TOOL FOR PROCESSING ENGINE BLOCK AND METHOD OF PROCESSING ENGINE BLOCK

Abstract

Disclosed is a tool for processing an engine block. The tool for processing the engine block includes: multiple cutting inserts; and main cutting edges which are formed at end portions of the inserts, respectively, in which the main cutting edge has a positive axial inclination angle and a radial inclination angle of 5 degrees to 0 degree.

Claims

1. A tool for simultaneously processing an engine block made of different materials, the tool comprising: multiple cutting inserts; and main cutting edges which are formed at end portions of the inserts, respectively, wherein the main cutting edge has a positive axial inclination angle and a radial inclination angle of 5 degrees to 0 degree.

2. The tool of claim 1, wherein the tool processes the engine block made of different materials with a cutting speed of 400 to 800 m/min and a feed per tooth of 0.05 to 0.099 mm/tooth.

3. The tool of claim 2, wherein the tool processes the engine block made of different materials with a spindle rotational speed of 637 to 764 rpm.

4. The tool of claim 2, wherein the tool processes the engine block made of different materials with a cutting speed of 500 to 600 m/min and a feed per tooth of 0.062 to 0.087 m/tooth.

5. A method of processing an engine block made of different materials by using a tool including a cutting insert, wherein the tool processes the engine block made of different materials with a cutting speed of 400 to 800 m/min, a feed per tooth of 0.05 to 0.099 mm/tooth, and a spindle rotational speed of 637 to 764 rpm.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0018] FIG. 1 is a perspective view illustrating a tool for processing an engine block according to the present disclosure.

[0019] FIG. 2 is a schematic view briefly illustrating an axial inclination angle and a radial inclination angle of a main cutting edge according to the present disclosure.

[0020] FIG. 3A is a view illustrating a tool life with respect to a cutting speed according to the present disclosure.

[0021] FIG. 3B is a view illustrating surface roughness with respect to a feed per tooth according to the present disclosure.

[0022] FIG. 3C is a view illustrating a tool life with respect to a radial inclination angle of an insert according to the present disclosure.

[0023] FIG. 4 is a view illustrating an engine block which is processed by the tool for processing an engine block according to the present disclosure.

DETAILED DESCRIPTION

[0024] In the following detailed description, reference is made to the accompanying drawing, which forms a part hereof. The illustrative embodiments described in the detailed description, drawing, and claims are not meant to be limiting. Other embodiments may be utilized, and other changes may be made, without departing from the spirit or scope of the subject matter presented here.

[0025] Hereinafter, exemplary embodiments of the present disclosure will be described in detail with reference to the accompanying drawings so that those skilled in the art to which the present disclosure pertains may easily carry out the exemplary embodiments. However, the present disclosure may be implemented in various different ways, and is not limited to exemplary embodiments described herein. A part irrelevant to the description will be omitted in the drawings in order to clearly describe the present disclosure, and similar constituent elements will be designated by similar reference numerals throughout the specification.

[0026] FIG. 1 is a perspective view illustrating a tool for processing an engine block according to the present disclosure, FIG. 2 is a schematic view briefly illustrating an axial inclination angle and a radial inclination angle of a main cutting edge according to the present disclosure, FIG. 3A is a view illustrating a tool life with respect to a cutting speed according to the present disclosure, FIG. 3B is a view illustrating surface roughness with respect to a feed per tooth according to the present disclosure, and FIG. 3C is a view illustrating a tool life with respect to a radial inclination angle of an insert according to the present disclosure.

[0027] Referring to FIG. 1, a tool 100 according to the present disclosure for processing an engine block such as an engine block illustrated in FIG. 4 includes a cutter main body 110, multiple inserts 120 which are formed along an outer circumference of the cutter main body 110, and main cutting edges 130 which are provided at end portions of the inserts 120, respectively.

[0028] The insert 120 may be particularly made of a poly crystalline diamond (PCD) material which is a diamond sintered material, but the insert 120 may also be made of other materials for simultaneously processing aluminum and cast iron.

[0029] The main cutting edge 130 for facing purpose and the main cutting edge 130 for wiping purpose may be alternately formed on the inserts, respectively, but particularly, only the main cutting edge 130 for wiping purpose may be formed to improve roughness of the engine block and increase a tool life.

[0030] To process an engine block made of different materials, it is essential to provide a tool for processing an engine block which has basically a prolonged tool life in order to inhibit burrs from being formed, ensure excellent roughness, improve economic feasibility regarding the processing, and improve productivity.

[0031] According to the present disclosure, experiments have been conducted under various conditions based on a cutting speed (vc), a spindle rotational speed (n), a feed per tooth (fz), and a table feed rate (ye in order to improve the tool life.

Example 1

[0032] Cutting speed=500 m/min

[0033] Spindle rotational speed=637 rpm

[0034] Feed per tooth=0.063 mm/tooth

[0035] Table feed rate=1,200 mm/min

Example 2

[0036] Cutting speed=600 m/min

[0037] Spindle rotational speed=764 rpm

[0038] Feed per tooth=0.087 mm/tooth

[0039] Table feed rate=2,000 mm/min

Comparative Example 1

[0040] Cutting speed=832 m/min

[0041] Spindle rotational speed=1,060 rpm

[0042] Feed per tooth=0.063 mm/tooth

[0043] Table feed rate=2,000 mm/min

Comparative Example 2

[0044] Cutting speed=1,570 m/min

[0045] Spindle rotational speed=2,000 rpm

[0046] Feed per tooth=0.033 mm/tooth

[0047] Table feed rate=2,000 mm/min

[0048] Examples 1 and 2 show excellent roughness, Example 1 shows a tool life of 1,000 ea/corner, and Example 2 shows a tool life of 900 ea/corner.

[0049] However, Comparative Example 1 shows defective roughness, Comparative Example 2 shows good roughness, Comparative Example 1 shows a tool life of 400 ea/corner, and Comparative Example 2 shows a tool life of 200 ea/corner.

[0050] Referring to FIG. 3A, regarding the tool life with respect to the cutting speed, the tool life is 1,000 ea/corner when the cutting speed is 500 m/min, and the tool life shows a tendency to be inversely proportional to an increase in cutting speed.

[0051] Referring to FIG. 3B, regarding the surface roughness with respect to the feed per tooth, the best surface roughness is shown when the feed per tooth is 0.033 mm/tooth, and the surface roughness has a good value until the feed per tooth becomes 0.099 mm/tooth.

[0052] Accordingly, according to the present disclosure, the tool may process the engine block made of different materials with the cutting speed of 400 to 800 m/min, the feed per tooth of 0.05 to 0.099 mm/tooth, and the spindle rotational speed of 637 to 764 rpm.

[0053] More particularly, according to an exemplary embodiment of the present disclosure, within a range in which the surface roughness is basically satisfied and the tool life of 900 ea/corner or more is also satisfied, the cutting speed is 500 to 600 m/min, the feed per tooth is 0.062 to 0.087 mm/tooth, and the spindle rotational speed is 637 to 764 rpm.

[0054] The processing may be performed with a cutting depth of 0.03 to 0.5 mm in order to satisfy the tool life.

[0055] Referring to FIG. 2, the main cutting edge 130 is formed to have a predetermined approach angle and a predetermined cutting angle, the main cutting edge 130 has a positive axial inclination angle AR and a radial inclination angle RR of 5 degrees to 0 degree, and the axial inclination angle AR has a positive value.

[0056] Referring to FIG. 3C, the tool life was measured while changing the radial inclination angle RR under a condition in which the axial inclination angle AR is 6 degrees, the cutting speed is 500 m/min, the feed per tooth is 0.062 mm/tooth, and the spindle rotational speed is 637 rpm.

[0057] In this case, the tool life is 1,000 ea/corner when the radial inclination angle

[0058] RR is 2 degrees, and the tool life is gradually decreased when the radial inclination angle RR is increased or decreased from 2 degrees.

[0059] Accordingly, it is possible to increase the tool life when the cast iron liner and the engine block made of aluminum are simultaneously processed under the aforementioned condition, and the increase in tool life reduces production costs and innovatively increases productivity of the engine block.

[0060] It will be appreciated that the exemplary embodiments of the present disclosure have been described above for purposes of illustration, and those skilled in the art may understand that the present disclosure may be easily modified in other specific forms without changing the technical spirit or the essential features of the present disclosure. Therefore, it should be understood that the above-described exemplary embodiments are illustrative in all aspects and do not limit the present disclosure. For example, each component described as a single type may be implemented in a distributed manner. Likewise, components described as a distributed type can be implemented in a combined type.

[0061] The scope of the present disclosure is represented by the claims to be described below rather than the detailed description, and it should be interpreted that the meaning and scope of the claims and all the changes or modified forms derived from the equivalent concepts thereto fall within the scope of the present disclosure.

[0062] From the foregoing, it will be appreciated that various embodiments of the present disclosure have been described herein for purposes of illustration, and that various modifications may be made without departing from the scope and spirit of the present disclosure. Accordingly, the various embodiments disclosed herein are not intended to be limiting, with the true scope and spirit being indicated by the following claims.