JP2011087494A - Operation unit structure of combine harvester - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide an operation unit structure of a combine harvester, which allows a crew to easily get on and off, and can prevent contact of a step for getting on and off with grain straws, levee or the like. <P>SOLUTION: The operation unit structure of a combine harvester includes an upper side climbing step 21 and a lower side climbing step 22 capable of being changed into a using attitude or a stored attitude. The lateral outside end part of the upper side climbing step 21 is placed on the inner side of a machine frame than a dustproof cover 10, and the lateral outer side end part of the lower side climbing step 22 is placed on the inner side of the machine frame than the dustproof cover 10 in the stored attitude, and is placed on the outer side of the machine frame than the dustproof cover 10 in the using attitude. <P>COPYRIGHT: (C)2011,JPO&INPIT

Description

  The present invention is provided in a cutting part disposed in the front part of the fuselage, a driving part disposed in the right or left side of the front part of the fuselage, and a lateral part of the fuselage behind the floor of the driving part. And a dust cover that introduces air into the radiator.

  In order for an occupant to get on and off the driving unit, conventionally, a step for getting on and off is sometimes provided on the lateral side of the body below the floor of the driving unit (see, for example, Patent Document 1).

  When the combine is large, the driving unit is at a high position, so two steps for getting on and off may be provided in the vertical direction. At this time, if the amount of protrusion of the two steps for getting on and off from the side of the machine body is increased, it becomes easier for the occupant to put his / her feet on the step for getting on and off, and the occupant can easily get on and off the driving unit.

Japanese Patent No. 3615945 (see FIGS. 2 and 3)

  However, if the amount of protrusion of the two steps for getting on and off is increased, the laterally outer end of the step for getting on and off may protrude to the outside of the fuselage rather than the dust cover. At this time, the step for getting on and off may come into contact with the culm during the cutting operation, and the culm may be entangled with the step for getting on and off. In addition, the boarding / exiting step may come into contact with the kite during the cutting operation at the shore, or the boarding / exiting step may be damaged by coming into contact with a power pole or a sign during traveling or transportation.

  An object of the present invention is to provide a driving unit structure of a combine that can prevent a passenger from getting in and out of the driving unit while the passenger can easily get on and off the driving unit.

The operation part structure of the combine according to the present invention includes a cutting part disposed at a front part of a fuselage, a drive part disposed at a right side or a left part of a front part of the fuselage, and a fuselage behind a floor of the drive part. Provided with a dustproof cover provided on the side portion for introducing air into the radiator,
The first characteristic configuration is provided in an upper boarding / alighting step fixed to a lower side of the airframe below the floor of the operating section, and provided on a side of the airframe below the upper boarding / alighting step. A lower step for getting on and off which can be changed to a use posture protruding from the side to the outside of the fuselage and a retracted posture folded to the side of the side of the fuselage. And the lower step for getting on and off is such that the laterally outer end is located on the inner side of the dust-proof cover in the retracted position, and the use posture is positioned on the lower side. In this case, the end portion on the lateral outer side is configured to be located on the outer side of the machine body with respect to the dust cover.

  When the passenger gets on and off, the lower step for getting on and off is changed to the use posture. At this time, the laterally outer end of the lower entry / exit step is located on the outer side of the fuselage, and the lateral outer end of the upper entry / exit step is located on the inner side of the fuselage cover. The protruding amount of the side getting-on / off step becomes larger than the protruding amount of the upper getting-on / off step, and it becomes easy for the occupant to put his / her feet on the lower getting-on / off step. Also, since the laterally outer end of the upper boarding step is located on the inner side of the aircraft (driving unit side) than the laterally outer end of the lower boarding step, the upper boarding step is on the upper side from the lower boarding step. It is easy to get on and off the step of getting on and off, and to get on the floor of the driving unit, and to get off from the floor of the driving unit to the upper and lower steps for getting on and off.

  When cutting or carrying out or transporting a combine, the lower boarding step is changed to the retracted posture. At this time, since the laterally outer ends of the lower and upper boarding steps are located on the inner side of the fuselage than the dust cover, the upper and lower boarding steps come into contact with the cereal and the cereal is used for getting on and off. It is possible to prevent the step for getting on and off from getting entangled with the step, or the steps for getting on and off at the upper and lower sides coming into contact with the eaves and the like.

  The second characteristic configuration of the present invention is that the lower boarding / alighting step is configured to enter the lower side of the upper boarding / alighting step in the retracted posture.

  According to this configuration, in the retracted posture, the lower boarding step gets under the upper boarding step. For this reason, it is possible to fold the lower boarding step in a compact manner by effectively using the space below the upper boarding step. Therefore, in addition to being able to reduce the size of the entire combine, it is possible to further prevent the lower step for getting on and off from coming into contact with the cereals and straws.

  According to a third characteristic configuration of the present invention, a space having an opening into which at least a toe side of an occupant's foot can be inserted is formed on an inner side of the body adjacent to the upper surface of the upper boarding step. It is in a certain point.

  According to this configuration, when the occupant puts his / her foot on the upper boarding / alighting step, the toe of the foot enters a space formed on the lateral side of the body adjacent to the upper surface of the upper boarding / alighting step. For this reason, even if the protrusion amount of the upper boarding / alighting step is smaller than the protrusion amount of the lower boarding / alighting step, it is easy for the occupant to put his / her feet on the upper boarding / alighting step.

  A fourth characteristic configuration of the present invention is that a battery is accommodated below the space.

  According to this configuration, the battery is accommodated below the space. For this reason, the battery can be arranged without difficulty by effectively using the lower part of the space.

  According to a fifth characteristic configuration of the present invention, in the plan view, the floor and the divider are arranged so that a straight line extending forward from the laterally outer end of the floor overlaps the divider on the operating unit side in the cutting unit. There is a point.

  According to this structure, even if it becomes difficult to visually recognize the divider on the driving unit side, the driver can visually recognize the end portion on the laterally outer side of the floor, so that the driving unit side on the extension line of the laterally outer end portion of the floor The position of the divider can be grasped.

  According to a sixth characteristic configuration of the present invention, the dustproof cover is located on the outer side of the airframe from the laterally outer end of the floor.

  According to this configuration, the dustproof cover is located on the outer side of the machine body from the laterally outer end of the floor. Therefore, the upper boarding step and the lower boarding step are folded more than the dustproof cover. A configuration that does not protrude outward can be easily obtained.

It is a side view which shows a combine. It is a top view which shows a combine. Front view showing an upper boarding step and a lower boarding step The top view which shows the step for the upper boarding / alighting and the step for the lower boarding Front view showing each state of the lower boarding steps A perspective view showing an upper boarding step and a lower boarding step

Hereinafter, the combine which concerns on this invention is demonstrated.
〔overall structure〕
As shown in FIGS. 1 and 2, this self-removing combine is provided with a harvesting unit C that harvests cereals at the front of an aircraft frame B (an example of an aircraft) equipped with a pair of left and right crawler type traveling devices A, Equipped with a driving unit D operated by an operator, at the rear of the machine frame B, a threshing device E for threshing the harvested cereal, a Glen tank F for storing the threshed grain, and an exhaust for discharging the stored grain Equipped with an auger G.

(Mowing part)
As shown in FIG. 1 and FIG. 2, the cutting part C includes a divider 1 for weeding cereals, a trigger device 2 for causing cereals to stand upright, and a clipper type for cutting the stock side of the induced cereals. The cutting device 3 and the vertical conveying device (not shown) that conveys the harvested cereal while rearwardly changing its posture to a laterally falling posture are provided.

(Operation part)
As shown in FIGS. 1 and 2, the operating unit D is disposed on the right side of the front part of the body frame B, and includes a floor 5, a seat support 6 located behind the floor 5, and a seat support thereof. A driver's seat 7 installed on the base 6 is provided.

  In a plan view, the floor 5 and the divider 1 are arranged so that a straight line L1 extending forward from the right end portion 5a of the floor 5 overlaps the divider 1 on the right side (operating unit D side) in the cutting unit C. Thereby, it becomes easy to grasp the position of the right divider 1 on the extension line of the right end portion 5 a of the floor 5. A front control tower and a side control tower are erected from the front part of the floor 5 and the inner side of the fuselage.

(Seat support)
As shown in FIGS. 1 to 3, the seat support 6 is disposed on the upper side of the body frame B, and includes a ceiling part 6 a, a front side wall part 6 b, a rear side wall part 6 c, a right side wall part 6 d (on the floor 5). An example of the lower machine body lateral side 12 is provided. A driver's seat 7 is installed on the ceiling portion 6 a of the seat support 6. An engine 8 and a radiator 9 are housed inside the seat support base 6. A dust cover 10 for introducing air into the radiator 9 is attached to the right side wall 6 d of the seat support 6. The seat support base 6 is configured to be rotatable around the axis X1. As a result, the seat support base 6 can be rotated to the outside of the machine body, and maintenance of the engine 8 and the radiator 9 can be easily performed. The height of the step surface of the floor 5 is set to be higher than the intermediate height between the upper and lower sides of the engine 8, and the driver's seat 7 is disposed at a high position so as to ensure the forward visibility.

  The dust cover 10 includes a rectangular upper surface portion 10a, a rectangular inclined surface portion 10b, a trapezoidal front side wall portion 10c, a trapezoidal rear side wall portion 10d, and a rectangular right side wall portion 10e. On the right side wall portion 10e of the dustproof cover 10, a ventilation window 10f with a dustproof net is provided. The right side wall portion 10e of the dust cover 10 protrudes outward from the airframe by a predetermined distance from the right end portion 5a of the floor 5 and the right side wall portion 6d of the seat support base 6. The height of the step surface of the floor 5 is located at the height of the upper and lower intermediate portions of the dust cover 10.

(Floor support)
As shown in FIGS. 1 to 4, a floor support base 11 is disposed on the upper side of the body frame B and on the front side of the seat support base 6. The floor support 11 includes a rectangular upper surface part 11a (an example of the floor 5), a rectangular front side wall part 11c, a left side wall part 11e, and a right side wall part 11f (an example of the machine body lateral side part 12 below the floor 5). It has.

  A mounting member 13 is installed between the front and rear body frames B inside the floor support 11. The mounting member 13 includes a rectangular plate-shaped mounting portion 13 a on which the battery 14 is mounted, and a bent portion 13 b that protrudes upward on both lateral sides of the mounting portion 13 a and restricts the lateral movement of the battery 14. Yes.

  A holding mechanism 15 that holds the battery 14 from above and restricts the vertical movement of the battery 14 is attached. The holding mechanism 15 includes a long pressing member 16 that presses the upper surface of the battery 14, and a threaded rod-like member 17 provided across the pressing member 16 and the machine frame B.

  A substantially rectangular opening 18 into which a passenger can insert his / her foot is formed on the upper side of the right side wall portion 11f of the floor support base 11. A rib 19 on which an occupant's foot can be placed is fixed to the lower side portion 18b of the opening 18 so as to protrude to the inside of the body. The upper surface of the rib 19 is configured to be slightly higher than the upper surface of the battery 14. That is, the battery 14 is located below the opening 18.

  A space 20 is formed between the upper surface portion 11a of the floor support 11 and the rib 19 and the battery 14 toward the inside of the machine body. Next to the left and right central sides of the battery 14 is a cylinder (not shown) for raising and lowering the cutting part C and for controlling the combine posture by moving the front swing link 42 and the rear swing link 43 up and down. On the other hand, a valve unit VU for supplying and discharging hydraulic oil is installed. Thereby, if the upper surface part 11a of the floor support base 11 is removed, the battery 14 and the valve unit VU can be easily maintained.

(Step for getting on and off)
As shown in FIGS. 3 to 6, an upper boarding step 21 and a lower boarding step 22 are vertically arranged on the lateral side portion 12 below the floor 5 and in front of the dust cover 10. Is provided.

  The upper boarding / alighting step 21 is fixed to the airframe lateral portion 12. The upper boarding / alighting step 21 includes a belt-like flat surface portion 21a (an example of a laterally outer end portion) and two belt-shaped bent portions 21b extending from both ends of the flat surface portion 21a in a direction intersecting the flat surface portion 21a. ing. At this time, the planar portion 21 a of the upper boarding step 21 in the plan view is located on the inner side of the right side wall portion 10 e of the dust cover 10. The upper surfaces of the flat surface portions 21 a and the bent portions 21 b are configured to have substantially the same height as the upper surfaces of the ribs 19. Thus, when the occupant places the heel side of the foot on the upper boarding step 21 and the rib 19, the toe side of the occupant's foot enters the interior of the space 20 through the opening 18.

  The lower getting-on / off step 22 is attached to the airframe lateral portion 12 so as to be rotatable around the axis X2. The lower step 22 for getting on and off includes a placement portion 23 on which the occupant's feet are placed, two arm portions 24 fixed in a state of projecting obliquely upward from both ends of the placement portion 23, and the airframe lateral side portion 12. The support part 25 which is attached to and supports the arm part 24 is provided.

  The placement portion 23 includes a belt-like flat portion 23a (an example of a laterally outer end portion), two belt-like bent portions 23b extending from both ends of the flat portion 23a in a direction intersecting the flat portion 23a, and the folding portions 23b. Two strip-shaped connecting portions 23c that connect the curved portions 23b are provided. The arm portion 24 is formed in a strip shape in which one of the four corners is cut out. One end side of the arm part 24 (the non-existing side of the notch part 24b of the arm part 24) is fixed to the distal end side of the bent part 23b. A long hole 24a is formed along the notch 24b on the other end side of the arm 24 (the side where the notch 24b of the arm 24 is present). The support portion 25 includes a support portion 26 that is fixed to the body frame B and protrudes to the side of the body and has a substantially L-shaped cross section, and a rectangular contact portion 27 that extends from the support portion 26 to the rear side of the body. ing. A pin 28 is fixed to the support portion 26. The rod portion 28 b of the pin 28 passes through the long hole 24 a of the arm portion 24.

(Operation of boarding / exiting steps)
As shown in FIG. 5 (b), when the lower boarding step 22 is in the retracted position folded to the side 12 of the fuselage, the rod portion 28 b of the pin 28 is connected to one end of the long hole 24 a of the arm portion 24 ( 5B, the notch 24b of the arm 24 comes into contact with the body frame B, and the lower boarding step 22 maintains the retracted posture.

  When the lower boarding step 22 is in the retracted position, the lower boarding step 22 enters below the upper boarding step 21 and is placed in a plan view as shown by a two-dot chain line in FIG. All of the flat part 23a of the part 23 is located on the inner side of the right side wall part 10e of the dust-proof cover 10, and a part of the flat part 23a of the mounting part 23 is more than the inclined surface part 10b of the dust-proof cover 10 in a front view. Located inside the aircraft. Further, the planar portion 21a of the upper boarding step 21 in the plan view is located on the inner side of the right side wall portion 10e of the dust cover 10, and the entire planar portion 21a of the upper boarding step 21 is dust-proof in the front view. It is located inside the fuselage with respect to the inclined surface portion 10 b of the cover 10. Therefore, it is possible to prevent the upper boarding / alighting step 21 and the lower boarding / alighting step 22 from coming into contact with the cereals, straws or the like.

  When the lower boarding step 22 in the retracted posture is lifted, the bar portion 28b of the pin 28 comes into contact with the other end of the long hole 24a of the arm portion 24 (the lower end of the paper surface in FIG. 5B). At this time, as shown in FIG. 5 (a), the lower boarding step 22 is turned to the outside of the machine body, and the end surface 29 of the bent portion 23 b of the mounting portion 23 is the contact portion 27 of the support portion 5. It abuts against the abutment surface 27a to prevent further rotation. Accordingly, the lower getting-on / off step 22 is in a use posture in which it protrudes outward from the airframe side portion 12. As described above, the lower step 22 for getting on and off can be changed from the retracted posture to the use posture by simply lifting the lower step 22 for getting on and off (one-touch operation).

  When the lower boarding step 22 is in the use posture, as shown by the solid line in FIG. 3, the lower boarding step 22 has the flat surface portion 23 a of the mounting portion 23 from the right side wall portion 10 e of the dust cover 10. Is also located outside the fuselage. Since the protruding amount of the lower boarding step 22 is larger than the protruding amount of the upper boarding step 21, it is easy for the occupant to put his / her feet on the lower boarding step 22. Further, when the occupant puts his / her foot on the upper boarding / alighting step 21 and the rib 19, the toe side of the occupant's foot enters the inside of the space 20.

  When the lower step 22 for getting in and out of the use posture is turned inward of the machine body, the rod part 28b of the pin 28 comes into contact with one end of the long hole 24a of the arm part 24, and the notch part 24b of the arm part 24 is brought into contact with the machine body frame B. In contact, the lower boarding step 22 in the use posture returns to the retracted posture. As described above, the lower step 22 for getting on and off can be changed from the retracted posture to the use posture by simply rotating the lower step 22 for getting on and off to the inside of the body (one-touch operation).

(Running device)
Since the left crawler traveling device A has the same configuration as the right crawler traveling device A, only the left crawler traveling device A will be described.

  As shown in FIG. 1, the crawler type traveling device A on the left side is connected to a support frame 41 fixed to the body frame B, and to the support frame 41 via a front swing link 42 and a rear swing link 43. A track frame 44, six ground wheels 45 supported on the track frame 44 so as to be free to rotate side by side in the front-rear direction, a crawler drive wheel 46 supported to be driven on the front portion of the support frame 41, and a track frame 44. Tensioning wheels 48 supported so as to be free to rotate by a rear end portion 44 via a tension adjusting mechanism 47, upper rollers 49 supported so as to be free to rotate in the middle portion of the support frame 41, and these wheels The crawler belt 50 is wound around.

  The front portion of the track frame 44 is provided with three front grounding wheels 45a so as to be freely rotatable, and the middle portion of the track frame 44 is provided with one middle grounding wheel 45b so as to be freely rotatable. Two rear grounding wheels 45c are provided on the rear portion of the frame 44 so as to be free to rotate. The front-side grounding wheel 45a, the rear-side grounding wheel 45c, and the upper wheel 49 are formed of the same wheel.

  The front grounding wheel 45a and the rear grounding wheel 45c are configured as outer rotation wheels located outside the pair of guide projections (not shown) of the crawler belt 50, and the intermediate grounding wheel 45b The inner contact wheel 45a has a smaller diameter than the ground contact wheel 45a and the rear contact wheel 45c and is located on the inner side of the pair of guide protrusions of the crawler belt 50.

  The front grounding wheel 45a and the rear grounding wheel 45c are positioned in contact with the crawler belt 50, but the intermediate grounding wheel 45b is positioned slightly away from the crawler belt 50. . An intermediate grounding wheel 45b is provided so as to be close to the position of the center of gravity CG in the front-rear direction of the combine when viewed from the side. In other words, the position of the center of gravity CG in the front-rear direction of the combine is such that the center position (straight line L2 in FIG. 1) of the rearmost ground wheel 45a in the front ground wheel 45a and the frontmost ground in the rear ground wheel 45c. A front-side grounding wheel 45a and a rear-side grounding wheel 45c are provided so as to be positioned between the center position of the wheel 45c (straight line L3 in FIG. 1).

  Thereby, in addition to improving the stability and turning performance of the combine, it is possible to smoothly move the center of gravity when crossing over a fence or getting on and off a truck. Further, since the front grounding wheel 45a, the rear grounding wheel 45c, and the upper wheel 49 are formed of the same wheel, the front grounding wheel 45a, the rear grounding wheel 45c, and the upper wheel 49 are connected to each other. The dual use can improve the maintainability and reduce the cost by reducing the number of parts. Further, when the rear grounding wheel 45c is damaged, it is possible to continue the operation of the combine by performing an emergency measure to replace the upper roller wheel 49.

[Another embodiment]
In the above-described embodiment, the configuration in which the driving unit D is disposed on the right side of the front portion of the body frame B is illustrated. However, instead of such a configuration, the driving unit D is disposed on the left side of the front portion of the body frame B. It is good also as a structure arranged.

  In the present invention, the configuration in which the combine is a self-removing type is illustrated, but the combine may be a normal type.

DESCRIPTION OF SYMBOLS 1 Divider 5 Floor 9 Radiator 10 Dust-proof cover 12 Airframe side part 14 Battery 18 Opening 20 Space 21 Upper boarding step 22 Lower boarding step B Machine body C Cutting part D Driving part L1 Straight line

Claims (6)

A cutting part located at the front of the aircraft,
A driving unit disposed on the right or left side of the front of the aircraft; and
A dust-proof cover provided on a lateral side of the fuselage behind the floor of the driving unit for introducing air into the radiator, and a combined driving unit structure comprising:
The upper boarding / alighting step fixed to the lower side of the fuselage below the floor of the driving unit, and the lower side of the upper boarding / lowering step of the upper boarding step is provided on the side of the body and protrudes outward from the side of the body. A lower step for getting on and off which can be changed to a use posture to be performed and a retracted posture folded to the side of the fuselage side,
In the upper boarding / alighting step, the laterally outer end is located on the inner side of the airframe than the dust cover,
In the lower landing step, the laterally outer end portion is positioned on the inner side of the airframe than the dustproof cover in the retracted posture, and the laterally outer end portion is positioned on the outer side of the airframe than the dustproof cover in the use posture. Combined drive structure configured to be located.   The combine driving section structure according to claim 1, wherein the lower boarding / exiting step is configured to enter below the upper boarding / exiting step in the retracted posture.   The space | side which has the opening which can insert at least the toe side of a passenger | crew's foot | leg is formed in the body lateral side part adjacent to the upper surface of the said step for boarding / alighting upwards toward the inner side of the body. Combined drive section structure.   The combine driving unit structure according to claim 3, wherein a battery is accommodated below the space.   5. The floor and the divider are arranged so that a straight line extending forward from the laterally outer end of the floor overlaps with the divider on the operating unit side in the cutting unit in plan view. The operation part structure of a combine according to item 1.   The combine operating part structure according to any one of claims 1 to 5, wherein the dust cover is located on the outer side of the machine body from the laterally outer end of the floor.

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