (42I, 42II), each outer wing (44I, 44II) rotates in an outer plane (48I, 48II) inclined to the corresponding inner plane , between an outer operating position where the outer wing (44I, 44II) extends along the straight working line (50), and an outer folded position, with the distal wing end (45I, 45II) substantially facing the center boom (25), and the outer wing (44I, 44II) are parallel to the corresponding inner wing (44I, 44II) and positioned upward in the outer plane.
    [2]
    Star cleaning arrangement (10) according to claim 1, which is new in that the center boom (25) has a center beam width adapted to form an equipment space (90) between the wing sections (40I, 40II).
    [3]
    Star cleaning arrangement (10) according to claim 2, which is new in that the star cleaning arrangement (10) comprises a seed drill (80) positioned in the equipment room (90).
    [4]
    The star cleaning arrangement (10) according to one or more of claims 1-3, which is new in that each outer plane forms an angle of 38-48 degrees, approx. 41-45 degrees or 43 degrees with the corresponding inner plane.
    DK 2019 00096 U1
    [5]
    Vehicle (100) associated with a star sensor arrangement (10) according to one or more of claims 1-4.
    5
    [6]
    Use of a star sensor arrangement (10) according to one or more of claims 1-4 for weeding a field.
    [7]
    Use of a star sensor arrangement (10) according to claim 3 or 4 for weeding and seeding a field simultaneously.
    [8]
    Use of a vehicle (100) according to claim 6 for weeding a field.
    [9]
    Use of a vehicle (100) according to claim 6 and a star sensor arrangement (10) according to claim 3 for simultaneously weeding and seeding a field.
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    同族专利:
    公开号 | 公开日
    DK201900096Y3|2020-03-11|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    法律状态:
    2020-01-15| UAT| Utility model published|Effective date: 20200111 |
    2020-03-11| UME| Utility model registered|Effective date: 20200311 |
    2021-02-10| UYA| Request for examination filed (utility model)|Effective date: 20210210 |
    优先权:
    申请号 | 申请日 | 专利标题
    DKBA201900096U|DK201900096Y3|2019-11-28|2019-11-28|Star cleaning arrangement and use of a star cleaning arrangement for weeding|DKBA201900096U| DK201900096Y3|2019-11-28|2019-11-28|Star cleaning arrangement and use of a star cleaning arrangement for weeding|
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