Maraging steel golf club head
Abstract
The invention concerns a golf club head whereof the strike surface zone at least is made of maraging steel essentially consisting of 6.0 to 9.0 wt. % of nickel, 11.0 to 15.0 wt. % of chromium, 0.1 to 0.3 wt. % of titanium, 0.2 to 0.3 wt. % of beryllium, the rest being iron and impurities resulting from production, the temperature of the martensitic phase being M s ≧130 ° C. and the ferrite content being adjusted at C Ferrit<3%. Said maraging steel typically exhibits tensile strength R m of about 2800 MPa, yield strength R p0.2 of about 2600 MPa, Vickers hardness>800 and alternating flexure strength o′ bw of about 1550 MPa.
Claims
exact text as granted — not AI-modified1 . Golf club head that is at least partly made of a corrosion-free, precipitation-hardened, maraging steel with a martensite temperature M s ≧130° C., a ferrite content C Ferrite<3%, wherein the maraging steel essentially consists of 6.0 to 9.0 wt. % nickel, 11.0 to 15.0 wt. % chromium, 0.1 to 0.3 wt. % titanium, 0.2 to 0.3 wt. % beryllium, the rest being iron together with unavoidable impurities, and wherein maraging steel in accordance with the invention exhibits a tensile strength R m >2000 MPa and a yield strength R p0.2 >1900 MPa.
2 . Golf club head in accordance with claim 1 wherein up to 35% of the chromium content can be replaced by molybdenum and/or tungsten.
3 . Golf club head in accordance with claim 2 wherein the maraging steel essentially consists of 8.0 wt. % nickel, 13.0 wt. % chromium, 0.2 wt. % titanium, 0.25 wt. % beryllium, 1.0 wt. % molybdenum, the rest being iron together with unavoidable impurities.
4 . Golf club head in accordance with claim 1 wherein the maraging steel comprises up to 0.1 wt. % cerium or cerium misch metal as a deoxidizing agent.
5 . Golf club head in accordance with claim 1 wherein the maraging steel can comprise at least one of the elements manganese, niobium or silicon in individual proportions of less than 0.5 wt. %.
6 . Golf club head in accordance with claim 1 wherein the maraging steel comprises at least one of the elements C, N, S, P, B, H, or O in individual proportions of less than 0.1 wt. %.
7 . Golf club head in accordance with claim 5 wherein the maraging steel exhibits a martensite temperature M s =[629.45−6.8(Cr+1.2 Mo+0.6 W)−24.5(Ni+0.15 Co)−13.2 Mn−11.2 Si−670(C+N)] ° C.
8 . Golf club head in accordance with claim 5 wherein the spring steel exhibits a ferrite content C Ferrite=[11.8 Si+7.92(Cr+Mo+0.5 W)+15.84 Ti−2.91 Mn−5.83(Ni+0.3 Co)−174.9(C+N)−77.08] wt. %.
9 . Golf club head in accordance with claim 1 wherein the maraging steel exhibits a tensile strength R m >2400 MPa.
10 . Golf club head in accordance with claim 9 wherein the maraging steel exhibits a tensile strength R m of approximately 2800 MPa.
11 . Golf club head in accordance with claim 1 wherein the maraging steel exhibits a yield strength R p0.2 >2100 MPa.
12 . Golf club head in accordance with claim 11 wherein the maraging steel exhibits a yield strength R p0.2 of approximately 2500 MPa.
13 . Golf club head in accordance with claim 1 wherein the maraging steel exhibits an alternating flexure strength o′ bw of approximately 1350 MPa.
14 . Golf club head in accordance with claim 13 wherein the maraging steel exhibits an alternating flexure strength o′ bw of approximately 1550 MPa.
15 . Golf club head in accordance with claim 1 wherein the maraging steel exhibits a Vickers hardness HV>700.
16 . Golf club head in accordance with claim 15 wherein the maraging steel exhibits a Vickers hardness HV>800.
17 . Golf club head in accordance with claim 1 wherein the maraging steel exhibits a maximal storable energy of more then 30 MPa.
18 . Golf club head in accordance with claim 17 wherein the maraging steel exhibits a maximal storable energy of approximately 40 MPa.
19 . Process for the manufacturing of maraging steel for a golf club head in accordance with claim 1 comprising the following process steps:
a) Melting the alloy under vacuum or protective gas followed by casting into an ingot; b) Hot forming the ingot into a strip at 900° C.≦T 1 ≦1150° C.; c) Carrying out a solution annealing of the strip at 850° C.≦T 2 ≦1100° C.; d) Cooling the strip to a temperature T 3 ≦300° C.; e) Grinding the strip to remove the beryllium-depleted edge zone; f) Cold forming the strip with a cold forming degree that is greater than or equal to 60%; g) First heat treatment of the strip at 400° C.≦T 4 ≦550° C. for a duration of 1 hour to 10 hours.
20 . Process in accordance with claim 17 comprising the following additional process step:
h) Second heat treatment of the strip at 300° C.≦T 5 ≦470° C. for a duration of ten to 100 hours.Join the waitlist — get patent alerts
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