JPS61111621A - Driver seat of combine - Google Patents

Abstract

(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

[Detailed description of the invention] Industrial applications The present invention relates to a cockpit for a combine harvester.

Problems to be Solved by the Invention In a combine harvester that is powered by an engine and reaps and threshes husks while running, when the engine starts, outside air is sucked in to cool the radiator or engine body, etc. HL, remove a large amount of straw and dust from the engine cover! In order to inhale from I4, it is necessary to clean and inspect each part of the engine, but the cover is divided depending on the arrangement of the radiator, cockpit, etc., and each cover is removed to clean and inspect the engine. However, the opening area of the cover is limited by the peripheral parts of the aircraft, making it difficult to perform the work.

Means for Solving the Problem This invention has a reaping device (1) for reaping the grain culm at the front part, and a threshing device (2) for receiving and threshing the harvested husk at the rear part.
), etc. A control platform (5) is provided on the front part of one side of the platform (4) on the aircraft platform (4), and the engine ( 6), an engine cover (7) that covers the engine (6) and has a pilot seat (8) on top, and a control floor between the pilot seat (8) and the pilot platform (5). (9) is integrated with the control floor (9), and a machine base (4) is provided so as to be rotatable outward and forward using the outer front part of this control floor (9) as a fulcrum (10) to constitute a combine operator's seat.

Functions and Effects of the Invention During the combine harvester operation, the operator sits on the operator's seat (8) and operates the traveling device (3), then reaps the husk with the reaping device (1) and removes the cut husk. The culm is a threshing device (2)
He was removed from FJ.

The cockpit (8), the cockpit floor (9), and the engine cover (7) are integrated into a single weight, centered around the fulcrum (10) on the outside front of the cockpit floor (9), and the reaping device on the outside front of the machine platform (4). (1) Can be rotated to the side.

During combine harvester work, a large amount of straw and dust is sucked in through the engine cover (7), so when cleaning and inspecting each part of the engine (6), the operator's seat (8) can be rotated. ), the cockpit floor (9) integrated with the engine cover (7) that covers the engine (6), and the engine cover (7) that covers the engine (6) are rotated to the outside front side of the aircraft platform (4) to cover the top and outside of the engine (6). The sides can be left wide open with no obstacles in the way, making inspection and adjustment easier.

Embodiment In the illustrated example, a threshing gc rack (2) is placed on the top of the machine stand (4), a traveling device (3) is attached to the bottom, and a reaping device (1) is attached to the front. It has a suspended configuration.

A control stand (5) is installed on the front part of one side of the machine stand (4), and a control stand (11) is installed on the side of the control stand (5) on the side of the threshing device (2). The control platform (5) is provided with a strike clutch lever (12) that changes the traveling direction of the aircraft from left to right in conjunction with a strike clutch mechanism, and the side control platform (11) is equipped with a reaping device ( The reaping latch lever (1) that interlocks the
3), a threshing clutch lever (
14) and a traveling speed change lever (15).

An engine (
6), and a radiator (1B) is provided outside the engine (6).

Front and rear sides of the engine (6), outer radiator (1B)
An engine cover (7) that covers the front and top surfaces of the engine cover (7) forms a framework.A ventilation net is provided on the radiator (1B) side of the engine cover (7).

At the top of the engine cover (7) is the PJ vertical seat (8).
A fuel tank (17) is installed behind the cockpit (8).
) has been established.

The engine cover (7) includes a control floor (9) between the cockpit (8) and the control platform (5), and a side control panel that stands up from the inner edge of the control floor (9). A cover (18) covering the side surface of the stand (11) is connected in one piece.

On the outer side of the aircraft base (4), there is a rotating flap b (1
9) tr: a';t, this rotating frame (19)
The outer portions of the engine cover (7) and the control floor (9) are fixed to. The rear end of the rotating frame (+9) is provided with a locking tool that can be engaged with and detached from the machine base (4).

(20) is a grain tank, (21) is a bag holder, (
22) is a cutter device.

The engine (6) transmits power to each part, the reaping latch lever (13) and the threshing clutch lever (14) are engaged to interlock the reaping device (1) and the threshing device (2), and the traveling gear shift lever (15) is activated. Operate to move the aircraft forward. The operator sits on the cockpit (8) and turns on and off the strike clutch lever (12') on the cockpit (5) before turning the reaping device (
1) is moved along the machine platform (4) by the traveling device (3) in line with the rows of the shell culm, and the shell culm is harvested and threshed, and the bag receiving stand (21
) The bagging operation is performed by supplying grain from the upper grain tank (20) to the grain bag placed on the grain bag.

During combine harvester operation, when the engine (6) is started, outside air is sucked in through the ventilation network of the engine cover (7) to cool the radiator (18) or the engine (6) body.

During combine harvester operation, a large amount of straw waste and dust are sucked in through the ventilation net, so it is necessary to clean and inspect each part of the engine (6). 4) and remove the lock from the cockpit (8) to the aircraft base (4).
When the driver's seat (8) is rotated toward the outer front reaping device (1) side, the operator's seat (8) is integrated with the engine cover (7), the control floor (9), and the cover (18) of the horizontally tilted control platform (11). , the rotating arm (19) is rotated about the fulcrum (10) at the front of the engine (6) to widen the outer and upper surfaces of the engine (6).

In addition, since the cover (18) of the side control platform (11) can be opened, the interlocking system from the engine (6) to the traveling device (3), reaping device (1), and threshing device (2) can be inspected. It can be made easier to do.

[Brief explanation of drawings]

The figures show one embodiment of the present invention, with FIG. 1 being a perspective view showing a part of the operating state, and FIG. 2 being an overall side view. In the figure, code (1) is the reaping device, (2) is the threshing device, and (3) is the reaping device.
) is the traveling gear, (4) is the aircraft platform, (5) is the control platform, (6)
is the engine, (7) is the engine cover, (8) is the cockpit, (9) is the cockpit floor, and (10) is the fulcrum. Figure 1

Claims (1)

[Claims] A reaping device (1) for reaping the shell culm is installed at the front, and a traveling device (3) is equipped with a threshing device (2) for receiving and threshing the cut culm at the rear. A cockpit (5) is provided at the front of one side of the aircraft base (4), an engine (6) is mounted on the rear side of the cockpit (5), and a cockpit (6) is mounted above the engine (6). The engine cover (7) having the 8) and the control floor (9) between the cockpit (8) and the cockpit (5) are integrated to form an outer front part of the control floor (9). A combine operator's seat is provided as a fulcrum (10) on a machine base (4) so as to be rotatable outward and forward.