JP2010124751A - Steering part structure of riding type implement - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To make it easy for performing maintenance by easily releasing the upper part of an engine of a riding type implement. <P>SOLUTION: The steering part structure of the riding type implement is provided by installing a steering part frame (5) supporting the steering part (20) consisting of a riding step (1), steering panels (2, 4) and an engine cover (3), pivoting the one end of a first supporting arm (6) at the first vertical shaft (9) installed at the position of more inside of the machine body than the right outside end part of a machine body frame (8), pivoting the second vertical shaft (10) installed at the left frontal part of the steering frame (5) at the other end of the first supporting arm (6), pivoting the one end of a second supporting arm (7) at the third vertical shaft (11) installed at the right side end part of the machine body frame (8) and pivoting the fourth vertical shaft (12) installed at the right and left middle part of frontal part of the steering frame (5) at the other end of the second supporting arm (7). <P>COPYRIGHT: (C)2010,JPO&INPIT

Description

  The present invention relates to a control unit structure of a riding-type work machine such as a combine or various harvesters.

  The combine which is a riding type work machine is provided with a riding step on which the operator gets on the right front of the fuselage, a steering part is provided on the front side of this riding step, and the upper part of the engine arranged behind the riding step is covered with an engine cover, It has an arrangement configuration in which a control seat is provided on the engine cover.

  In order to facilitate the maintenance of the engine, a control unit frame in which the riding step, the control unit, and the engine cover are integrally assembled is raised forward about the front pivot shaft, or provided at the right rear portion of the control unit frame. The upper part of the engine is released by rotating rightward about the vertical axis.

For example, in Japanese Patent Application Laid-Open No. 2007-37460, a control unit frame in which a riding step, a control unit, an engine cover, and the like are integrated is arranged in an up-down direction in which the combiner unit is arranged on the outer side of the combine unit in the lateral direction of the combine unit. A configuration is described in which the upper part of the engine can be released by rotating to the side around the shaft core.
JP 2007-37460 A

  The above engine release structure is supported by a single point for the structure that supports the control unit frame that integrates the riding step, control unit, engine cover, etc., with a single vertical support shaft provided on the body frame. Therefore, the control unit frame must be made strong and heavy. In addition, since the combine has a Glen tank that temporarily stores the harvested grains behind the engine, the pivot shaft is placed on the outside of the aircraft frame to release the upper part of the engine while avoiding this grain tank. Therefore, the width of the fuselage is increased.

  Therefore, in the present invention, a riding-type working machine in which a control unit is erected in front of the riding step and an engine is disposed behind the riding step, and the configuration in which the upper part of the engine is released to facilitate maintenance work is relatively. It is a problem to enable easy release operation with a simple configuration.

The above object of the present invention is achieved by the following configuration.
That is, a steering unit frame (5) that integrally supports a steering unit (20) including a riding step (1), a front operation panel (2), a side operation panel (4), and an engine cover (3) is provided. A first support arm (6) and a second support arm (7) for supporting the control unit frame (5) on the side of the body frame (8) are provided, and one end of the first support arm (6) is connected to the body frame (8). ) Is pivotally supported by a first vertical axis (9) provided at a position on the inner side of the airframe from the right outer end, and is provided at the left front of the control unit frame (5) at the other end of the first support arm (6). The second vertical axis (10) is pivotally supported, and one end of the second support arm (7) is pivotally supported on the third vertical axis (11) provided at the right end of the body frame (8). A fourth vertical axis (12) provided at the other end of the two support arms (7) at the middle in the left-right direction of the front part of the control unit frame (5) Pivoted, and a steering unit structure of riding working machine, characterized in that the movable structure to the right of the steering unit frame (5) a body frame (8).

  With this configuration, the control unit frame (5) is firmly supported by the body frame (8) by the two support arms of the first support arm (6) and the second support arm (7), and the control unit frame (5 ) Can be moved to the outside of the body frame (8), and the upper part of the engine is widely released.

  According to the present invention, the control unit frame (5) is firmly supported by the first support arm (6) and the second support arm (7), and the engine cover (3) covering the upper part of the engine is the control unit frame (5). At the same time, the engine frame (8) can be moved to the right side so that the engine can be widely opened, so that the engine and the power transmission mechanism around the engine can be easily maintained.

Next, embodiments of the present invention will be described with reference to the drawings.
In the present specification, the left side and the right side refer to directions when the combine is directed in the forward direction.

  FIG. 1 is a plan view of a combine. A control section comprising an engine cover 3 provided with a riding step 1 on which the operator gets on the right side of the airframe, a front operation panel 2 that erects a steering lever 18, a side operation panel 4 that erects a shift lever 19, and a cockpit 24. 20 and a cabin 27 is provided so as to cover the control unit 20. A grain tank 21 for storing harvested grains is provided on the rear side of the control unit 20, and a grain discharge auger 23 is provided so as to be able to undulate while being connected to a milled cylinder 22 raised from the rear part of the grain tank 21. An engine 25 is mounted at the bottom of the control unit 20.

  As shown in FIGS. 2 and 3, the control unit 20 including the riding step 1, the front operation panel 2, the side operation panel 4, and the engine cover 3 is provided on a control unit frame 5 assembled in a square shape. In addition, an auxiliary step 36 used when riding on the riding step 1 is attached to the control unit frame 5 so that it can be used even when the control unit frame 5 is pulled out to the side. ing. The auxiliary step 36 can be in a state of projecting to the side and a state of folding upward.

  The control unit frame 5 is provided with a fourth vertical axis 12 at a substantially horizontal center position on the front side of the control unit 20, and the fourth vertical axis 12 and a third vertical axis 11 provided at the right end of the body frame 8 are L-shaped. The second vertical axis 10 is provided at the front part of the left side of the control unit frame 5, and the second vertical axis 10 and the third vertical axis 11 of the body frame 8 are connected. A first vertical axis 9 provided at a position inside the machine body is connected by an L-shaped first support arm 6. The second support arm 7 is provided with a receiving roller 26 that receives the lower surface of the control unit frame 5.

  The control unit frame 5 is fixed at a normal position on the fuselage frame 8 and the combine is used. However, when maintaining the engine and its surroundings, the control unit frame 5 is released and moved laterally to the right. To do. The lateral movement of the control unit frame 5 is temporarily stopped at a position where it does not come into contact with the Glen tank 21, and after moving the Glen tank 21 to the side, it can be moved further outward.

  As shown in FIGS. 6 and 7, the traveling speed change lever 19 provided on the side operation panel 4 is attached so that its base portion is pivoted back and forth on the pivoting plate 42 of the wet oil disk 37. Then, the movement of the rotating plate 42 is detected by the first potentiometer 38 and the second potentiometer 39, and the detection signal is sent to the controller to shift the hydraulic transmission. The wet oil disc 37 is configured so that the rotation resistance can be changed to the traveling speed change lever 19, and the rotation resistance can be increased by lubricating the oil hole 45 from the cockpit 24 side and tightening the adjustment nut 44. . In addition, the mounting bracket 40 to which the wet oil disc 37 is attached is attached to the lower mounting surface 41 of the side operation panel 4 with the bolt 43 just by providing a slit for projecting the rotating plate 42 on the mounting upper surface. There are few openings, and dust does not enter the wet oil disk 37, the first potentiometer 38, and the second potentiometer 39. Further, since the first potentiometer 38 and the second potentiometer 39 are attached to the side operation panel 4 after being attached to the mounting bracket 40 together with the wet oil disk 37, sensor adjustment and signal check can be performed before attaching to the side operation panel 4. It is.

  In this way, the steering operation tool such as the travel shift lever 19 provided on the side operation panel 4 is connected to the operation target by the communication cable, so that the control unit frame 5 remains attached to the control unit frame 5. 5 can be pulled to the side without any trouble.

FIG. 8 shows an attachment configuration of the parking brake pedal 48.
A parking brake pedal 48 is pivotally supported by a parking pedal shaft 49 on an auxiliary step 47 attached to the body frame 8 side, and a rear end of the parking brake pedal 48 is connected to a brake drum 46 of a transmission case 57 by a brake rod 50 and a tension spring 55. The brake is connected to the brake arm 56, and the parking brake is activated when the front side of the parking brake pedal 48 is depressed.

  A hook 53 is provided downward in the front and rear intermediate portion of the parking brake pedal 48. The hook 53 and the unlocking piece 51 pivotally supported at the tip of the parking brake pedal 48 are connected by a release rod 52, and the parking brake pedal 48 is depressed. And the hook 53 engages with the pin 54 of the auxiliary step 47 to maintain the depressed state and maintain the parking brake action. Then, when the unlocking piece 51 is stepped on, the hook 53 is detached from the pin 54 and the parking brake pedal 48 is returned to the original state to release the parking brake. Since the parking brake pedal 48 is attached to the body frame 8 side, the parking brake pedal 48 remains in the same position even if the control unit frame 5 is moved outward.

  The control unit frame 5 is normally fixed and used at the position shown in FIG. 2. However, during maintenance work, the front side of the control unit frame 5 is large and the rear side is rotated small as shown in FIG. The upper part of the body frame 8 is released. In a state where the control unit frame 5 is pulled out to the side, the second support arm 7 fits in the lower part of the control unit frame 5 and does not protrude to the side, so that the maintenance work is not disturbed.

  The side pull-out position of the control unit frame 5 is temporarily stopped at the first pull-out position where it does not come into contact with the normal position of the Glen tank 21. The second pull-out is further extended to the side by releasing the Glen tank 21 to the side. It can be fixed in position.

  The engine 25 is mounted on the released body frame 8 side, and the upper part of the radiator 14 is also released. When the engine 25 is lowered from the body frame 8, the control unit frame 5 is placed on and supported by a separately prepared support base, and after removing the first support arm 6, the engine 25 is suspended by a crane.

  Further, since the auxiliary frame 29 to which the hydraulic block 28 is attached on the right front side of the machine body frame 8 can be removed, the work can be facilitated if it is removed during maintenance around the engine 25. Since the fuel filter 32, the suction filter 33, the HST suction filter 34, and the HST line filter 35 are centrally arranged in the airframe frame 8 in front of the auxiliary frame 29, these maintenance operations are also performed laterally. It is easy to pull out.

  Further, when the control unit frame 5 is pulled out to the side, the air cleaner 30 at the top of the engine 25 and the electrical component storage chamber 31 provided at the front side are exposed, so that the engine and other automatic control controllers and the like are inspected.・ Repair becomes easy. Since the electrical component storage chamber 31 has a wide space, electrical components can be arranged in a concentrated manner, and the cockpit 24 provided in the engine cover 3 with the control unit frame 5 fixed at a predetermined position. You can check from the rear inspection window.

  FIG. 9 shows the rear part of the fuselage frame 8, and the left and right side frames 60, 61 of the fuselage frame 8 are connected to provide a first rear frame 62 and a second rear frame 63. The first rear frame 62 and the second rear frame A fuel tank 64 and an auxiliary fuel tank 65 are provided between the frames 63, and the first rear frame 62 and the second rear frame 63 are connected by a connecting frame 67, and an auger metal 66 of the milling cylinder 22 is attached.

  Since the second rear frame 63 is located below the bottom surfaces of the fuel tank 64 and the auxiliary fuel tank 65, the rear portion of the fuel tank 64 and the auxiliary fuel tank 65 is prevented from directly colliding with or colliding with the ground. To prevent it.

FIGS. 10 and 11 show a reinforcing structure of a portion where the machine body frame 8 and the crawler frame 70 of the crawler traveling device 69 are connected by the pitching metal 71.
The left and right side frames 60 and 61 of the body frame 8 are connected by a horizontal frame 72, and a metal mounting plate 74 positioned on the lower surface of the left and right side frames 60 and 61 is connected to the horizontal frame 72 and the left and right side frames inside the left and right side frames 60 and 61. It connects with the reinforcement member 73 connected integrally to 60,61.

  With this configuration, the left and right side frames 60 and 61, the horizontal frame 72, and the metal mounting plate 74 are firmly connected by the reinforcing member 73, and become strong against the lateral load during turning.

It is a top view which shows the whole combine of this invention Example. It is a partial enlarged plan view. It is the enlarged plan view which moved the control part frame. It is a partial enlarged left side view. It is a partial enlarged front view. It is a partial enlarged right side view. It is a partial enlarged front sectional view. It is a partial enlarged left side sectional view. FIG. It is a partial enlarged front sectional view. It is a partial enlarged right side view.

Explanation of symbols

DESCRIPTION OF SYMBOLS 1 Riding step 2 Front operation panel 3 Engine cover 4 Side operation panel 5 Steering part frame 6 First support arm 7 Second support arm 8 Airframe frame 9 First vertical axis 10 Second vertical axis 11 Third vertical axis 12 Fourth vertical Axis 20 Pilot section 24 Pilot seat

Claims (1)

A steering unit frame (5) that integrally supports a steering unit (20) including a riding step (1), a front operation panel (2), a side operation panel (4), and an engine cover (3) is provided. A first support arm (6) and a second support arm (7) for supporting the part frame (5) on the side of the body frame (8) are provided, and one end of the first support arm (6) is attached to the body frame (8). A first longitudinal axis (9) provided at a position on the inner side of the airframe from the right outer end and a second support provided at the left front portion of the control unit frame (5) at the other end of the first support arm (6). The second longitudinal axis (10) is pivotally supported, and one end of the second support arm (7) is pivotally supported on the third longitudinal axis (11) provided at the right end of the body frame (8). The other end of the arm (7) is pivotally supported by a fourth vertical axis (12) provided at the middle in the left-right direction of the front part of the control unit frame (5), Maneuverable part structure of riding working machine, characterized in that the movable structure to the right of the vertical section frame (5) a body frame (8).

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