RAZOR BLADE AND COMPOSITION FOR A RAZOR BLADE
20220250266 · 2022-08-11
Inventors
Cpc classification
B26B21/4068
PERFORMING OPERATIONS; TRANSPORTING
C21D9/18
CHEMISTRY; METALLURGY
C22C38/002
CHEMISTRY; METALLURGY
B21D53/60
PERFORMING OPERATIONS; TRANSPORTING
B26B21/565
PERFORMING OPERATIONS; TRANSPORTING
International classification
B21D53/60
PERFORMING OPERATIONS; TRANSPORTING
C21D1/18
CHEMISTRY; METALLURGY
C21D9/18
CHEMISTRY; METALLURGY
Abstract
A razor blade has a first and a second portion. The first portion has a cutting edge at an exterior end and is angled relative to the second portion by a bending process. A bent region that can be arcuate is intermediate the first and second portions. The razor blade is manufactured from martensitic stainless steel being mostly iron and having (by weight): 0.40 to 0.60% C; 0.30 to 0.55% Si; 0.70 to 0.90% Mn; 13.0 to 14.0% Cr; 0.50 to 1.0% Mo; and 0.03 to 0.2%, more preferably 0.03-0.1% N.
Claims
1. A razor blade (50), comprising: a first portion (66) and a second portion (68), the first portion (66) having a cutting edge (20) at an exterior end thereof and being angled relative to the second portion (68) by a bending process; and a bent region (52) intermediate the first portion (66) and the second portion (68); wherein the razor blade (50) comprises a martensitic stainless steel comprising mainly iron and having (by weight): 0.40 to 0.60% Carbon 0.30 to 0.55% Silicon 0.70 to 0.90% Manganese 13.0 to 14.0% Chromium 0.50 to 1.0% Molybdenum, and 0.03 to 0.2% Nitrogen.
2. The razor blade (50) of claim 1, wherein the first portion (66) is angled relative to the second portion (68) by an angle (60) in a range 105 to 130 degrees.
3. The razor blade (50) of claim 1, wherein the bent region (52) includes an external radius (54) in a range 0.2 to 1.5 mm.
4. The razor blade (50) of claim 1, wherein the second portion (68) has a thickness (14) in a range 0.05 to 0.125 mm.
5. The razor blade (50) of claim 1, wherein the bending process is not preceded by a reheating process to modify the structure at a bending region (70).
6. The razor blade (50) of claim 1, wherein the martensitic stainless steel further comprises (by weight): Sulphur in a range up to 0.02% and Phosphorous in a range up to 0.0025%.
7. The razor blade (50) of claim 1, wherein the razor blade (50), in a region of the cutting edge (20), has a hardness in a range 550 to 640 HV.
8. The razor blade (50) of claim 1, wherein the cutting edge (20) extends along a length (40) of the razor blade (50).
9. A method of making a razor blade (50), comprising the steps of: a) providing a martensitic stainless steel strip (10) having a width (12) and a thickness (14) and including a front edge portion (16) and a back edge portion (18), the strip (10) comprising mainly iron and having (by weight): 0.40 to 0.60% Carbon 0.30 to 0.55% Silicon 0.70 to 0.90% Manganese 13.0 to 14.0% Chromium 0.50 to 1.0% Molybdenum, and 0.03 to 0.2% nitrogen; b) hardening the strip (10); c) forming a cutting edge (20) along at least one of the front edge portion (16) and rear edge portion (18); d) applying a coating (30) comprising at least a fluoropolymer material to the cutting edge (20) and curing the fluoropolymer material to thereby anneal at least a portion containing the cutting edge (20) to a hardness at least 550 HV; preferably 620-640 HV e) separating the strip (10) to provide a discrete length (40); and f) forming the discrete length (40) in a bending process to provide a bent region (52) intermediate a first portion (66) having the cutting edge (20) at an exterior end thereof, the first portion (66) being angled relative to a second portion (68).
10. The method of claim 9, wherein step d) is performed after step e).
11. The method of claim 9, wherein the bent region (52) includes an external radius (54) in a range 0.2 to 1.5 mm.
12. The method of claim 9, wherein the strip (10) has a thickness (14) in a range 0.05 to 0.125 mm.
13. The method of claim 9, wherein the first portion (66) is angled relative to the second portion (68) by an angle (60) in a range 105 to 130 degrees.
14. The method of claim 9, wherein the strip (10) further comprises (by weight): Sulphur in a range up to 0.02% and Phosphorous in a range up to 0.0025%.
15. The method of claim 9, wherein step f) is a swivel bending process.
16. The razor blade of claim 1, wherein the martensitic stainless steel contains (by weight) 0.03 to 0.1% Nitrogen.
17. The method of claim 9, wherein the martensitic stainless steel contains (by weight) 0.03 to 0.1% Nitrogen.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0013]
[0014]
DETAILED DESCRIPTION
[0015] Martensitic stainless steels having a carbon content 0.6-0.7% or more, about 13% (e.g. 12.5% to 13.5%) chromium and substantially free of molybdenum have been used for making razor blades. These materials are widely available, have adequate corrosion resistance for their intended use and can be sharpened to provide a high-quality cutting edge. Exemplary commercially available materials are those such as GINS made by HITACHI METALS and 13C26 made by SANDVIK. These materials appear as Alloy 1 in Table 1, below. Another commercially available martensitic stainless steel suitable for manufacturing razor blades is the grade designated GIN7 manufactured by HITACHI METALS that appears as Alloy 2 in Table 1. Alloy 3 and Alloy 4 are experimental compositions according to the present disclosure.
TABLE-US-00001 TABLE 1 (All % by weight) C % Cr % Si % Mn % Mo % N % Fe Alloy 1 0.62-0.75 12.7-13.7 0.2-0.5 0.45-0.75 ≤trace 0 Balance Alloy 2 0.48-0.52 13.0-14.0 0.3-0.55 0.7-0.9 1.2-1.4 0 Balance Alloy 3 0.45-0.6 13.0-14.0 0.3-0.55 0.7-0.9 0.5-1.0 0 Balance Alloy 4 0.45-0.6 13.0-14.0 0.3-0.55 0.7-0.9 0.5-1.0 0.03-0.1 Balance (All alloys can contain ≤0.02 Sulphur and ≤0.0025 Phosphorous, Alloy 4 can contain 0.03-0.2% N).
[0016] Referring now to the drawings and in particular
[0017] A representative sectional view of the razor blade 50 having a bent portion 52 is shown in
[0018] Razor blades having bent portions of the four alloys (Alloy 1-Alloy 4) were produced according to varying thickness (t, 14), hardness (Hv), bend angle (α, 60) and outer bend radius (Ro, 54) as shown in Table 2, below and depicted in
TABLE-US-00002 TABLE 2 Test # Alloy t Hv α Ro Crack ED 1 Alloy 1 0.1 620 123 1.3 ≤100 1 2 Alloy 1 0.076 550 108-112 0.92 ≤10 4 3 Alloy 1 0.076 620 123 0.98 ≤100 1 4 Alloy 1 0.076 610 118 0.98 ≤100 1 5 Alloy 2 0.076 590 108-112 0.48 None 3 6 Alloy 3 0.076 610 110 0.7 None 2 7 Alloy 4 0.076 610 110 0.3-0.48 None 2 Where: t = strip thickness (mm); Hv = strip hardness (Vickers) at 200 g load on cross section, all hardness values ± 20 units; α = bend angle (degrees); Ro = outer radius of bent region (mm); Crack = presence of end cracks at dimension noted (microns); ED = cutting edge durability, ranked 1-4 where 1 = most durable, 4 = least durable, as evaluated.
[0019] The addition of Nitrogen to Alloy 4 advantageously provides a razor blade of desirable ductility wherein the bent portion can beneficially have a smaller outer bend radius with a low bend angle while the razor blade exhibits a relatively desirable cutting edge durability. Without being limited by theory, it is believed the nitrogen alloyed martensitic structure is finer and more uniform than carbon alloyed material, giving a very fine precipitate distribution and superior properties on tempering.
[0020] While various embodiments have been described above, it should be understood that they have been presented by way of example only, and not limitation. For instance, modifications or changes as can be made within the scope of the attached claims and features disclosed in connection with any one embodiment can be used alone or in combination with each feature of the respective other embodiments. Thus, the breadth and scope of any embodiment should not be limited by any of the above described exemplary embodiments but should be defined only in accordance with the following claims and their equivalents.