IP Library Granted Patent US 10,174,391
Granted Patent B2
US 10,174,391 · App. 13/382,052 · Granted Jan 8, 2019

Cryogenic treatment of martensitic steel with mixed hardening

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Quick Facts
Patent No.
US 10,174,391
App. No.
13/382,052
Granted
Jan 8, 2019
Kind
B2
Abstract

The invention relates to a method for producing martensitic steel that comprises a content of other metals such that the steel can be hardened by an intermetallic compound and carbide precipitation, with an Al content of between 0.4% and 3%, comprising the following steps: (a) heating the entirety of the steel above its austenizing temperature, (b) cooling said steel approximately to ambient temperature, (c) placing said steel in a cryogenic medium. The temperature T 1 is substantially lower than the martensitic transformation temperature Mf, and the time t during which said steel is kept in said cryogenic medium at a temperature T 1 from the moment when the hottest part of the steel reaches a temperature lower than the martensitic transformation temperature Mf is at least equal to a non-zero time t 1 , the temperature T 1 (in ° C.) and the time t 1 (in hours) being linked by the equation T 1 =ƒ(t 1 ), the first derivative of the function ƒ relative to t, ƒ′(t), being positive, and the second derivative of ƒ relative to t, ƒ″(t), being negative.

Claims (55)

1. A method for producing a martensitic steel, the method comprising:

(a) heating a steel to a first temperature above an austenizing temperature thereof,

(b) subsequently cooling the steel to a second temperature equal to an ambient temperature, and

(c) subsequently placing and keeping the steel in a cryogenic medium at a third temperature T 1 for a period of time t greater than a time t 1 and less than 5 hours,

wherein

the third temperature T 1 is less than a martensitic transformation end temperature M f of the steel, which is below 0° C.,

the period of time t in (c) is determined from a moment when an internal portion of the steel having a highest temperature following said cooling (b) reaches a temperature lower than M f ,

the third temperature T 1 in ° C. with a tolerance of +/− 5° C. and the time t 1 in hours with a tolerance of +/− 5% are related according to an equation T 1 =ƒ(t 1 ), where the function ƒ is given by

ƒ(t)=57.666×(1−1/(t 0.3 −0.14) 1.5 )−97.389

or by a temperature-translated curve relative to ƒ(t), and

the steel comprises Al in a content of from 0.4 wt % to 3 wt % and is capable of being hardened by an intermetallic compound and carbide precipitation.

2. The method of claim 1 , wherein the steel consists of:

0. 18 to 0.3 wt % of C,

5to 7 wt % of Co,

2to 5 wt % of Cr,

1to 2 wt % of Al,

1to 4 wt % of Mo+W/2,

traces to 0.3 wt % of V,

traces to 0.1 wt % of Nb,

traces to 50 ppm of B,

10.5 to 15 wt % of Ni with Ni ≥7+3.5 Al,

traces to 0.4 wt % of Si,

traces to 0.4 wt % of Mn,

traces to 500 ppm of Ca,

traces to 500 ppm of at least one rare earth metal,

traces to 500 ppm of Ti,

traces to 50 ppm of O if developed from molten metal or to 200 ppm of O if developed through powder metallurgy,

traces to 100 ppm of N,

traces to 50 ppm of S,

traces to 1 wt % of Cu,

traces to 200 ppm of P, and

a remainder of Fe.

3. The method of claim 2 , wherein

a content of C is from 0.200 wt % to 0.250 wt %,

a content of Ni is from 12.00 wt % to 14.00 wt %,

a content of Co is from 5.00 wt % to 7.00 wt %,

a content of Cr is from 2.5 wt % to 4.00 wt %,

a content of Al is from 1.30 wt % to 1.70 wt %, and

a content of Mo is from 1.00 wt % to 2.00 wt %.

4. The method of claim 1 , wherein the time t 1 is at least 1 hour.

5. The method of claim 1 , wherein said cooling (b) comprises quenching the steel in a medium with a drasticity of at least a drasticity of air.

6. The method of claim 1 , wherein (c) starts less than 70 hours after a surface temperature of the steel reaches 80° C.

7. A piece made from a martensitic steel obtained by the method of claim 1 , wherein a residual austenite level in the martensitic steel is less than 3wt %.

8. A turbomachine transmission shaft made from a martensitic steel obtained by the method of claim 1 , wherein a residual austenite level in the martensitic steel is less than 3 wt %.

9. A martensitic steel obtained by the method of claim 1 , wherein an average hardness of the martensitic steel is 575 Hv with a statistical minimum of 570 Hv and maximum of 579 Hv.

10. The method of claim 1 , wherein t 1 is greater than 2 hours.

11. The method of claim 1 , wherein t 1 is greater than 3 hours.

12. The method of claim 1 , wherein t 1 is greater than 4 hours.

13. The method of claim 1 , wherein a residual austenite level in the martensitic steel is less than 3 wt %.

14. The method of claim 1 , wherein a residual austenite level in the internal portion of the martensitic steel is less than 3 wt %.

15. The method of claim 14 ,

wherein the martensitic steel has an average hardness of 575 Hv with a statistical minimum of 570 Hv and maximum of 579 Hv.

16. The method of claim 1 , wherein an average hardness of the martensitic steel is 575 Hv with a statistical minimum of 570 Hv and maximum of 579 Hv.

17. The method of claim 1 , wherein the internal portion of the steel during (c) is a central region of the steel.

18. The method of claim 17 , wherein after the internal portion of the steel reaches a temperature lower than M f and before the time t i , a residual austenite level increases from a surface region to the internal portion.

Assignments (4)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded Jul 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 047528/0916 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 27, 2012
From: FERRER, LAURENT
To: SNECMA
Reel/Frame 027934/0598 →