JP6460725B2 - Combine - Google Patents

Description

  The present invention relates to a combine that harvests and conveys cereal while traveling, and more particularly, to a headlamp that illuminates the front of the combine.

  In general, a combine is known that has a headlamp that illuminates the front and a worklamp that illuminates the periphery of the divider so that harvesting can be performed even in dark conditions due to sunset or cloudy weather. Conventionally, even if a headlight and work light are arranged above the pulling device and an auxiliary pulling device is installed in front of the pulling device, the irradiation range of the headlight and work light is obstructed. The combine which does not carry out is proposed (refer patent document 1).

JP 2009-136178 A

  Usually, in order to perform a harvesting operation along the grain row, the worker advances the aircraft while visually checking a divider arranged on the outermost side of the aircraft. However, since the combine described in Patent Document 1 raises the headlamp and the work lamp and arranges them above the apparatus, the headlamp and the work lamp are moved upward from the upper cover that covers the lateral transmission cylinder of the pretreatment unit. Or it was the structure which protrudes ahead largely. For this reason, when an operator sits in the cabin, the projecting headlamps and work lamps that protrude greatly interfere with each other, and there is a problem in the visibility of the divider.

  Then, this invention aims at providing the combine which has arrange | positioned so that the protrusion amount to the upper direction or the front of a headlamp may be suppressed, and solved the subject mentioned above.

The present invention supports a pretreatment unit (5) having a plurality of raising devices (12,...) And a divider (11,. The power from the engine arranged at the top of the pre-processing section (5) is transmitted through a transmission shaft (32) built in a horizontal transmission cylinder (31) extending in the left-right direction of the airframe. In the combine (1) transmitted to the pulling device (12, ...),
Headlamps (22, 26) for irradiating the front of the pretreatment unit (5);
A work lamp (23) for illuminating the periphery of the divider (11, 11);
Extending downward from the transmission shaft (32) and transmitting power to the outermost raising devices (12L, 12R) arranged on the outermost side in the left-right direction among the plurality of raising devices (12,...). A pulling shaft,
A pulling transmission cylinder (39) containing the pulling transmission shaft;
The sockets (22c, 26c) of the headlamps (22, 26) are below the axial center of the transmission shaft (32), above the upper surface of the outermost raising device (12L, 12R), and the raising and aircraft outside in the lateral direction than the transmission cylinder (39), before Symbol outermost Pick device (12L, 12R) inboard from the outer surface in the horizontal direction of, and in the axial direction of the transmission shaft (32) As viewed, at least a part is arranged so as to overlap the transmission cylinder (39) ,
The work lamp (23) is disposed on the outer side in the left-right direction with respect to the outermost raising device (12L) and the headlamp (22) and on the rear side in the front-rear direction with respect to the headlamp (22). And
The front surfaces of the headlamp (22) and the work lamp (23) are integrally covered by a single lens (25),
The area of the reflector (22a) of the headlamp (22) is larger than the area of the reflector (23a) of the work lamp (23),
The reflector (23a) of the work lamp (23) is disposed to be inclined to the outside of the body in the left-right direction with respect to the direction of the reflector (22a) of the headlamp (22), and the headlamp It is arranged so as to overlap in the vertical direction with respect to the reflector (22a) of the lamp (22).
It is characterized by that.

  In addition, although the code | symbol in the said parenthesis is for contrast with drawing, it does not limit the structure of this invention at all.

According to the first aspect of the present invention, the socket of the headlamp is located below the shaft center of the transmission shaft, above the top surfaces of the plurality of pulling devices, outside the fuselage in the left-right direction from the pulling transmission tube, And it has arrange | positioned inside the body rather than the outer side surface in the said left-right direction of the said outermost raising apparatus. For this reason, the headlamp socket is connected to the transmission shaft, the outermost raising device and the raising transmission cylinder, while the irradiation range of the headlamp is not greatly blocked by the relatively long grain ridge or auxiliary raising device. It is arrange | positioned so that a horizontal transmission pipe | tube may be avoided using the limited space enclosed by, and it can arrange | position, suppressing the protrusion to the front and front by a headlamp. Thereby, the visibility of a divider can be improved. In addition, since the socket of the headlamp is raised outside and arranged on the inner side of the outer side of the device in the left-right direction, the combine can be made compact without increasing the width of the main unit.
In addition, since the work lamp is raised outside and the rear side of the headlight from the device and the headlight, the width of the body is suppressed while suppressing upward and forward protrusions by the headlight and the worklight. An arrangement space can be secured without widening. Thereby, the visibility of a divider can be improved.

The whole side view which shows the combine which concerns on this Embodiment. The front view. The perspective view which shows the pre-processing part of a combine. The perspective view which shows the transmission structure of a pre-processing part. It is a figure which shows arrangement | positioning of the socket of a headlamp, Comprising: (a) is a left view, (b) is a right view. The top view which shows the irradiation direction of a headlamp and a work lamp. The side view.

  Hereinafter, embodiments of the present invention will be described with reference to the drawings. As shown in FIGS. 1 and 2, the combine 1 according to the present embodiment has a traveling machine body 3 supported by a traveling apparatus 2 that is a pair of left and right crawler traveling apparatuses. Is provided with a pre-processing unit 5 for cutting grain culm in the field so as to be movable up and down. A cabin 6 on which a worker performs a driving operation is provided on one front side of the traveling machine body 3, and on the other side, the cereals harvested and transported by the pretreatment unit 5 are threshed and processed. A threshing device 7 for performing a sorting process is provided. A grain tank 9 for storing the grains threshed and selected by the threshing device 7 is disposed behind the cabin 6. The grain tank 9 stores the grain tank 9 behind the cabin 6. A discharge auger 10 is provided for discharging the grain out of the machine. An engine (not shown) is accommodated in the cabin 6 below the driver seat (not shown).

  The pre-processing unit 5 causes a plurality of (six in the present embodiment) dividers 11, which are provided in the front part to weed the cereals, and cause the cereals that have been weeded behind the dividers 11. A plurality of (in this embodiment, five) pulling devices 12,..., A reciprocating cutting blade 13 that cuts the culm, and a stock rake device that scrapes the raised culm stock side 15 and a conveying device 16 that conveys cereals harvested by the cutting blade 13 backward and delivers them to a feed chain (not shown) of the threshing device 7. Side covers 17 and 17 that can be easily attached and detached for maintenance and maintenance are disposed on both side surfaces of the pre-processing unit 5, and these side covers 17 and 17 are arranged on the pre-processing unit 5. It covers the outside of the aircraft in the left-right direction.

  As shown in FIGS. 2 and 3, an upper cover 19 extending in the left-right direction is provided above the plurality of pulling devices 12,... Between the upper cover 19 and the side covers 17, 17. The left and right light units 20 and 21 are provided. Hereinafter, in the left-right direction, the left side or the right side with respect to the aircraft forward direction is simply referred to as the left side or the right side. The left light unit 20 includes a headlamp 22 and a work lamp 23 that are integrally arranged side by side on the left and right sides, and a lens 25 that covers the front side of the headlamp 22 and the work lamp 23 in a curved manner. Have. The right light unit 21 includes a headlamp 26 and a work lamp 27 that are integrally arranged on the left and right sides, and a lens 29 that covers the front side of the headlamp 26 and the work lamp 27 in a curved surface. have.

  That is, the left headlamp 22 and the work lamp 23, and the right headlamp 26 and the work lamp 27 are all disposed above the plurality of pulling devices 12,. The left and right light units 20 and 21 are provided substantially symmetrically. The headlamps 22 and 26 are arranged inside the machine body, and the work lights 23 and 27 are arranged outside the machine body. In addition, dustproof covers 28 (see FIG. 2) and 30 extend behind the upper cover 19, and these dustproof covers 28 and 30 cover the upper part of the conveying path of the cereal and prevent scattering of dust and the like. doing.

  As shown in FIG. 4, a lateral transmission cylinder 31 extends in the left-right direction behind the upper cover 19. The lateral transmission cylinder 31 includes a lateral transmission shaft 32 (transmission shaft, see FIG. 5A). ) Is built-in. A vertical transmission cylinder 33 rises at the left end of the pre-processing unit 5, and the power from the engine transmitted to a vertical transmission shaft (not shown) built in the vertical transmission cylinder 33 is transmitted to the transmission gear case 35. It is branched to the horizontal transmission shaft 32 via A connection case 36 to which the lateral transmission cylinder 31 is connected is attached to the upper surface of the transmission gear case 35. A support frame 37 fixed to a fixing member extends upward at the right end of the pretreatment unit 5, and the support frame 37 supports the right end side of the horizontal transmission cylinder 31. That is, the lateral transmission cylinder 31 is supported by the connection case 36 on the left end side and the support frame 37 on the right end side.

  Five pulling transmission cylinders 39,... Branch downward from the lateral transmission cylinder 31, and the pulling transmission shafts (not shown) built in these pulling transmission cylinders 39,. Power is transmitted to each of the two raising devices 12,. A sprocket 40 is provided at the lower part of each pulling transmission cylinder 39, and the power is transmitted to the chain with claw (not shown) of the pulling device 12 by the sprocket 40. Each pulling device 12 is provided with a mounting portion 41 of an auxiliary pulling device (not shown) at a position corresponding to the sprocket 40. Mowing performance can be improved.

  Here, the arrangement of the headlamp 22 and the work lamp 23 of the left light unit 20 and the headlamp 26 and the work lamp 27 of the right light unit 21 will be described in detail. First, the left light unit 20 will be described. In the following description, of the five pulling devices 12,..., The pulling device arranged on the outermost side in the left-right direction is referred to as the outermost pulling device, and in particular in FIG. The arranged raising device is called the leftmost raising device 12L, and the raising device arranged on the rightmost side is called the rightmost raising device 12R.

  As shown in FIG. 4, the left light unit 20 has a center line C1 (center) above the leftmost pulling device 12L (outermost pulling device) and in the left-right direction of the leftmost pulling device 12L. Part) outside the fuselage. The headlamp 22 of the light unit 20 is disposed so as to overlap the leftmost pulling device 12 </ b> L in the left-right direction and on the outer side of the fuselage 39 in the left-right direction than the transmission cylinder 39. The work lamp 23 is disposed outside the machine body in the left-right direction of the leftmost pulling device 12 </ b> L and the lateral transmission cylinder 31. Moreover, the work lamp 23 is arrange | positioned behind the headlamp 22 (refer FIG. 6).

  The area of the reflector 22 a of the headlamp 22 is set larger than the area of the reflector 23 a of the work lamp 23. Further, as shown in FIG. 5A, the socket 22c into which the light main body 22b of the headlamp 22 is screwed is lower than the axial center of the lateral transmission shaft 32 and more than the leftmost pulling device 12L. It is arranged above. As shown in FIG. 5A, the socket 22 c of the headlamp 22 is arranged at a position where it does not interfere with the connection case 36 and the transmission gear case 35, and is located on the side of the transmission cylinder 39 in a side view. Yes.

  Next, the right light unit 21 will be described. As shown in FIG. 4, the right light unit 21 is located above the rightmost pulling device 12R (outermost pulling device) and on the center line C2 (center of the rightmost pulling device 12R in the left-right direction). Part) outside the fuselage. The headlamp 26 of the light unit 21 is disposed on the outer side of the fuselage 39 in the left-right direction so as to overlap with the rightmost pull-up device 12 </ b> R in the left-right direction. The work lamp 27 is disposed outside the machine body in the left-right direction of the rightmost pulling device 12 </ b> R and the lateral transmission cylinder 31. The work lamp 27 is disposed behind the headlamp 26.

  The area of the reflector 26 a of the headlamp 26 is set larger than the area of the reflector 27 a of the work lamp 27. Further, as shown in FIG. 5B, the socket 26c into which the light main body 26b of the headlamp 26 is screwed is lower than the axial center of the lateral transmission shaft 32 and more than the rightmost raising device 12R. It is arranged above. As shown in FIG. 5B, the socket 26 c of the headlamp 26 is disposed at a position where it does not interfere with the support frame 37 and beside the transmission cylinder 39 as shown in FIG.

  Next, the irradiation directions of the headlamps 22 and 26 and the work lamps 23 and 27 will be described. However, since the left light unit 20 and the right light unit 21 are substantially bilaterally symmetric, Only the irradiation direction of the work lamp 23 will be described. As shown in FIGS. 6 and 7, the headlamp 22 irradiates light in the direction of arrow F toward the front and slightly below the pretreatment unit 5. The work lamp 23 emits light toward the periphery of the divider 11 arranged on the leftmost side, outward of the machine body, and forward and downward, that is, in the direction of the arrow W. Since the light main body 22b of the headlamp 22 and the light main body 23b of the work lamp 23 are mounted in the same direction, irradiation is performed depending on the orientation and shape of the reflector 22a of the headlamp 22 and the reflector 23a of the work lamp 23. The direction, that is, the directions of arrows F and W are defined. Since the light main bodies 22b and 23b are attached in the same direction, the attachment / detachment workability can be improved.

  As shown in FIG. 7, a substantially half-moon-shaped recess 17 a is formed in the side cover 17 immediately below the work lamp 23. The concave portion 17a is formed so as not to prevent light irradiation in the direction of the arrow W of the work lamp 23, can reliably illuminate the periphery of the leftmost divider 11, and improves the visibility of the divider 11. Can do. The recess 17a is provided with a lock handle 17b, and the side cover 17 can be easily attached and detached by operating the lock handle 17b. The side cover 17 on the right side surface of the pretreatment unit 5 is similarly provided with a recess 17a and a lock handle 17b, and of course has the same effect.

  Since this Embodiment consists of the above structures, an operator sits on the driver's seat in the cabin 6, operates the combine 1, and performs the harvesting / threshing work of the cereal. The operator turns on the left and right light units 20 and 21 when sunset approaches during the work.

  By turning on the headlamps 22 and 26, the front visibility of the preprocessing unit 5 can be improved. Then, by turning on the work lamps 23 and 27, the visibility of the leftmost and rightmost dividers 11 and 11 can be improved, and the cutting operation can be efficiently performed in accordance with the grain row. At this time, since the concave portion 17a is formed in the side cover 17, the left and right dividers having poor visibility for the worker who has entered the cabin 6 can illuminate directly below the work lights 23 and 27. 11 and 11 can be reliably illuminated.

  Moreover, since the right and left light units 20 and 21 are disposed above the plurality of pulling devices 12,..., The left and right light units 20 and 21 are attached to a relatively long grain pod extending from the field or the mounting portion 41 of the pulling device 12. The visibility of the divider 11 and the front can be improved without obstructing the irradiation of light by the auxiliary pulling device. Then, when the side covers 17 and 17 are removed by operating the lock handle 17b of the side cover 17, the left and right light units 20 and 21 are positioned so as not to interfere with the leftmost pulling device 12L and the rightmost pulling device 12R. Since it is arranged, maintenance such as replacement of the light main bodies 22b, 23b, 26b, and 27b can be easily performed.

  The left and right light units 20 and 21 are arranged outside the fuselage from the center lines C1 and C2 of the leftmost and rightmost pulling devices 12L and 12R. More specifically, the headlamps 22 and 26 are respectively leftmost. In addition, the right and left pulling devices 12L and 12R are arranged so as to overlap in the left-right direction, and the work lamps 23 and 27 are arranged in the left-right direction with respect to the left-most and right-most pulling devices 12L and 12R and the lateral transmission cylinder 31, respectively. Therefore, the protrusions of the light units 20 and 21 in the forward and upward directions can be reduced while reducing the width of the airframe and having a compact structure. Thereby, the operator seated in the cabin 6 can visually recognize the leftmost and rightmost dividers 11 and 11 without being obstructed by the light units 20 and 21, and the visibility of the divider can be improved. .

  Further, since the sockets 22c and 26c of the headlamps 22 and 26 are disposed below the lateral transmission shaft 32 of the lateral transmission cylinder 31 and are pulled up to avoid the transmission cylinder 39 laterally, these lateral transmissions are performed. The protrusions forward and upward of the light units 20 and 21 can be reduced without interfering with the cylinder 31 and the raised transmission cylinder 39 while being close to each other. More specifically, the socket 22c of the left headlamp 22 is raised and disposed at a position surrounded by the transmission cylinder 39, the connecting case 36, and the transmission gear case 35, and the socket 26c of the right headlamp 26 is lateral. The transmission cylinder 31 and the support frame 37 are disposed so as to avoid the sides. In addition, the work lamps 23 and 27 are arranged behind the headlamps 22 and 26.

  Combined with such a configuration, the headlamps 22 and 26 and the work lamps 23 and 27 are disposed above the pulling device 12,. Therefore, the protrusion of the light units 20 and 21 forward and upward can be reduced, and the visibility of the divider can be improved.

  Further, while the headlamps 22 and 26 and the work lamps 23 and 27 are arranged in a limited space, the area of the reflector of the headlamps 22 and 26 is larger than the area of the reflector of the work lamps 23 and 27. Since it is set, it is possible to irradiate light well in accordance with the irradiation range.

  Note that the headlamp and the work lamp may both be disposed outside the machine body in the left-right direction with respect to the outermost raising device.

  Further, the area of the reflector of the headlamp or work lamp may be either a projected area or a surface area in front view.

  Further, in this embodiment, the shape of the concave portion of the side cover is formed in a substantially half-moon shape, but if the straight line connecting the work lamp and the divider is not obstructed by the side cover, the shape of the concave portion is It may be formed.

DESCRIPTION OF SYMBOLS 1 Combine 3 Traveling machine body 5 Pre-processing part 11 Divider 12, ... Plural raising device 12L Outermost raising device (leftmost raising device)
12R Outermost lifting device (rightmost lifting device)
22, 26 Headlamps 22c, 26c Sockets 23, 27 Work lamp 31 Horizontal transmission cylinder 32 Transmission shaft (transverse transmission shaft)
39 Pulling transmission cylinder

Claims (1)

A pre-processing unit having a plurality of pull-up devices and dividers is supported in front of the traveling machine body so as to be movable up and down, and power from an engine disposed in the traveling machine body is disposed on an upper part of the pre-processing unit and is In a combine that is transmitted to a plurality of the pulling devices via a transmission shaft built in a lateral transmission cylinder extending in the direction,
A headlamp for illuminating the front of the pretreatment unit;
A work light that illuminates the periphery of the divider;
An erecting transmission shaft that extends downward from the transmission shaft and transmits power to the outermost erecting device arranged on the outermost side in the left-right direction among the plurality of elevating devices;
A pulling transmission cylinder containing the pulling transmission shaft;
Socket of the headlight, lower than the shaft center of the transmission shaft, wherein above the upper surface of the outermost Pick device, the Pick body outside in the lateral direction than transmission cylinder, before SL and outermost cause Arranged so that at least a part of the device is raised and overlaps the transmission cylinder when viewed in the axial direction of the transmission shaft and the outer side surface of the device in the left-right direction ,
The work lamp is disposed outside the fuselage in the left-right direction than the outermost raising device and the headlight and on the rear side in the front-rear direction than the headlight,
The front surfaces of the headlamp and the work lamp are integrally covered by a single lens,
The area of the reflector of the headlamp is larger than the area of the reflector of the work lamp,
The reflector of the work lamp is disposed so as to be inclined to the outside of the body in the left-right direction with respect to the direction of the reflector of the headlamp, and over the reflector in the vertical direction. Wraps and is placed,
Combine that is characterized by that.

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