JP2010042031A - Combine - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a combine harvester capable of easily and widely opening an engine and its vicinity. <P>SOLUTION: The combine harvester is provided with an engine hood 23, a driver's seat 11, a driver's platform floor 12, and a steering tower 13, disposed to be integrally rotated around a vertical driving part opening shaft P2 of the machine body positioned at the front side of a self-propelled machine body relative to the engine 21 and at an outer side of the machine body in lateral direction of the machine body relative to the engine 21, so as to be switched between a closed state where the engine 10 is covered with the engine hood 23 and the driver's platform floor 12 positions above a machine frame 2, and an opened state where the engine 21 is opened from the engine hood 23 and the driver's seat 11 and the driver's platform floor 12 positions outside the machine body by plane view of the body. <P>COPYRIGHT: (C)2010,JPO&INPIT

Description

  The present invention relates to a combine equipped with a driver seat positioned above an engine bonnet.

Conventionally, for example, Patent Documents 1 and 2 disclose the above combine.
That is, in Patent Document 1, a driver's seat 12 is mounted on the upper surface of an engine cover 11 (corresponding to an engine bonnet), a handle tower 9 (corresponding to a control tower), step 8 (corresponding to a driver's floor), The cover body A, in which the engine cover 11 and the side plate 14 (corresponding to the side wall) are integrated, is supported by the body frame 34 via the fulcrum bracket 35, and the cover body A is slightly horizontal with the longitudinal fulcrum y of the fulcrum bracket 35 as the center. By swinging outward and swinging upward about the lateral fulcrum x of the fulcrum metal fitting 35, the engine cover 11 and the driver seat 12 are integrally turned up and rotated with respect to the fuselage frame 34, and the engine. 10 is released. At this time, the side plate 14, the step 8, and the handle tower 9 are rotated together with the engine cover 11, and the self-propelled machine body is also opened on the front side of the engine 10.

  In Patent Document 2, the driver's seat 2a is supported by the engine bonnet 9, the engine bonnet 9 is supported by the bonnet support part 50 so that it can be opened and closed freely, and the bonnet support part 50 is located on the front end side of the floor plate 2b of the driver part 2. By being connected to the body frame 4 so as to be rotatable around the pivot axis Y which is vertically below the fuselage, the engine bonnet 9 is released and the bonnet support 50 is pivoted around the pivot axis Y. The engine bonnet 9 and the driver's seat 2a are swung around the turning axis Y to the lateral side of the self-propelled body with respect to the body frame 4, and the engine 8 is opened.

JP 2001-136823 (paragraphs [0041], [0053]-[0055], FIGS. 2, 3 and 7) JP 2004-34780 (paragraphs [0013], [0017], [0018], [0023], FIGS. 11 and 14)

  In the one shown in Patent Document 1, the engine bonnet and the operating unit floor rotate around the axis of the self-propelled machine body sideways. In particular, the front side of the engine is opened upward in a state free of work obstacles. If this is possible, the engine bonnet and the driver's seat need to be raised from a closed state to a high place, and the opening / closing operation tends to be heavy.

  In the thing shown by patent document 2, the driving | operation part floor | floor was not open | released and the self-propelled aircraft body was not able to be open | released in the front side of the engine.

  An object of the present invention is to provide a combine that can easily open not only the engine and the self-propelled aircraft on the front side of the engine at once, but also wide open above them. .

In the first invention, in the combine provided with the driver seat located above the engine bonnet,
The engine bonnet, the driver's seat, the driver's floor and the control tower located in front of the driver's seat, and the lateral side wall that partitions the inside and outside of the driver at the side of the driver's floor, the rear side of the self-propelled aircraft from the engine In addition, the engine bonnet covers the engine and is integrated around the open shaft center of the self-propelled aircraft that is located on the outer side of the self-propelled aircraft in the lateral direction of the self-propelled aircraft from the engine. The closed state with the floor and side walls positioned above the self-propelled aircraft frame, the engine bonnet and the driver's seat open the engine, and the driver's floor, side walls, and control tower are self-propelled in plan view. It is configured to be freely switchable to an open state located outside the machine body.

  In the combine, a grain recovery unit is provided behind the driving unit, and the pre-cutting processing unit is positioned in front of the driving unit. In the first aspect of the invention, the engine bonnet and the like are rotated around the operating unit opening axis to switch to the open state to open the engine, so that the kernel tank of the kernel recovery unit is rotated open. Measures to avoid the interference between the engine bonnet and the grain recovery unit, and the measures to avoid the interference between the engine bonnet and the pre-cutting processing unit, such as rotating and opening the pre-cutting processing unit. Even without that, the engine can be opened by rotating the engine bonnet and the driver seat. In addition, because the engine bonnet and the like are rotated around the driving unit opening axis centering up and down the self-propelled machine body, the arrangement height is the same or almost the same as the arrangement height when the engine bonnet and the operation unit floor are closed. Can be moved to the open state. When the engine bonnet is switched to the open state, the operation part floor, the control tower, and the side wall rotate together with the engine bonnet and are located outside the self-propelled aircraft in the plan view of the self-propelled aircraft. Is released.

  This makes it possible to move the engine bonnet, driver's seat, control tower, driver's floor, and side walls all at once without taking measures to prevent the engine bonnet from interfering with the grain recovery unit and the pre-cutting processing unit. In addition, the engine bonnet and the operation unit floor are moved at the same or substantially the same arrangement height as the arrangement height in the closed state, and the engine and the self-propelled body in front of the engine are moved to the engine bonnet and the operation unit. It can be opened in a state where the floor is located above or the side wall is not left.

  Therefore, according to the first invention, the engine and the self-propelled aircraft in front of the engine can be quickly opened by moving the engine bonnet, the driver's seat, the control tower, the driver's floor, and the side wall all at once. However, the engine and the front side of the engine can be opened to the state where there is no obstacle such as the engine bonnet or the like, or the side wall is not left, so that the inspection work can be performed efficiently. In addition, it is not necessary to take time and effort to avoid interference between the grain recovery unit and the pre-cutting processing unit and the engine bonnet, etc., and the same as the arrangement height when the engine bonnet and the operation unit floor are closed or It is possible to perform the inspection work advantageously from this aspect by moving it while maintaining the almost same arrangement height and opening it easily.

In the second aspect of the invention, in the combine provided with the driver seat located above the engine bonnet,
The engine bonnet, the driver's seat, and the driver's floor located in front of the driver's seat are on the front side of the self-propelled aircraft from the engine and on the outer side of the self-propelled aircraft in the lateral direction of the self-propelled aircraft. A closed state where the engine bonnet covers the engine and the operation part floor is located above the self-propelled machine frame, and the engine bonnet and the driver seat The engine is opened and the operation unit floor is configured to be freely switchable to an open state located outside the self-propelled aircraft in a plan view of the self-propelled aircraft,
The grain tank is supported so as to be freely opened and closed around a tank opening axis centered on the self-propelled machine body arranged on the rear side of the grain tank.

That is, the grain tank is opened around the axis of the tank opening to secure a path for the engine bonnet to move to the front end side of the grain collection unit, and the engine bonnet etc. can rotate without interfering with the grain tank. Then, the engine bonnet, the driver's seat, and the like are rotated around the driving unit opening axis to switch to the open state to open the engine. At this time, the operating unit floor is also opened together with the engine bonnet and is located outside the self-propelled aircraft, and the self-propelled aircraft on the front side of the engine is opened.
As a result, the engine bonnet, the driver's seat, and the driver's floor can be moved all at once and the engine hood, driver's floor, etc. can be moved without taking measures to prevent the engine bonnet from interfering with the pre-cutting processing unit. The engine and the self-propelled aircraft in front of the engine are moved to the state where the engine bonnet and the operation part floor do not exist above by moving with the arrangement height that is the same or almost the same as the arrangement height in the closed state. be able to.

  Therefore, according to the second aspect of the invention, the engine bonnet, the driver's seat, and the driver's floor can be moved all at once to quickly open the engine and the self-propelled aircraft in front of the engine. Inspection work can be efficiently performed by opening the front side of the engine to a state where there are no obstacles such as the engine bonnet or the operating unit floor not being positioned above. Moreover, it is not necessary to take time and effort to avoid interference between the pre-cutting processing unit and the engine bonnet, and the same or almost the same arrangement height as when the engine bonnet and the operation unit floor are closed. It can be moved as it is, and the opening operation can be easily performed, and the inspection work can be advantageously performed from this aspect.

In the third aspect of the invention, in the combine provided with a driver seat located above the engine bonnet,
The engine bonnet, the driver's seat, the driver's floor located in front of the driver's seat, and the control tower are located on the front side of the self-propelled aircraft with respect to the engine and in the lateral direction of the self-propelled aircraft with respect to the engine. A closed state in which the engine bonnet covers the engine and the operation unit floor is located on the upper side of the self-propelled machine frame, integrally with the self-propelled machine vertically oriented driving unit opening shaft core disposed on the side; The driver's seat opens the engine, and the driver's floor is configured to be freely switchable to an open state located outside the self-propelled aircraft in a plan view of the self-propelled aircraft,
The pre-cutting processing unit is supported so as to be openable and closable around a self-propelled machine body up-and-down cutting unit opening axis positioned on the side opposite to the driving unit side of the pre-cutting processing unit.

That is, the cutting pre-processing unit is opened around the cutting unit opening axis to secure a space for accommodating the engine bonnet in front of the driving unit, and the engine bonnet and the driving seat are arranged around the driving unit opening axis. Rotate to switch to the open state and open the engine. At this time, the driving section floor and the control tower are also opened together with the engine bonnet and are located outside the self-propelled aircraft, and the self-propelled aircraft on the front side of the engine is opened.
As a result, the engine bonnet, the driver's seat, the driver's floor, and the control tower can be moved all at once without taking measures to avoid the engine bonnet from interfering with the grain recovery unit. Move the engine and the self-propelled aircraft in front of the engine so that the engine bonnet and the operation part floor are not positioned above the same height as the arrangement height in the closed state. Can be opened.

  Therefore, according to the third aspect of the present invention, the engine bonnet, the driver's seat, the driver's floor, and the control tower can be moved all at once, so that the engine and the self-propelled aircraft in front of the engine can be quickly opened. The engine and the front side of the engine can be opened to a state where there are no obstacles such as the engine bonnet or the operation unit floor not being positioned above, so that inspection work and the like can be performed efficiently. In addition, it is not necessary to take time and effort to avoid interference between the grain collection unit and the engine bonnet, and the arrangement height is the same or almost the same as the arrangement height when the engine bonnet or the operation unit floor is closed. It can be moved as it is, and the opening operation can be easily performed, and the inspection work can be advantageously performed from this aspect.

  In the fourth aspect of the invention, in the configuration of the second or third aspect of the invention, the lateral side wall that partitions the inside and outside of the driving unit on the side of the driving unit floor is supported so as to be rotatable together with the engine bonnet. .

  In other words, when the engine bonnet or the like is switched to the opened state, the lateral side wall also rotates together with the engine bonnet to be in the open state, and the free-running aircraft on the front side of the opened engine remains on the lateral side wall. No open state.

  Therefore, according to the fourth aspect of the present invention, the self-propelled aircraft on the front side of the engine is brought into an open state in which not only the operation unit floor is located above but also the side wall is not present, and the traveling device and the pre-cutting process from the engine. The transmission system that transmits power to the section is released, and it becomes easier to perform work such as inspection and repair of the transmission system.

Combine side view Overall plan view of combine Plan view of the operating section and driving section in partial cross-section Side view of the driving section and driving section with a partial cross-section (A) is a plan view of the driving unit and the driving unit when the engine is closed, and (B) is a plan view of the driving unit and the driving unit when the engine is open. The perspective view in the separation state of the interlocking structure of the main transmission lever and the transmission It is a top view of the combine provided with another implementation structure, (A) is a plan view in the engine closed state of the driving unit and the driving unit, (B) is a plan view in the engine open state of the driving unit and the driving unit Furthermore, it is a top view of the combine provided with another implementation structure, (A) is a plan view in the engine closed state of the driving unit and the driving unit, (B) is a plane in the engine open state of the driving unit and the driving unit Figure Side view of the front part of a combine with a horizontal screw conveyor with another implementation structure Perspective view of hook mounting part of horizontal screw conveyor

Embodiments of the present invention will be described below with reference to the drawings.
[First embodiment]
As shown in FIGS. 1 and 2, a driving unit 10 configured to be self-propelled by a pair of left and right crawler type traveling devices 1 and equipped with a driving seat 11, and an engine 21 arranged below the driving seat 11 are provided. A base end portion of the pretreatment unit frame 31 of the pre-cutting processing unit 30 is rotatably connected to the front part of the body frame 2 of the self-propelled machine body including the prime mover 20 that is equipped. The threshing device 4 disposed on the rear side of the self-propelled machine body is provided on the rear part of the body frame 2, and the grain recovery unit A including the grain tank 5 disposed on the rear side of the self-propelled machine body of the operation unit 10 is disposed on the body frame 2. The combine is constituted.

  This combine harvests rice, wheat, soybeans, and the like. When an elevating cylinder (not shown) linked to the pretreatment unit frame 31 is operated, the elevating cylinder moves the pretreatment unit frame 31 to the body frame 2. The lowering operation state in which the pre-cutting processing unit 30 is raised and the lower end portion of the device 32 is positioned near the ground, and the raising device 32 and the like are raised from the ground. Move up and down to a non-working state. When the pre-cutting processing unit 30 is in the descending work state and the self-propelled machine body travels, the pre-cutting processing unit 30 causes the plurality of pulling devices 32 arranged in the lateral direction of the self-propelled machine body to cause and process the planted culm. The planted side of the planted culm is cut by the clipper-shaped reaping device 33, and the reaped cereal from the reaping device 33 is conveyed backward by the feeding device 34 and supplied to the threshing device 4. . The threshing device 4 performs the threshing process by supplying the tip side to the handling room (not shown) while holding and conveying the stock side of the harvested cereal rice cake in the rear direction of the self-propelled machine body by the threshing feed chain (not shown). The grain collection unit A collects and stores the threshing grains from the threshing device 4 in the grain tank 5, and the threshing grains stored in the grain tank 5 are located in the bottom of the grain tank 5. Grain by a bottom screw 6, a vertical screw conveyor 7 that is located on the rear side of the grain tank 5, and a vertical screw conveyor 7 that is vertically movable, and a horizontal screw conveyor 8 that is connected to the upper end of the vertical screw conveyor 7 so as to be swiveled and vertically driven. It is designed to be taken out from the tank 5.

  As shown in FIGS. 3 and 4, the engine bonnet 23 that covers the engine 21, the engine cooling radiator 22 positioned on the laterally outer side of the engine 21, etc. An air intake case 24 provided on the upper surface of the top plate 23a is provided.

  As shown in FIGS. 3 and 4, the engine bonnet 23 includes a front wall 23 b located on the front side of the self-propelled aircraft body of the engine 21, a rear wall 23 c located on the rear side of the self-propelled aircraft body of the engine 21, and a self-propelled aircraft body of the engine 21. A lateral wall 23e positioned on the lateral outer side and the top plate 23a positioned above the engine 21 are provided.

  Self-propelled aircraft lateral direction so that the output of the engine 21 is transmitted to the traveling mission (not shown), the pre-cutting processing unit 30, and the threshing device 4 inside the self-propelled aircraft body in the lateral direction of the engine bonnet 23. A transmission opening 25 facing inward of the machine body is provided. The lateral wall 23e of the engine bonnet 23 has a dust-removing net with a self-propelled laterally-facing air intake 26, a blower 27 for supplying cooling air to the engine cooling radiator 22, the air intake 26, and the air intake case 24. Is provided with an internal space S <b> 1 that communicates the inside thereof with the air blowing port 27. The front wall 23b of the engine bonnet 23 is provided with a front-facing air intake 28 with a dust removal net and an internal space S2 that connects the air intake 28 to the internal space S1 of the lateral wall 23e.

  As shown in FIGS. 1 to 4, the driving unit 10 is disposed above the engine bonnet 23 and supported by the top plate 23 a of the engine bonnet 23, in front of the driving seat 11, and in the engine. Driving section floor 12 disposed in front of front wall 23b of bonnet 23, control tower 13 disposed in front of driving seat 11 and at the front end of driving section floor 12, opposite to the entrance side of driving section floor 12 The side wall 14 provided to partition the inside and outside of the driving unit 10 between the engine bonnet 23 and the control tower 13 and the side side of the driver seat 11 on the side where the side wall 14 is located. A horizontal operation panel 15 is provided.

  The control tower 13 is provided with a steering lever 16, and the lateral operation panel 15 is provided with a main transmission lever 17, a sub transmission lever 18, and a clutch lever 19. The steering lever 16 performs a steering operation of the self-propelled aircraft by swinging in the lateral direction of the self-propelled aircraft and shifting and stopping the left and right crawler traveling devices 1 separately. This steering lever 16 is also used as a lever for raising and lowering the pre-cutting processing unit 30, and the raising and lowering cylinder can be operated by swinging in the front-rear direction of the self-propelled machine body. The main speed change lever 17 performs forward / reverse switching, stepless speed change, and stop operation of the left and right traveling devices 1. The auxiliary transmission lever 18 is used for auxiliary transmission of the left and right crawler traveling devices 1 between a low speed state and a high speed state. The clutch lever 19 switches between a cutting clutch (not shown) for turning on and off the cutting pretreatment unit 30 and a threshing clutch (not shown) for turning on and off the threshing device 4.

  The engine bonnet 23, the operation unit floor 12, the control tower 13, the lateral side wall 14, and the lateral operation panel 15 are supported by one operation unit frame F, and the operation unit frame F is from the engine 21. The self-propelled aircraft up-and-down direction driving unit arranged on the front side of the self-propelled aircraft rather than the grain tank 5 on the rear side of the self-propelled aircraft and on the outer side of the self-propelled aircraft in the lateral direction of the self-propelled aircraft. It is supported by the body frame 2 so as to be rotatable around the open shaft core P1. The driver's seat 11 is supported by the top plate 23a of the engine bonnet 23, and the engine hood 23, the driver's seat 11, the driver's floor 12, the control tower 13, the side wall 14, and the lateral operation panel 15 are integrally opened. It is supported so as to rotate with respect to the body frame 2 around the axis P1, and as shown in FIG. 6 (a), the closed state located in the driving unit 20 and the operating unit 10 on the upper side of the body frame 2, and FIG. As shown in (b), it can be switched to the open state located on the side of the grain tank 5 as the outside of the self-propelled machine body in plan view.

  That is, at the normal time such as working or traveling, the driving unit frame F is closed and rotated around the driving unit opening axis P1 on the inner side of the machine body. Then, the engine bonnet 23 and the like are in the closed state, the engine 21 and the engine cooling radiator 22 are covered with the engine bonnet 23, and the driver seat 11 is supported forward on the engine bonnet 23. Become. The driver's floor 12 and the control tower 13 are in front of the driver's seat 11 on the upper side of the fuselage frame 2, the lateral wall 14 is on the lateral side of the driver's floor 12 on the upper side of the fuselage frame 2, and the lateral operation panel 15 is in the fuselage. It will be in the state located in the side of the driver's seat 11 of the upper side of the flame | frame 2, respectively, and it will be possible to board the driver | operator 10 and to drive | operate and operate the self-propelled machine body and the cutting pre-processing part 30.

  When performing management or repair work such as inspecting the engine 21, the operating unit frame F is opened and rotated 90 degrees or more from the closed position around the operating unit opening axis P1 to the lateral side of the self-propelled machine body. Then, the engine bonnet 23 moves to the outside of the body without hitting the engine 21 due to the transmission opening 25 and the engine passage hole 29 (see FIG. 3) of the rear wall 23c, and the engine bonnet 23 and the like are in the open state. Thus, the engine bonnet 23 and the driver's seat 11 open the engine 21 and the engine cooling radiator 22 to facilitate inspection and repair of the engine accessory device such as the engine 21 and the engine cooling radiator 22. In addition, the driving unit floor 12, the control tower 13, the side wall 14, and the horizontal operation panel 15 are in a state in which the self-propelled machine body in the vicinity of the engine is opened, and the driving power is transmitted from the engine 21 to the traveling device 1 and the pre-cutting processing unit 30. It becomes easy to inspect and repair the transmission system and the like from the front side of the engine 21.

  The steering lever 16, the auxiliary transmission lever 18, and the clutch lever 19 are attached to the steering tower 13 and the side operation panel 15 when the engine bonnet 23 and the like are opened and closed. The steering clutch, the sub-transmission device, and each clutch are linked via an operation cable (not shown) so that it is not necessary to cut off the linkage with the transmission and each clutch.

  As shown in FIG. 6, the main transmission lever 17 and the operation shaft 40 a of the traveling transmission 40 that is a hydrostatic continuously variable transmission are provided with a swing arm 41 attached to the main transmission lever 17. The lever-side interlocking mechanism LR and the transmission-side interlocking mechanism HR including an operation arm 50 attached to the operation shaft 40a of the travel transmission 40 are configured to be interlocked.

  The lever-side interlocking mechanism LR is provided on the swinging arm 41 connected to the base portion 17a of the main transmission lever 17 so as to be integrally rotatable, and on the self-propelled aircraft body whose upper end is connected to the swinging arm 41 so as to be relatively rotatable. A downwardly linked interlocking rod 42, a first swinging link 44 interlocked to the lower end portion of the interlocking rod 42 via a connecting pin 43, and a rotation support shaft 45 of the first swinging link 44 are connected to be rotatable together. A second swing link 46 is provided.

  The transmission-side interlocking mechanism HR includes the operation arm 50 connected to the operation shaft 40a of the traveling transmission 40 so as to be integrally rotatable, and an interlocking rod 51 whose one end is connected to the operation arm 50 so as to be relatively rotatable. A rocking link 52 in which the other end side of the interlocking rod 51 is connected so as to be relatively rotatable, an interlocking rod 53 whose one end is connected to the rocking link 52 so as to be relatively rotatable, and the other end of the interlocking rod 53. The first oscillating link 54 whose front end portion is connected to be rotatable is provided, and the second oscillating link 56 is connected to the rotation support shaft 55 of the first oscillating link 54 so as to be integrally rotatable. It is.

  The lever-side interlocking mechanism LR is supported by the operating unit frame F and the like so as to move on a structure including the engine bonnet 23 and the like when the lateral operation panel 15 is opened and closed together with the engine bonnet 23 and the like. The transmission side interlocking mechanism HR is supported by the body frame 2. As a result, when the lateral operation panel 15 is opened and closed together with the engine bonnet 23 and the like, the interlocking pin 47 provided on the second swinging link 46 of the lever side interlocking mechanism LR causes the second swinging of the transmission side interlocking mechanism HR. Both second swings so that the swinging force of the second swing link 46 is transmitted to the second swing link 56 via the interlocking pin 47 by engaging with the notch 57 provided in the motion link 56. The links 46 and 56 are configured to be switched to the interlocked state, or the interlocking pin 47 is detached from the notch portion 57, so that the second swing links 46 and 56 are switched to the separated state. .

  That is, when the engine bonnet 23 or the like is switched to the open state, the main transmission lever 17 and the travel transmission device 40 are automatically disconnected between the second swing links 46 and 56, and the main transmission lever 17. When the engine bonnet 23 and the like are returned to the closed state, the main transmission lever 17 automatically returns to the state interlocked with the travel transmission device 40.

As shown in FIG. 1, an inclined bottom portion 8 c that is inclined in a state that becomes lower from the conveyance start end side to the discharge cylinder 8 b in a state where the horizontal screw shaft core 8 a is horizontal in the conveyance cylinder of the horizontal screw conveyor 8. It is provided.
That is, soybeans can roll along the inclined bottom portion 8c and easily move to the discharge cylinder 8b, and can be discharged even if the screw pitch of the horizontal screw 8d is increased, and the conveying effect of the horizontal screw 8d on the soybean is small. This makes it possible to transport soybeans while preventing them from being damaged.

[Second Embodiment]
FIG. 7 shows a combine having another embodiment structure. In this combine, the support structure of the grain tank 5 and the support structure of the structure of the operation unit 10 are the same as those of the combine of the first embodiment. It has a different implementation structure.

  That is, the engine bonnet 23, the operation unit floor 12, the control tower 13, the lateral side wall 14, and the lateral operation panel 15 are supported by one operation unit frame F. The operation unit frame F is a self-propelled machine body than the engine 21. It is supported by the body frame 2 so as to be rotatable around a driving unit opening axis P2 which is disposed on the front side and on the outer side of the self-propelled aircraft in the lateral direction of the self-propelled aircraft with respect to the engine 21. ing.

  The grain tank 5 opens and closes around a tank opening axis T that is vertically oriented on the self-propelled machine body and is arranged on the rear side of the grain tank 5 so as to be the same axis as the screw axis of the vertical screw conveyor 7. It is supported by the body frame 2 so as to freely rotate together with the vertical screw conveyor 7.

That is, during normal times such as working or traveling, as shown in FIG. 7 (a), the operating unit frame F is closed and rotated around the operating unit opening axis P2 to the inside of the machine body. Then, the engine bonnet 23, the driver's seat 11, the driver's floor 12, the control tower 13, the lateral side wall 14, and the lateral operation panel 15 are in a closed state located in the driving section 20 and the driver 10 on the upper side of the fuselage frame 2. 21 and the engine cooling radiator 22 are covered with the engine bonnet 23, and the driver's seat 11 is supported forward on the engine bonnet 23. The driver's floor 12 and the control tower 13 are in front of the driver's seat 11 on the upper side of the fuselage frame 2, the lateral wall 14 is on the lateral side of the driver's floor 12 on the upper side of the fuselage frame 2, and the lateral operation panel 15 is in the fuselage. It will be in the state located in the side of the driver's seat 11 of the upper side of the flame | frame 2, respectively, and it will be possible to board the driver | operator 10 and to drive | operate and operate the self-propelled machine body and the cutting pre-processing part 30.
At this time, the grain tank 5 is rotated around the tank opening axis T toward the inner side of the self-propelled machine, and the front and rear direction of the grain tank 5 is self-propelled on the side of the threshing device 4 behind the operation unit 10. Keep the aircraft in the closed position, facing forwards and backwards.

  When carrying out management and repair work such as inspecting the engine 21, as shown in FIG. 7 (b), the grain tank 5 is rotated from the closed state around the tank opening axis T to the lateral side of the self-propelled machine body. The front end side of the grain tank 5 is in the open state located on the lateral outer side of the self-propelled machine body, thereby securing a space for the engine bonnet 23 and the like to move to the front end part of the grain recovery part A, and driving the operating part frame F Around the part rotation axis P2, it is opened and rotated about 90 degrees from the closed position to the laterally outward side of the self-propelled aircraft. Then, the engine bonnet 23 does not hit the engine 21 due to the transmission opening 25 and moves to the outside of the aircraft body, and the engine bonnet 23 and the driver seat 11 are outside the self-propelled aircraft body in a plan view of the self-propelled aircraft. As a result, the engine 21 and the engine cooling radiator 22 are opened, and the engine accessory devices such as the engine 21 and the engine cooling radiator 22 are easily inspected and repaired. In addition, the driving unit floor 12, the control tower 13, the side wall 14, and the horizontal operation panel 15 are also opened together with the engine bonnet 23 and located outside the driving unit 10 as the outside of the driving unit in a plan view of the driving unit. Thus, it is easy to inspect and repair the transmission system that transmits power from the engine 21 to the traveling device 1 and the pre-cutting processing unit 30 from the front side of the engine 21 in the vicinity of the engine.

[Third embodiment]
FIG. 8 shows a combine equipped with yet another implementation structure. In this combine, the first and second implementations of the support structure for the pre-cutting processing unit 30 and the support structure for the structure of the operating unit 10 are shown. It has an implementation structure different from that of the example combine.

  That is, the engine bonnet 23, the operation unit floor 12, the control tower 13, the lateral side wall 14, and the horizontal operation panel 15 are supported by one operation unit frame F. The operation unit frame F is a self-propelled machine body than the engine 21. It is supported by the body frame 2 so as to be rotatable around a driving unit opening axis P3 which is disposed on the front side and on the side of the self-propelled aircraft in the lateral direction of the self-propelled aircraft relative to the engine 21. ing.

  The pre-cutting processing unit 30 is arranged on the same side as the transmission shaft located at the horizontal end of the transmission case 35 on the side opposite to the horizontal end on the driving side of the pre-cutting processing unit 30. Is supported by the body frame 2 so as to be able to open and close and rotate about a cutting part opening axis K that is vertically oriented.

That is, during normal times such as working or traveling, as shown in FIG. 8 (a), the operating unit frame F is closed and rotated around the operating unit opening axis P3 to the inside of the machine body. Then, the engine bonnet 23, the driver's seat 11, the driver's floor 12, the control tower 13, the lateral side wall 14, and the lateral operation panel 15 are in a closed state located in the driving section 20 and the driver 10 on the upper side of the fuselage frame 2. 21 and the engine cooling radiator 22 are covered with the engine bonnet 23, and the driver's seat 11 is supported forward on the engine bonnet 23. The driver's floor 12 and the control tower 13 are in front of the driver's seat 11 on the upper side of the fuselage frame 2, the lateral side wall 14 is on the lateral side of the driver's floor 10 on the upper side of the fuselage frame 2, and the horizontal operation panel 15 is in the fuselage. It will be in the state located in the side of the driver's seat 11 of the upper side of the flame | frame 2, respectively, and it will be possible to board the driver | operator 10 and to drive | operate and operate the self-propelled machine body and the cutting pre-processing part 30.
At this time, the pre-cutting processing unit 30 is rotated to the rear side of the self-propelled machine body around the cutting unit opening axis K, and the closed state in which the free end 30a of the pre-cutting processing unit 30 is located near the front of the operating unit 10 Keep it.

  When performing management and repair work such as inspecting the engine 21, as shown in FIG. 8 (b), the pre-cutting processing unit 30 is rotated around the pre-processing unit opening axis K to the front side of the self-propelled machine body. The free end portion 30a of the pre-cutting processing unit 30 is opened away from the driving unit 10, thereby ensuring a space where the engine bonnet 23 and the like is located on the front side of the driving unit 10 of the driving unit 10, and the driving unit frame F. About 90 degrees of the self-propelled aircraft body is opened and rotated from the closed position around the driving unit rotation axis P3. Then, the engine bonnet 23 does not hit the engine 23 due to the transmission opening 25 and moves to the outer side of the body, and the engine bonnet 23 and the driver seat 11 are outside the self-propelled body in a plan view of the self-propelled body. The engine 21 and the engine cooling radiator 22 are opened in the open state located on the front side, and it becomes easy to inspect and repair the engine accessory devices such as the engine 21 and the engine cooling radiator 21. In addition, the driving unit floor 12, the control tower 13, the side wall 14, and the horizontal operation panel 15 are also in an open state that is located on the front side of the driving unit 10 as the outside of the self-propelled aircraft in plan view with the engine bonnet 23. It is easy to inspect and repair the transmission system that transmits power from the engine 21 to the traveling device 1 and the pre-cutting processing unit 30 from the front side of the engine 21 by opening the self-propelled body in the vicinity of the engine.

[Fourth embodiment]
FIG. 9 shows a combine having a further embodiment. In this combine, a hook 60 is provided on the front end side of the transverse screw conveyor 8.

  The hook 60 suspends and supports the structure including the engine bonnet 23 when the engine bonnet 23 is opened and closed, and reduces the load applied to the operating unit frame F due to the weight of the engine bonnet 23 and the like. While opening and closing. As shown in FIG. 10, the hook 60 is supported by a support rail 62 of the horizontal screw conveyor 8 through a bearing 61 provided at the base of the hook 60 so that the position of the hook 60 can be adjusted. When the opening and closing operation is performed, the position can be changed to the front end side of the horizontal screw conveyor 8 than when the engine bonnet 23 is suspended and supported, and the suspension can be used for the suspension support of the pre-cutting processing unit 30. .

[Another Example]
In the case of a combine equipped with a driving cabin, the lateral wall of the driving cabin is provided as the lateral side wall 14, and the front side wall with an operation panel of the driving cabin is provided as the control tower 13, and the present invention is provided with a driving cabin. It can also be applied to a combine.

2 Machine frame 5 Grain tank 11 Driver's seat 12 Driver's part floor 13 Control tower 14 Side wall 21 Engine 23 Engine bonnet 30 Cutting pretreatment part P2, P3 Driving part open shaft T Tank open shaft core K Cutting part open shaft core

Claims (4)

A combine with a driver seat located above the engine bonnet,
The engine bonnet, the driver's seat, the driver's floor located in front of the driver's seat and the control tower are located on the front side of the self-propelled aircraft from the engine and outside the self-propelled aircraft in the lateral direction of the self-propelled aircraft. Closed state where the engine bonnet covers the engine and the driving part floor is located above the fuselage frame, integrally around the driving part opening shaft core facing the up and down side of the self-propelling machine located on the side or the side of the self-propelled machine And the engine bonnet and the driver's seat open the engine, and the combiner is configured to be freely switchable to an open state in which the driver's floor is located outside the self-propelled aircraft in plan view. The engine bonnet, the driver's seat, the driver's part floor, and the control tower are arranged on the outer side of the self-propelled machine body in the vertical direction of the self-propelled machine body arranged in the lateral direction of the self-propelled machine body from the engine. Integrally configured to be freely switchable between the closed state and the open state,
The combine according to claim 1, wherein the grain tank is supported so as to be freely opened and closed around a tank opening axis centering on a self-propelled machine body arranged on the rear side of the grain tank. The engine bonnet, the driver's seat, the driver's floor, and the control tower are arranged on the side of the self-propelled aircraft in the direction of the self-propelled aircraft in the lateral direction of the self-propelled aircraft from the engine. Integrally configured to be freely switchable between the closed state and the open state,
The combine according to claim 1, wherein the pre-cutting processing unit is supported so as to be openable and closable around a self-propelled machine body up-and-down mowing unit opening axis positioned on the side opposite to the driving unit side of the pre-cutting processing unit.   The combine as described in any one of Claims 1-3 with which the side wall which partitions off the inside and outside of a driving | running | working part by the side of the said driving | running | working part floor is supported by the said engine bonnet so that rotation is possible.

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