JP5246227B2 - Ride type rice transplanter - Google Patents

Description

The present invention relates to a riding type rice transplanter .

Conventionally, there is a working traveling vehicle in which an engine is mounted on a machine body and a fertilizer is provided at the rear of the machine body (see Patent Document 1) .

JP 2003-154858 A

The wet granular fertilizer may adhere to the fertilizer transport part of the fertilizer application and cause clogging of the fertilizer, and there has been a problem in performing appropriate fertilization work.
Further, when the engine is mounted at the center of the fuselage, there is a problem in that the fertilizer scattered from the fertilizer near the engine is applied to the engine, corroding the engine and shortening its life.

The present invention enables a simple and strong frame structure, can be made into a low-priced and compact machine structure, can exhibit excellent running performance due to its weight reduction, and is also safe and workable. The task is to obtain an improved riding rice transplanter.

In order to solve the above-mentioned problem, the invention according to claim 1 is a riding type rice transplanter in which a rice transplanter (3) is mounted on a traveling vehicle (1) via a lifting link device (2). ) The frame (10c) provided on the lower side is extended in a U-shape downward to form a U-shaped portion (10i). The handrail part (10j) for getting on and off is arranged on the side of the cockpit (20) and near the seedling platform (163) of the rice transplanter (3). It was set as the riding type rice transplanter which fixed the step (10k) for boarding / alighting to the shape part (10i).

According to the second aspect of the present invention, a fertilizer tank (4a) of a fertilizer application device (4) is provided at the rear of the machine body, and the fertilizer application device (4) feeds the fertilizer in the fertilizer tank (4a) by the feeding device (4b). It was set as the structure conveyed with the pressure wind generated by (4c), and it was set as the riding type rice transplanter of Claim 1 arrange | positioned near the fertilizer tank (4a) for the handrail part for boarding / alighting .

The invention according to claim 3 is configured such that the engine (12) equipped with the radiator (12c) is mounted on the fuselage, and the blower (4c) sucks air from the rear side in the longitudinal direction of the radiator (12c). The riding type rice transplanter described in Item 2 was used.

According to a fourth aspect of the present invention, the radiator (12c) is disposed behind the engine (12) mounted in the center of the airframe, and the engine waste hot air is discharged toward the rear of the airframe by the radiator fan (12d). The passenger type rice transplanter according to claim 3, wherein the blower (4c) sucks air from a rear position of the radiator (12c).

According to the first aspect of the present invention, since the step 10k for getting on and off and the handrail part 10j for getting on and off are configured using the frame of the traveling vehicle 1, it is possible to form a strong frame configuration with a simple configuration, Further, since the handrail portion 10j is arranged on the side of the cockpit 20 and near the seedling platform 163 of the rice transplanter 3, it is not only a handrail for getting on and off the aircraft, but also a seedling to the seedling platform 163. It can also be used as a handrail during supply, improving safety and workability.

According to the invention described in claim 2, in addition to the effect of the invention described in claim 1, the handrail portion 10j is disposed near the fertilizer tank 4a, so that it can be used as a handrail when supplying fertilizer to the fertilizer tank 4a. It can be used and is safe and improves workability.

According to the third aspect of the invention, in addition to the effect of the second aspect of the invention, the blower 4c sucks hot air generated by the radiator 12c and uses it for conveying the granular fertilizer. This prevents the wet granular fertilizer from adhering to the fertilizer transport section of the fertilizer application device 4 and causing clogging of the fertilizer, and appropriate fertilization work can be performed. In addition, the blower 4c can be easily sucked by the flowing air of the radiator fan 12d that generates the cooling air of the radiator 12c, and the blower 4c may be a small one having a relatively small electromotive force. Thus, the working vehicle can be reduced in weight, and excellent running performance can be exhibited by the reduction in weight.

According to the invention described in claim 4 , in addition to the effect of the invention described in claim 3, for the purpose of improving the balance between the front and rear of the aircraft and reducing the size of the aircraft, the engine 12 is mounted in the center of the aircraft and the fertilizer is installed at the rear of the aircraft. 4 is a working traveling vehicle provided with a fertilizer tank 4a. Since the radiator 12c is disposed behind the engine 12 and the engine exhaust hot air is discharged toward the rear of the machine body by the radiator fan 12d. Even if the fertilizer leaks from the device 4 and falls downward, the waste hot air is forced to flow backward from the engine 12, so that the fertilizer can be blown rearward and flow into the engine 12 side. Can be prevented. Therefore, it is possible to avoid such a situation that the corrosion suffered a fertilizer in which the engine 12 is scattered, Ru can do the proper work with no engine trouble. Further, since the blower 4c of the fertilizer application device 4 is configured to suck air from the rear position of the radiator 12c, the blower 4c sucks hot air exhausted rearward from the radiator 12c and uses it for conveying the granular fertilizer. Therefore, there is an effect of drying the granular fertilizer, and the wet granular fertilizer is prevented from adhering to the fertilizer transport portion of the fertilizer application device 4 and causing clogging of the fertilizer, and appropriate fertilization work can be performed. Further, since the direction of the wind of the radiator fan 12d that causes the cooling air of the radiator 12c and the suction direction of the blower 4c are the same direction, the flow of waste heat air of the radiator fan 12d helps the suction of the blower 4c, and the suction of the blower 4c. Since the power works to assist the flow of the waste heat wind of the radiator fan 12d , the radiator fan 12d and the blower 4c are promoted to each other, and the radiator fan 12d and the blower 4c are used in a small size with a relatively small electromotive force. Therefore, an inexpensive and compact machine configuration can be achieved, the working vehicle can be reduced in weight, and excellent driving performance can be exhibited due to the reduction in weight.

BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is an overall side view showing an eight-row planting type rice transplanter that is an embodiment of the present invention. It is a whole top view of the riding type rice transplanter shown in FIG. It is a schematic plan view which shows the transmission structure of a traveling vehicle. It is an expanded sectional view of a mission case. It is an enlarged side view of the principal part. It is a rear view of a change lever part. It is a block circuit diagram of a control system. It is a whole side view of the 8-row planting type rice transplanter which shows a 2nd example. It is a whole top view of the 8-row planting type rice transplanter which shows the 3rd example.

  An 8-row planted rice transplanter as an embodiment of the present invention will be described in detail with reference to the drawings. The traveling vehicle 1 is provided with a rice planting device 3 which is a kind of working device by using a lifting and lowering link device 2 and provided with a fertilizer application device 4, and is configured as a riding type fertilizer rice transplanter as a whole. The traveling vehicle 1 is a four-wheel drive vehicle having a pair of left and right front wheels 6 and 6 and rear wheels 7 and 7 as drive wheels. The left and right rear wheels 7, 7 are each composed of a main wheel 7a, an inner auxiliary wheel 7b having a slightly smaller diameter, and an outer field wheel 7c in order to increase the traction force.

A transmission case 11 is fixed to the front portions of the left and right main frames 10 and 10 with bolts, and a steering post 14 projects upward from the front portion of the transmission case 11.
A steering handle 16 and an operation panel 17 are provided at the upper end of the steering post 14. A fuselage cover 19, in which steps are integrally formed from a synthetic resin serving as a control floor, is attached to the upper part of the fuselage, and a cockpit seat 20 is installed above the diesel engine 12 (the cockpit 20 is the fuselage seat). The cover 19 is attached to the rear upper surface).

  The front wheels 6, 6 are pivotally supported by front wheel support cases 22, 22 provided on the side of the mission case 11 so as to be capable of turning. The rear wheels 7 and 7 are pivotally supported by rear wheel support cases 24 and 24 that are integrally attached to the left and right ends of the rolling rod 23. The rolling rod 23 is rotatably supported in a plane perpendicular to the traveling direction by a rolling shaft 25 projecting from a horizontal frame 10a connecting the rear ends of the left and right main frames 10, 10.

  The lower part of a U-shaped front connecting frame 10b connecting the both is welded and fixed to the front parts of the left and right main frames 10, 10, and the front horizontal pipe frame 10c extending in the left-right direction is fixed to the front connecting frame 10b. Has been. The lower portions of the U-shaped rear connection members 10d, 10d are fixed to the rear portions of the left and right main frames 10, 10 by welding, and the rear pipe frame 10e extending in the left-right direction is fixed to the rear connection members 10d, 10d. Has been.

  The left and right engine support frames 10f and 10f in the front-rear direction are fixed to the center of the front horizontal pipe frame 10c and the rear pipe frame 10e, and the front rubber mounts M1 and M1 and the rear part are attached to the left and right engine support frames 10f and 10f. A water-cooled diesel engine 12 is mounted via rubber mounts M2 and M2. The front ends of the left and right engine support frames 10f and 10f are fixed to the side wall of the transmission case 11 so as to protrude forward from the front horizontal pipe frame 10c.

  Further, a base portion of a front frame 10g having a plan view gate shape is fixed to a front portion of the front horizontal pipe frame 10c. A middle part in the front-rear direction of the front frame 10g is fixedly supported by the mission case 11, and left and right bumpers 13, 13 are fixed to the front end part thereof. Further, left and right aircraft cover support frames 10h in the front-rear direction are fixed to the left and right sides of the front horizontal pipe frame 10c and the rear pipe frame 10e. The left and right aircraft cover support frames 10h. The machine body cover 19 that also serves as a step for moving or working is fixedly supported.

  The diesel engine 12 is mounted such that its output shaft 12a is provided toward the left side, and a drive pulley 12b is provided on the output shaft 12a. And the radiator 12c is arrange | positioned at the rear part of the diesel engine 12, and the radiator fan 12d driven with an electric motor is mounted in the rear wall of the diesel engine 12. Further, the exhaust muffler 12e of the diesel engine 12 is disposed at a position below the body cover 19 in a position near the outside of the left output shaft 12a in a front view of the body. Therefore, since the exhaust muffler 12e, which is a heavy object, is arranged near the outside of the output shaft 12a at the center position in the front-rear direction of the diesel engine 12, the vibration of the exhaust muffler 12e due to the operation of the diesel engine 12 This reduces the vibration and noise of the entire aircraft, improves the working environment of the working vehicle, and improves the workability.

  Further, the radiator 12c provided at the rear part of the diesel engine 12 is a left and right center position of the fuselage, and is a position where it is stuck in the longitudinal direction of the fuselage at the inner position of the left and right rear wheels 7 and 7 (the inner position of the left and right inner auxiliary wheels 7b and 7b). (The position where only the distance a is stuck), and the front-rear length of the aircraft is shortened.

  The hydraulic continuously variable transmission HST is fixed to the right side wall of the transmission case 11 when viewed from the front of the machine body. It is configured to be driven by the engine 12. The driving force of the hydraulic continuously variable transmission HST is transmitted from the output shaft 36 to the mission input shaft 34 via the belt B2. The trunnion operating arm mounted on the trunnion shaft provided protruding from the side wall of the hydraulic continuously variable transmission HST and the HST operating lever 112 provided on the right side of the cockpit 20 are linked by a linked operating mechanism, and the HST operation is performed. When the lever 112 is in the center position in the front-rear direction (neutral position), the hydraulic continuously variable transmission HST is held in neutral and the aircraft is stopped, and the HST operating lever 112 is directed from the neutral position to the front side (maximum forward speed position). The trunnion shaft is gradually operated in the forward direction, and the aircraft gradually increases in forward speed. Conversely, as the HST operating lever 112 is operated from the neutral position toward the maximum reverse speed position, the trunnion shaft is gradually operated in the reverse direction, and the aircraft gradually increases in reverse speed.

On the other hand, two fuel tanks 12f are arranged on the left side of the diesel engine 12 when viewed from the front of the fuselage, and are fixed so as to be suspended from the left fuselage cover support frame 10h.
Accordingly, since the muffler 12e is disposed on the left side of the diesel engine 12 and the fuel tank 12f is disposed on the right side as described above, the fuel tank 12f is disposed at a position far from the muffler 12e. Thus, the fuel tank 12f can be prevented from being heated and is safe, and since the fuel tank 12f is arranged on the left and right sides of the airframe, the left-right balance of the airframe is improved and the running performance is improved. Therefore, the riding type rice transplanter can perform an appropriate seedling planting operation in the paddy field by the appropriate traveling performance of the traveling vehicle 1.

  On the other hand, the fertilizer application device 4 is disposed above the rear portion of the diesel engine 12. As described above, the radiator 12 c is disposed at the rear portion of the diesel engine 12 and is driven by an electric motor on the rear wall of the diesel engine 12. Since the radiator fan 12d is mounted so that the cooling air of the radiator 12c flows toward the rear of the diesel engine 12, even if the fertilizer leaks from the fertilizer application apparatus 4 and falls downward, the diesel engine 12 Since the cooling air is forcibly flowing toward the rear, the fertilizer can be prevented from being blown rearward and flowing into the diesel engine 12 side. Therefore, the situation where the diesel engine 12 is corroded by the scattered fertilizer can be avoided, and appropriate fertilization and seedling planting work without engine trouble can be performed.

  In addition, the fertilizer application device 4 includes a fertilizer tank 4a in which granular fertilizer is put, a feeding device 4b that feeds the granular fertilizer in the fertilizer tank 4a in a fixed amount for each strip, and compressed air generated by the electric blower 4c in an air chamber. Each strip that guides the granular fertilizer to the grooving device 4f that makes fertilizer in the mud by creating a fertilizer groove in the field by the compressed air supply section 4e that is sent to each strip through 4d and the pressurized wind of the pressurized wind supply section 4e. Each fertilizer pipe is composed of 4 g. The air suction portion 4c ′ of the electric blower 4c extends to the rear position of the radiator 12c, and the air suction port 4c ″ is disposed so as to face the rear of the radiator 12c. Since the electric blower 4c sucks the hot air exhausted backward from the radiator 12c and uses it for conveying the granular fertilizer, it has an effect of drying the granular fertilizer, and the wet granular fertilizer is fed into the feeding device 4b and fertilizer. It is prevented that the fertilizer is clogged by adhering to the pipe 4g, and appropriate fertilization work can be performed.

  Furthermore, since the direction of the wind of the radiator fan 12d that causes the cooling air of the radiator 12c and the suction direction of the electric blower 4c are the same direction, the flow of waste heat air from the radiator fan 12d helps the suction of the electric blower 4c, and the electric blower Since the suction force of 4c serves to assist the flow of waste heat air from the radiator fan 12d, the radiator fan 12d and the electric blower 4c are in a mutually supporting relationship, and the radiator fan 12d and the electric blower 4c are relatively small in the electromotive force. Smaller ones may be used, resulting in an inexpensive and compact machine configuration, which makes it possible to reduce the weight of the work vehicle and to exhibit excellent driving performance due to the light weight (especially in paddy field field driving). If the working vehicle is light, its running performance will be much better).

  On the other hand, a main clutch 43 is provided on the mission input shaft 34, and the driving force of the hydraulic continuously variable transmission HST is transmitted to the mission input shaft 34 via the main clutch 43. The main clutch 43 is a well-known multi-plate clutch. In the figure, 44 is a friction plate on the main clutch shaft side, 45 is a friction plate on the mission input shaft side, 46 is a spring that presses both friction plates, and 47 and 48 are switching operations. Fixing member and sliding member.

  The mission input shaft 34, the counter shaft 50, the traveling primary shaft 51, the traveling secondary shaft 52, the planting primary shaft 53, and the planting secondary shaft 54 are supported in parallel on the front portion of the casing 40 of the mission case 11. ing. The gear G1 of the mission input shaft 34 and the gear G2 of the counter shaft 50, and the gear G2 and the gear G3 of the traveling primary shaft 51 are engaged with each other, and the rotation of the mission input shaft 34 is transmitted to the traveling primary shaft 51 in the forward direction. It is done.

  As the main transmission B, the gear G3 and the gear G4 are respectively fitted in fixed positions on the traveling primary shaft 51, and the gears G5 and G6 formed integrally with the traveling secondary shaft 52 are slidable in the axial direction. It is mated. When the gears G5 and G6 are moved by the shifter 56 and the gears G4 and G5 are engaged with each other, a low working speed is obtained, and when the gears G3 and G4 are engaged, a high road traveling speed is obtained. The planted primary shaft 53 is fitted with a gear G7 and a back gear G8 that are always meshed with the gear G4. When the gear G6 is meshed with the back gear G8, the reverse speed is achieved. The position where the gears G5 and G6 do not mesh with any gear is neutral. A change lever 90 operated by the main transmission B is provided on the operation panel 17.

  As the inter-strain transmission C, gears G9 and G10 formed integrally with the planting primary shaft 53 are slidably fitted in the axial direction, and gears G11 and G12 are mounted on the planting secondary shaft 54. Are attached to each. By appropriately moving the gears G9 and G11 with the shifter 57, three combinations of the gear G9 and the gear G10, the gear G10 and the gear 11, and the gear G10 and the gear G12 are obtained, and the three-stage stock switching can be performed. It is transmitted from the planting secondary shaft 54 to the planting part transmission shaft 58 via the bevel gears G13 and G14.

  Rear axles 60, 60 and front axles 61, 61 are supported at the rear of the casing 40, and are transmitted from the traveling secondary shaft 52 to the rear axles 60, 60 via the rear differential device D and from the rear differential device D to the front differential. It is transmitted to the left and right front axles 61 and 61 via the device E. The left and right front wheels 61 and 61 are driven and rotated by the left and right front axles 61 and 61, respectively.

  The rear differential device D includes a container 63 in which a gear G16 meshing with the gear G15 of the traveling secondary shaft 52 is formed on the outer peripheral portion, a primary bevel gear G17 attached to a longitudinal axis 64 in the container, and left and right rear axles 60, 60. The secondary bevel gears G18 and G18 attached separately to each other are housed in a state where they mesh with each other, and the driving force transmitted to each axle is appropriately changed.

  The front differential device E has the same configuration as the rear differential device D. In the figure, 65 is a container, 66 is a vertical axis, G19 is a gear on the rear differential device side, G20 is a gear on the front differential device side, and G21 is attached to the vertical axis 66. The bevel gear G22 is a bevel gear attached to the front axle 61. The rear differential device D and the front differential device E are provided with differential lock devices F and H that stop the differential function and transmit the driving force evenly to the left and right axles. The differential lock device F (H) includes a claw 69 (70) formed on the container 63 (64), a claw 73 (74) of a differential lock member 71 (72) fitted to a square rod portion of the axle, and an axle 50 (51). ) Are fixed to each other. A differential lock lever 91 for operating the rear wheel differential lock device F is provided on the operation panel 17. The front wheel differential lock device H is configured such that the differential function is stopped when a differential lock pedal 91 ′ provided on the body cover 19 is depressed. The diff lock lever 91 and the diff lock pedal 91 'are both arranged at the front of the aircraft. (Ride on the front edge of the aircraft to replace your body weight) and move the aircraft forward or backward to safely cross this heel, but at this time either one of the left and right front wheels 6, 6 or left and right rear When either of the wheels 7 or 7 is idle, the pilot can immediately operate the diff lock lever 91 and the diff lock pedal 91 'in the front of the aircraft in an easy posture so that the diff lock state can be set and the vehicle can be safely crossed. it can.

  The rear axles 60, 60 are connected to the side clutch shafts 76, 76 by bevel gears G23, G24,..., And are further transmitted from the side clutch shafts to the rear output shafts 77, 77 via the side clutches I, I. The side clutch I is a multi-plate clutch, 80 is a friction plate on the side clutch shaft side, and 81 is a friction plate on the rear output shaft side. An operating cylinder 82 is slidably fitted to the rear output shaft 77 and is urged by a leaf spring 83 in a direction in which both friction plates are pressed, and the side clutch I is always engaged. When the operating cylinder 82 is moved in the direction opposite to the urging direction by the shifter 85I, the side clutch I is disengaged.

  Further, rear wheel brake devices J and J are provided on the rear output shafts 77 and 77. The rear wheel brake device J presses the pressure plates 88,... Against the disks 87,... Attached to the rear output shaft 77 for braking, and the pressure plates 88,. That is, the side clutch I is normally engaged and the rear wheel brake device J is not engaged, and the side clutch I is disengaged by operating the shifter 85I to move the operating cylinder 82 in the direction opposite to the urging direction. When the shifter 85J is operated, the rear wheel brake device J is applied. The operations of the side clutch I and the rear wheel brake device J (operations of the left and right shifters 85I and 85J) are performed by a pedal 140 provided on a body cover 19 described later. Note that the base of the left and right clutch operation arm 86I is fixed to the left and right shifter 85I, and the base of the left and right brake operation arm 86J is fixed to the left and right shifter 85J.

  The rear end portions of the rear output shafts 77, 77 protrude out of the casing 40, and left and right rear wheel transmission shafts 89, 89 that are transmitted to the rear wheel support cases 24, 24 are connected to the protruding end portions. The left and right rear wheels 7, 7 are driven and rotated by the left and right rear wheel transmission shafts 89, 89, respectively.

  The operation position of the change lever 90 is reverse speed, neutral, work speed, and road speed in the order of operation from the rear to the front. When the diff lock lever 91 is operated forward, the diff lock is operated, and when operated backward, the diff lock lever 91 is operated.

  Therefore, when performing the rice transplanting work in the field, the diff lock lever 91 is set to the diff lock, the change lever is shifted to the working speed, the seedling is placed on the seedling stage of the rice transplanting device 3, and the fertilizer tank of the fertilizer application device 4 is granular. When the fertilizer is put in and the parts are driven to move forward, the differential lock device F of the left and right rear wheels 7 and 7 is in the state of being differentially locked and the differential function is stopped. Can be done at the same time. In the case of traveling on the road, if both the rear differential device D and the front differential device E are operated in a state in which the differential function works, the vehicle can travel safely.

  Reference numeral 140 denotes a pedal for operating both the main clutch 43 and the left and right rear wheel brake devices J. The pedal 140 is disposed on the lower right side of the steering handle 16. When the pedal 140 is depressed, the main clutch 43 is disengaged, and subsequently the left and right rear wheels. Wheel brake J is applied and the aircraft stops.

Next, the rice transplanter 3 is mounted on the traveling vehicle 1 so as to be movable up and down by the link device 2 for raising and lowering. The configuration for raising and lowering and the configuration of the rice transplanter 3 will be described.
First, the piston upper end portion of a general hydraulic cylinder 160 whose base is rotatably provided on the traveling vehicle 1 is connected to the lifting link device 2, and the solenoid hydraulic valve 161 is connected to the hydraulic pump 13 provided on the traveling vehicle 1. The rice transplanter 3 connected to the lifting / lowering link device 2 is moved up and down by supplying / discharging pressure oil to / from the hydraulic cylinder 160 and extending / retracting the piston of the hydraulic cylinder 160.

  The rice transplanting device 3 is supported by a planting transmission case 162 that also serves as a frame that is freely mounted on the rear of the lifting link device 2 via a rolling shaft, and a support member provided in the planting transmission case 162. A seedling mounting table 163 that reciprocates in the left-right direction of the machine body, and a seedling planting tool 164 that is attached to the rear end of the planting transmission case 162 and divides seedlings one by one from the lower end of the seedling mounting table 163 to be planted in the field. ... and a center float 165, a side float 166, etc., which are leveling bodies whose rear part is pivotally supported at the lower part of the planting transmission case 162 and whose front part is mounted so as to freely swing up and down. The center float 165 and the side float 166 are provided to level the field and level the front of the field where the seedlings are planted by the seedling planting tools 164.

  Reference numeral 167 denotes a PTO transmission shaft having universal joints at both ends, and is provided so as to transmit the power of the fertilization drive case 168 to the planting transmission case 162 of the rice transplanter 3. Reference numeral 169 denotes a center float sensor configured by a potentiometer that detects the vertical position of the front portion of the center float 165, and is linked to the upper surface of the front portion of the center float 165 by a link. Based on the detection of the vertical position of the center float 165 front part of the center float sensor 169, the solenoid hydraulic valve 161 is controlled by the rice transplanter lifting means of the controller 170, and the vertical position of the rice transplanter 3 is controlled by the hydraulic cylinder 160. Is configured to do.

  That is, when the front part of the center float 165 is lifted to an appropriate range or more by an external force, the hydraulic oil pumped out from the transmission case 11 by the hydraulic pump 13 is sent to the hydraulic cylinder 160 to cause the piston to protrude and to move up and down. The device 2 is moved up to raise the rice transplanter 3 to a predetermined position, and when the front part of the center float 165 is lowered beyond the proper range, the pressure oil in the hydraulic cylinder 160 is returned to the mission case 11 for raising and lowering. The link device 2 is moved down to lower the rice transplanter 3 to a predetermined position, and when the front part of the center float 165 is in an appropriate range (when the rice transplanter 3 is in an appropriate predetermined position), the hydraulic cylinder 160 It is provided in order to stop the pressure oil inside and out and to keep the rice transplanter 3 in a fixed position. As described above, the center float 165 is used as a ground sensor for automatic height control of the rice transplanter 3.

  Reference numeral 171 denotes a finger lever disposed below the steering handle 10. When the finger lever 171 is operated in the vertical direction, a finger lever switch 172 constituted by a potentiometer is actuated by the PTO clutch actuating means of the control device 170. The PTO clutch actuating SOL 173 is operated to operate the PTO clutch for connecting / disconnecting the power provided in the fertilizer application case 168 so that the power to the fertilizer application device 4 and the rice transplanting device 3 can be turned on and off. The rice transplanter lifting / lowering means of the control device 170 is configured to operate the solenoid hydraulic valve 161 to manually move the rice transplanter 3 up and down.

  That is, when the finger lever 171 is operated to “up”, the PTO clutch is disengaged, the operations of the fertilizer application device 4 and the rice transplanter 3 are stopped, and the solenoid hydraulic valve 161 is forcibly switched to the side of raising the rice transplanter 3.

  When the finger lever 171 is operated “up” once after the finger lever 171 is operated “up”, the solenoid hydraulic valve 161 is automatically controlled by the vertical movement of the center float 165, and the rice transplanter 3 If the state is raised, the rice transplanter 3 is lowered until the center float 165 comes into contact with the ground and reaches an appropriate posture. When the finger lever 171 is operated to “down” once more, the PTO clutch is engaged and the fertilizer application device 4 and the rice transplanting device 3 are in an automatic control state in which the solenoid hydraulic valve 161 is switched by the vertical movement of the center float 165. Driven. Thereafter, each time the finger lever 171 is operated “down”, the PTO clutch is alternately switched between on and off while the solenoid hydraulic valve 161 remains in the automatic control state where the center hydraulic valve 161 is switched by the vertical movement of the center float 165.

Next, a control configuration for automatically raising the rice transplanter 3 will be described.
First, there is provided a backlift switch 191 that comes into contact with a contact piece 190 provided at the base of the change lever 90 when the change lever 90 is operated to reverse speed. Thus, the solenoid hydraulic valve 161 is controlled so that the rice transplanter 3 is raised to the maximum position by the hydraulic cylinder 160.

  As described above, when the change lever 90 is operated to the reverse speed, the rice transplanter 3 is automatically raised to the maximum position, so that the machine can be used for turning the machine at the edge of the field. When moving backward, the rice transplanter 3 is automatically raised to the maximum position, so that it is possible to prevent the rice transplanter 3 from colliding with the ridge and being damaged, and the workability is good.

  If the auto lift switch 183 is turned ON when the steering handle 16 is rotated 230 degrees to the left or right, the solenoid hydraulic valve 161 is controlled by the rice planting device raising means of the control device 170 and the hydraulic cylinder 160 controls the rice planting device. 3 is raised to the maximum position.

  As described above, when the steering handle 16 is rotated to the left or right as much as possible in order to turn the aircraft at the heel, the auto lift switch 183 is turned on, and the rice transplanter 3 is automatically raised to the maximum position. The operation of raising the rice transplanter 3 at the time of turning the body is not necessary, and the turning of the body can be performed efficiently and the workability is good.

  On the other hand, on the left and right outer sides of the wall surface on the cockpit seat 20 side of the operation panel 17, when the auto lift switch 183 is turned on, the rice transplanter 3 is automatically raised by the rice transplanter raising means of the controller 170 and the auto lift. An autolift changeover switch 192a is provided for switching to a state in which the switch is not automatically raised even when the switch 183 is turned on. Further, on the left and right inner sides of the wall of the operation panel 17 on the side of the cockpit 20, when the back lift switch 191 is turned ON, the rice transplanter 3 is automatically raised by the rice transplanter raising means of the control device 170 and the back lift. A backlift switching switch 192b is provided for switching to a state in which the switch 191 is not automatically raised even when the switch 191 is turned on.

  For example, when going over a ridge to get out of the field, in order to improve the front / rear balance of the aircraft, the rice transplanter 3 is moved down and moved forward while going over the ridge. At that time, the operator further improves the front / rear balance. Next, he leaves the cockpit 20 and stands at the front end of the aircraft to raise the front weight of the aircraft and go over the heel. At this time, when the advancing direction of the airframe has been changed due to the influence of the hail, the operator tries to correct the advancing direction of the airframe by operating the steering handle 16, but at this time, the steering handle 16 If the auto lift switch 183 is turned on by the turning operation and the rice transplanter 3 is automatically raised, there is a risk that the balance of the front and rear of the machine deteriorates and the machine falls. Therefore, by disposing the auto lift changeover switch 192a on the left and right outer sides of the operation panel 17, as described above, the auto lift switch 183 is turned on by the turning operation of the steering handle 16 when the steering wheel is crossed, and the rice transplanter 3 is turned on. When it is going to be automatically raised, the operator can easily switch the automatic lift changeover switch 192a to OFF from the front end of the machine body to stop the automatic raising of the rice transplanter 3, and it is safe to avoid danger.

  In addition, when the autolift changeover switch 192a and the backlift changeover switch 192b are turned off and the backlift switch 191 is turned on or the autolift switch 183 is turned on, the rice transplanter 3 is not automatically raised. Even if the change lever 90 is operated to reverse speed when the machine is moved backward to the barn etc., the rice transplanter 3 does not automatically move up, so the rice transplanter 3 can be lowered while moving backward, and the upper part of the barn entrance or in the barn It is possible to avoid a situation where the rice transplanter 3 is hit against other members. In addition, when planting around a vine in a deformed field such as a fan shape or a gourd type, a planting operation is performed while turning the steering handle 16 along a curved heel. At this time, an autolift changeover switch 192a is used. When the steering wheel 16 is rotated to the left or right by 230 degrees or more, the rice transplanter 3 automatically rises and the planting operation cannot be performed. However, when the auto lift changeover switch 192a is turned off. Even if the steering handle 16 is rotated to the left or right by 230 degrees or more, the rice transplanter 3 does not rise, so that the planting operation can be performed, and the seedling planting operation can be appropriately performed even in the modified farm field.

In the figure, reference numeral 200 denotes a spare seedling stage provided at the front of the machine body, and 201 denotes a center mascot used as an indicator of straight traveling.
FIG. 8 is an overall side view of an eight-row planted rice transplanter showing another example. A frame 10c constituting a frame of the traveling vehicle 1 is extended downward in a U-shape to form a U-shaped portion 10i. Furthermore, the rear end of the U-shaped portion 10i extends to above the body cover 19 that also serves as a step, thereby forming a handrail portion 10j for getting on and off. Note that the rear end portion of the U-shaped portion 10i and the rear frame 10e are connected, and the rear end of the handrail portion 10j is connected to the rear frame.

  A step plate is fixed to the U-shaped portion 10i to form a step 10k for getting on and off. Further, the configuration of the boarding step 10k and the handrail portion 10j is the same on both the left and right sides of the traveling vehicle 1.

  If comprised as mentioned above, since boarding step 10k and handrail part 10j are constituted using a frame of traveling vehicle 1, a strong frame composition is possible with a simple structure, and handrail part 10j Since the structure is provided on the side of the cockpit 20 and in the vicinity of the fertilizer tank 4a and the seedling stage 163 of the fertilizer application apparatus 4, not only a handrail for getting on and off the aircraft, but also fertilizer to the fertilizer tank 4a. It can also be used as a handrail when supplying or supplying seedlings to the seedling stage 163, and is safe and improves workability.

  FIG. 9 is an overall plan view of an 8-row riding rice transplanter showing still another example. FIG. 9A shows an example in which the rice transplanter 3 is mounted on a traveling vehicle 1 of a short wheel base (foil base L1), and FIG. An example in which a rice transplanter 3 is mounted on a traveling vehicle 1 having a long wheel base (wheel base L2, L1 <L2) is shown. Then, the body cover 19 in which the steps are integrally formed is divided into a front cover 19a and a rear cover 19b that forms a step at a high position at the rear of the body. Therefore, in the case of the short foil base of FIG. A, the front cover 19a and the rear cover 19b constitute the fuselage cover 19, and in the case of the long foil base of FIG. B, between the front cover 19a and the rear cover 19b. An airframe cover 19 is configured with an additional step 19c. In this way, a model with different specifications can be produced simply and inexpensively by simply dividing the airframe cover at a step at a high position at the rear of the airframe and adding the additional step 19c.

  Finally, in a configuration in which a line drawing marker is drawn on the left and right sides of the traveling vehicle 1 and the drawing part is automatically moved up and down by an electric motor in the field, when the line drawing marker is not used. Storing along the front-rear direction of the aircraft so that it does not get in the way with the drawing section slightly lowered. Therefore, when the drawing marker is stored, a marker storing switch is provided, and when the switch is pressed, the drawing portion of the left and right drawing marker is automatically set to the storing height, so that the working efficiency is improved. Become.

  The present invention can be applied to various riding seedling transplanting machines such as a riding type vegetable transplanting machine and a riding type grass transplanting machine in addition to the riding type rice transplanting machine, and also to any other traveling vehicle such as a tractor and a construction machine. It may be applied.

DESCRIPTION OF SYMBOLS 1: Passenger type traveling vehicle , 2: Lifting link apparatus, 3: Rice transplanting apparatus , 4: Fertilizer application , 4a: Fertilizer tank , 4c: Blower (electric blower) , 10c: Frame, 10i: U-shaped part, 10j: Handrail for getting on and off, 10k: Step for getting on and off, 12: Engine (water-cooled diesel engine) , 12c: Radiator , 12d: Radiator fan , 19: Airframe cover, 20: Pilot seat, 163: Seedling stage

Claims (4)

In a riding type rice transplanter in which a rice transplanter (3) is mounted on a traveling vehicle (1) through a lifting link device (2), a frame (10c) provided on the traveling vehicle (1) extends downward in a U-shape. A U-shaped portion (10i), and a handrail portion (10j) for getting on and off extending from the U-shaped portion (10i) to above the body cover (19). (10j) is arranged on the side of the cockpit (20) and near the seedling platform (163) of the rice transplanter (3), and the step (10k) for getting on and off is fixed to the U-shaped part (10i). Riding type rice transplanter . A fertilizer tank (4a) of a fertilizer application device (4) is provided at the rear of the machine body. The fertilizer application device (4) feeds the fertilizer in the fertilizer tank (4a) by the feeding device (4b) and is blasted by the blower (4c). The riding type rice transplanter according to claim 1, wherein the handrail portion (10 j) for getting on and off is arranged near the fertilizer tank (4 a) . The riding type rice planting according to claim 2, wherein an engine (12) equipped with a radiator (12c) is mounted on the fuselage, and the blower (4c) sucks air from the rear side in the longitudinal direction of the radiator (12c). Machine. A radiator (12c) is arranged behind the engine (12) mounted in the center of the airframe, and the engine waste hot air is discharged toward the rear of the airframe by the radiator fan (12d). The blower (4c) The riding type rice transplanter according to claim 3, wherein air is sucked from a rear position of 12c).

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