JPS58561Y2 - Traveling device in management machine - Google Patents

Description

[Detailed description of the invention] The present invention relates to a traveling device for a management machine, and in particular, it is a traveling device that can be attached to both axles of a management machine as an attachment. To provide a vehicle that can propel an aircraft strongly and smoothly and has a simple structure that can be suitably implemented.

Next, the embodiment shown in the drawings will be described.

B is a management machine, which has left and right axles 3, 3' on both sides of the lower part of the mission case 4, has an engine 5 mounted on the front part of the machine body, has a handle 6 extending to the rear, and has a handle 6 extending to the rear of the mission case 4. The hitch 7 attached to the machine is constructed in the same manner as the conventional structure so that various work devices can be connected to the hitch 7 to perform management work.

On both axles 3 and 3' of the management machine B, there is a running rotor A.

A' are each removably attached, but the rotors A and A' for delimiting rows have a hollow moist cavity ring a consisting of a hollow triangular prism of an equilateral triangle when viewed from the side, and a hollow moist hollow cylinder a made of a hollow triangular prism of an equilateral triangle when viewed from the side. Hollow wet cavity rings a' are integrally arranged side by side with their corners shifted, and the hollow wet cavity rings a are wider than the hollow rings a', and each of them has three wide flat surfaces around it. 1 and 1', respectively, and from the corner from each of the rain cavity rings a and a', from the end of one wide surface 1 and 1', claw plates 2 and 2' are formed.
are respectively extended and formed into protrusions, and an inner hollow ring a.

Shaft cylinders 8, 8' are protruded from the center of the inner surface of a', and can be installed by fitting both shaft cylinders 8, 8' onto the axles 3, 3' and inserting a pin into the pin hole 9°9. Configure it as follows.

In addition, an inner ring 10 is attached to the outer periphery of the rain cavity rings a and a', and an outer ring 11 that fits the tips of the claw plates 2 and 2' is assembled so as to be supported by the inner ring 10. When traveling, the claw plate 2,
The mounting configuration is such that both rings 10. 11 may be left assembled.

Therefore, the shaft cylinder 8°8' is fitted to the axle 3, 3' of the management machine B, and the rotor A for demarcation is attached as an attachment.
When A' is installed, both rotors A,
The rotation of A' causes the claw plates 2 and 2' to bite and exert driving force, and the hollow rings a and a' are hollow,
In addition, since it is triangular and has a wide peripheral surface of 1° 1', it has float-like buoyancy, and the driving force is strong, making it possible to perform plowing and plowing operations.

In this way, the present invention integrates the hollow wet hollow rings a and a', which are made of hollow triangular prisms that are triangular in side view, by shifting the corners of at least two adjacent hollow hollow hollow rings. The running rotors A and A' are formed by protruding claw plates 2 and 2' from the corners of the hollow wet cavity rings, and when they are inserted into the axles 3 and 3', attachments are attached to both axles. When a running rotor is installed as a 7, the driving force can be exerted by the biting of the claw plate, and since the hollow shaft is hollow and triangular, if the surrounding wide surface is in contact with the ground, it can be used reliably even in extremely wet fields. It maintains buoyancy and has a strong driving force to propel the aircraft smoothly, and since the parallel cavity axes are in different phases, the overall balance is better and the driving force is stronger, and the structure is simple. It has characteristics that allow it to be implemented suitably.

[Brief explanation of the drawing]

The drawings show an embodiment of the present invention; Fig. 1 is a side view of the management machine, Fig. 2 is an enlarged view of a part thereof, Fig. 3 is a plan view of the main part,
FIGS. 4 and 5 are side views taken from line 1--I and line 2--2 in FIG. 3, respectively, and FIG. 6 is a perspective view of both rotors. 1.1'... Wide surface, a, a'... Cavity axis, 2, 2'... Claw plate, A, A'...
...Rotor for running, 3,3'...Axle.

Claims (1)

[Scope of utility model registration request] A hollow wet cavity ring a consisting of a hollow triangular prism that is triangular in side view;
At least two a' are integrally arranged side by side with the corners of each adjacent hollow moist cavity ring shifted, and claw plates 2, 2' are protruded from the corner of the hollow wet cavity ring. A running device for a management machine, characterized in that running rotors A and A' are formed and inserted into axles 3 and 3'.