JPS6235315Y2 - - Google Patents

Description

[Detailed explanation of the idea] Harvesters are equipped with a shelling section at the front in the direction of movement of the aircraft and an engine section at the rear. Conventionally, harvesters have been produced in such a way that the front-to-back balance of the aircraft is maintained even when the shelling section is mounted. Therefore, when the heavy shelled part is removed and used as a transport vehicle, the front part is light when it is empty and the front and rear balance is greatly disrupted, so when the transport vehicle starts or climbs a slope, the head door will not open. It was extremely dangerous. In order to prevent this risk, it may be possible to attach a balance weight to the front end of the cargo platform, but a simple balance weight has the drawbacks of increasing the weight of the machine, making it inconvenient to attach and detach, and increasing costs. The present invention attempts to overcome the above-mentioned conventional drawbacks by attaching and detaching a balance weight and auxiliary loading platform having approximately the same width as the loading platform to the front of the loading platform.

This will be explained below with reference to the drawings. 1 in the figure is the traveling part 2
An engine section 3 is mounted on the rear end of the fuselage frame 1, and power is transmitted from the engine section 3 to the traveling section 2 by an appropriate transmission device. It's becoming like that. Further, a driving operation section 4 is provided above the engine section 3. 5 is supported by the fuselage frame 1 in front of the engine section 3, and the shelled section 6
This is a loading platform configured so that it can be attached and detached. The shelling section 6 is mounted on the loading platform 5 so that the dust exhaust port 7 faces the front of the machine body, the shell culm supply port 8 is located on one side of the machine body, and the culm discharge device 9 is located on the other side of the machine body. ing. Reference numeral 10 denotes a balance weight and auxiliary loading platform (hereinafter referred to as the auxiliary loading platform) which is located almost directly below the culm removal device 9 and has approximately the same width as the loading platform and is configured to be detachably attached to the side surface of the loading platform 5. A plurality of branch culms 11 provided at one end of the carrier 10 are fitted into side support holes 12 formed in the side of the loading platform 5 and are removably fixed. When this auxiliary loading platform 10 is installed directly below the culm ejecting device 9 when a binding machine or cutter is not attached to the culm ejecting device 9 of the shelling section 6, it helps maintain the weight balance between the left and right sides of the machine body. Reference numeral 13 designates a shell discharge pipe for the shelling section, which is disposed so as to open directly above the paddy holder 14 provided below the operation section 4. Figure 3 shows the shelling part 6
This is a perspective view when the cargo platform 5 and the auxiliary cargo platform 10 are installed in a perspective view when the cargo platform 5 is removed and used as a transport vehicle, and a front end support hole 15 having the same shape as the side support hole 12 is formed at the front end of the cargo platform 5. As a result, the auxiliary loading platform 10 can be attached to and removed from the front of the loading platform 5. Figures 4 and 5 show the auxiliary loading platform 10 and loading platform 5.
As shown in the figure, the cargo platform extends forward for a long time, increasing the loading area and moving the center of gravity forward to stabilize the aircraft.
6 to 10 show other embodiments,
Figures 6 to 8 show examples in which the rice holder can be attached to the front of the loading platform, and the side loading platforms provided on both sides of the loading platform can be moved forward. To explain this with a diagram, reference numeral 16 is a balance weight/auxiliary loading platform (hereinafter referred to as an auxiliary loading platform) having approximately the same width as the loading platform 5, which has a plurality of support rods 17 at one end, and is provided at both the front and rear ends of the loading platform 5. Support pipe 18,1
9, and can be attached to the rear of the loading platform 5 during shelling work and used as a paddy holder, and during transportation work it can be attached to the front of the loading platform 5 to serve as a balance weight and support. It is used as a loading platform. In addition, 20 and 21 each have a plurality of support culms 22 inside,
23, which is attached to both sides of the cargo platform 5. 24 and 25 are support pipes provided on both sides of the loading platform 5 to support the side loading platforms 20 and 21;
is arranged so as to enable both a position where the front ends of the side loading platforms 20 and 21 and the front end of the loading platform 5 are in line with each other, and a position where the front end of the auxiliary loading platform 16 attached to the front of the loading platform 5 is in line with each other. There is. Because of this configuration, when the shelling section 6 is mounted, the side cargo platforms 20, 2
1 is attached to the loading platform 5 so that its front end is in line with the front end of the loading platform 5, and when the shelled part 6 is removed, the auxiliary loading platform 16 is attached to the front of the loading platform 5,
The front end of both side loading platforms 20 and 21 is the auxiliary loading platform 16.
The purpose of this is to move the aircraft so that it is aligned with the front end of the aircraft, thereby widening the loading platform and moving the center of gravity forward to maintain stability of the aircraft. The details of the attachment part are, for example, as shown in FIG.
a, and the support culm 22 of the side loading platform 20 is inserted into this and fixed.

As described above, in a harvester in which the shelling section 6 is mounted on the front of the body frame 1 and the engine section 3 is mounted on the rear, when the shelling section 6 is removed and used as a transport vehicle, the side of the loading platform 5 or the body of the machine is Since the structure is such that a balance weight and auxiliary cargo platform 10, which is approximately the same width as the cargo platform 5 provided at the rear, is attached to the front of the machine to balance the front of the machine, when using the harvester, it is necessary to remove the shell from the shell. When removed and used as a transport vehicle, the auxiliary loading platform 10 is attached to the front of the loading platform 5, so when empty, the front of the aircraft is light and the front-to-back balance of the aircraft will not be significantly disturbed. Since the aircraft does not tilt when starting or climbing a slope, it is safe to handle.The auxiliary cargo bed is configured to have approximately the same width as the cargo bed, so the left and right balance is maintained, and the steering wheel does not tilt while driving. There is no risk of being taken to one side. Furthermore, when transporting rice, wheat, etc., the auxiliary loading platform 10 can be attached to the front of the loading platform 5 to increase the loading capacity and improve work efficiency.
The auxiliary loading platform constructed in this manner is not just a balance weight, but has the feature that it is extremely easy to attach, detach, and move, and can be used for multiple purposes.

[Brief explanation of the drawing]

Fig. 1 is a side view of the harvester of the present invention, Fig. 2 is a plan view thereof, Fig. 3 is a perspective view when used as a carrier, Fig. 4 is a side view of the same, Fig. 5 is a plan view of the same, Fig. 6 to 10 show other embodiments, FIGS. 6 and 7 are plan views showing working conditions, and FIG. 8 is a sectional view of the mounting portion. 3...Engine section, 4...Driving operation section, 5...
Loading platform, 6... Shelling section, 9... Culm removal device, 10...
Balance weight and auxiliary loading platform, 11...branch, 1
2...Support hole, 13...Shell grain discharge pipe, 14...
...Paddy holder, 15...Front end support hole.

Claims (1)

[Scope of utility model registration request] In a harvester in which a shelling section 6 is mounted in the front of the body frame 1 and an engine section 3 is mounted at the rear, the shelling section 6 is made detachable from the loading platform 5, and is connected to the loading platform 5 provided on the side of the loading platform 5 or at the rear of the body. The balance weight and auxiliary loading platform 10 of approximately the same width are made removable, and when the shelled part is removed and used as a transport vehicle, the balance weight and auxiliary loading platform 10 is attached to the front of the loading platform 5 to balance the machine. A balance weight and auxiliary loading platform for a harvester characterized by being configured as follows.