IP Library Granted Patent US 8,152,938
Granted Patent B2
US 8,152,938 · App. 12/869,268 · Granted Apr 10, 2012

Hardened martensitic steel, method for producing a component from this steel and component obtained in this manner

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Quick Facts
Patent No.
US 8,152,938
App. No.
12/869,268
Granted
Apr 10, 2012
Kind
B2
Abstract

The invention relates to steel which is characterized by the following composition as expressed in percentages by weight: —C=0.18 0.30%, —Co=5-7%, —Cr=2-5%, —Al=1-2%, —Mo+W/2=1-4%, —V=trace 0.3%, —Nb=trace 0.1%, —B=trace—50 ppm, —Ni=10.5-15% with Ni≧7+3.5 Al, —Si=trace 0.4%, —Mn=trace 0.4%, —Ca=trace—500 ppm, —Rare earths=trace—500 ppm, —Ti=trace—500 ppm, —O=Trace—200 ppm if the steel is obtained by means of powder metallurgy or trace—50 ppm if the steel is produced in air or under a vacuum from molten metal, —N=trace—100 ppm, —S=trace—50 ppm, —Cu=trace—1%, and —P=trace—200 ppm, the remainder including iron and the inevitable impurities resulting from production. The invention also relates to a method of producing a part from said steel and to the part thus obtained.

Claims (36)

1. Mechanical component or structural element component, characterized in that it is produced in accordance with a method for producing a component from steel, characterized in that the method comprises the following steps prior to the finishing of the component which provides the component with its definitive shape:

preparing a steel characterized in that the composition thereof is, in percentages by weight:

C=0.18-0.30%

Co=5-7%

Cr=2-5%

Al=1-2%

Mo+W/2=1-4%

V=trace levels—0.3%

Nb=trace levels—0.1%

B=trace levels—50 ppm

Ni=10.5-15% with Ni≧7+3.5 Al

Si=trace levels—0.4%

Mn=trace levels—0.4%

Ca=trace levels—500 ppm

Rare earth elements=trace levels—500 ppm

Ti=levels—500 ppm

O=trace levels—200 ppm if the steel is obtained by means of powder metallurgy, or trace levels—50 ppm if the steel is obtained by means of production in air or under vacuum from liquid metal

N=trace levels—100 ppm

S=trace levels—50 ppm

Cu=trace levels—1%

P=trace levels—200 ppm

the remainder being iron and inevitable impurities resulting from the production operation;

forging the steel;

a softening tempering operation at 600-675° C. for from 4 to 20 hours followed by cooling in air;

solution heat treating at 900-1000° C. for at least 1 hour, followed by cooling in oil or air which is sufficiently rapid to prevent the precipitation of intergranular carbides in the austenite matrix; and

hardening ageing at 475-600° C. for from 5-20 h,

wherein Rm at ambient temperature is between 2200 and 2350 MPa.

2. Mechanical component according to claim 1 , characterized in that the component is an engine transmission shaft.

3. Mechanical component according to claim 1 , wherein the hardening ageing is from 490-525° C. for from 5-20 h.

4. Mechanical component according to claim 3 , characterized in that the component is an engine transmission shaft.

5. Mechanical component according to claim 1 , wherein the method further comprises a cryogenic processing operation at −50° C. or lower in order to convert all the austenite into martensite, the temperature being 200° C. or more lower than Ms, at least one of the processing operations lasting at least 2 hours, wherein the cryogenic processing operation is carried out between the cooling in oil or air and the hardening ageing.

6. Mechanical component according to claim 5 , wherein the cryogenic processing operation is at −80° C. or lower.

7. Mechanical component according to claim 6 , wherein the cryogenic processing operation is followed by stress relieving operation.

8. Mechanical component according to claim 1 , wherein Rm is about 1800 MPa at 400° C.

9. Mechanical component according to claim 1 , wherein Rp0.2 is from 1959 to 2135 MPa.

10. Mechanical component according to claim 1 , wherein C=0.20-0.25%.

Assignments (4)
CHANGE OF ADDRESS Recorded Dec 28, 2022
From: AUBERT & DUVAL
To: AUBERT & DUVAL
Reel/Frame 062231/0342 →
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 May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
CHANGE OF NAME Recorded May 16, 2018
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 045825/0950 →