Patent Application
20230287551
This patent application claims the benefit and priority of Chinese Patent Application No. 202210241473.5, filed with the China National Intellectual Property Administration on Mar. 11, 2022, the disclosure of which is incorporated by reference herein in its entirety as part of the present application.
The present disclosure relates to the field of heat treatment of nickel-based superalloy forgings, in particular to a heat treatment method for realizing grain boundary serration in a nickel-based superalloy forging.
At present, thermal power is still the main electric power resource in the world. In order to improve thermal efficiency, thermal power is gradually developing from subcriticality to supercriticality, and then to ultra-supercriticality. The steam pressure is up to 30-35 MPa, and the steam temperature is up to 593-600° C. or higher. In high temperature, high pressure, high humidity and acidic environments, in addition to requiring high strength and high temperature resistance of valve bodies and pipe fittings, the valve bodies are further required to have excellent resistance to high temperature grain boundary corrosion and stress corrosion resistance. Inconel 617 alloy has excellent high temperature strength, plasticity, oxidation resistance, and corrosion resistance, so the alloy is often used as superheaters and reheaters in ultra-supercritical units.
However, during elevated temperature's service, because the grain boundary is a typical planar defect, it will produce many failure behaviors such as: intergranular corrosion, stress corrosion, high temperature creep, stress rupture, and fatigue failure, which will endanger production safety seriously. Therefore, how to improve the properties of alloys by regulating grain boundaries has always been paid attention to by researchers inside and outside of China.
Serrated grain boundary is a special grain boundary that improves grain boundary properties by changing the grain boundary structure—transforming a straight grain boundary into a serrated grain boundary. It should be pointed out that the formation mechanism of the serrated grain boundary is still unclear at present, and the formation mechanism is different in different alloy systems. However, it is clear that the grain boundary energy of the serrated grain boundary is lower than that of the straight random grain boundary, which can effectively improve the segregation of elements at the grain boundary and the precipitation morphology of carbides at the grain boundary. Thus, the grain boundary corrosion, intergranular crack initiation and propagation are inhibited, and the creep fatigue and welding properties of the alloy are improved.
Therefore, from the perspective of grain boundaries, without changing the alloy composition and without affecting the mechanical properties of the material, it is especially important that the straight grain boundaries in the forgings are transformed into serrated grain boundaries through a simple heat treatment method to improve the service performance of the material. This patent realizes grain boundary serration in nickel-based superalloy forgings through an appropriate heat treatment process, so as to achieve the objective of grain boundary regulation, which is of great significance to further improve the alloy durability, creep, fatigue and welding properties.
In view of the above deficiencies in the prior art, the present disclosure provides a heat treatment method for realizing grain boundary serration in a nickel-based superalloy forging, which can realize the grain boundary serration in the nickel-based superalloy forging.
To achieve the above objective, the present disclosure provides a heat treatment method for realizing grain boundary serration in a nickel-based superalloy forging, including introducing a serrated grain boundary into a microstructure of the nickel-based superalloy forging by using a heat treatment method for controlling a cooling rate, where the heat treatment method for controlling a cooling rate includes the following steps:
Preferably, a designation of the nickel-based superalloy forging is Inconel 617.
Preferably, the heat treatment method for controlling a cooling rate is carried out in a heat treating furnace capable of controlling the cooling rate.
Preferably, the heat treatment method for controlling a cooling rate promotes grain boundary segregation of Mo, Cr and C in the nickel-based superalloy forging during controlled cooling, produces plate-like M6C and M23C6 at the grain boundary, has a dragging effect on the migration of the grain boundary, and forms the serrated grain boundary between grains.
Preferably, an average amplitude of the serrated grain boundary in the nickel-based superalloy forging may be greater than 1 μm.
Preferably, room temperature mechanical properties of the nickel-based superalloy forging are tested with reference to GB/T 228.1 Metallic Materials—Tensile Testing—Part 1: Method of Test at Room Temperature.
The present disclosure has the following beneficial effects due to the adoption of the above technical solution:
Preferred examples of the present disclosure are given and described below in detail with reference to
As shown in
A designation of the nickel-based superalloy forging is Inconel 617.
The heat treatment method for controlling a cooling rate is carried out in a heat treating furnace capable of controlling the cooling rate.
The heat treatment method for controlling a cooling rate promotes grain boundary segregation of Mo, Cr and C in the nickel-based superalloy forging during controlled cooling, produces plate-like M6C and M23C6 at the grain boundary, has a dragging effect on the migration of the grain boundary, and forms the serrated grain boundary between grains.
An average amplitude of the serrated grain boundary in nickel-based superalloy forging is greater than 1 μm.
Room temperature mechanical properties of the nickel-based superalloy forging are tested with reference to GB/T 228.1 Metallic Materials—Tensile Testing—Part 1: Method of Test at Room Temperature.
In the present example, the heat treatment for controlling a cooling rate (hereinafter referred to as: controlled cooling heat treatment) is conducted on the Inconel 617 nickel-based superalloy forging after forging and forming. Some straight random grain boundaries were transformed into serrated grain boundaries, and the average amplitude of the serrated grain boundary was 1 μm. A specific implementation process was as follows:
After the Inconel 617 nickel-based superalloy forging in this example was subjected to the controlled cooling heat treatment (holding for 1 h at 1,200° C., cooling to 750° C. at a cooling rate of 10° C./min and holding for 8 h, taking out and cooling to room temperature with water), some straight grain boundaries were transformed into serrated grain boundaries. The average amplitude of the serrated grain boundary was 1.5 μm. The room temperature mechanical properties of the alloy were not influenced while introducing the serrated grain boundaries.
Table 1. Mechanical properties of Inconel 617 nickel-based superalloy in the first controlled cooling heat treatment
It was basically the same as Example 1. There were the following differences: the controlled cooling heat treatment process was holding for 1.5 h at 1,100° C., cooling to 700° C. at a cooling rate of 6° C./min, holding for 6 h, taking out and cooling to room temperature with water; and the average amplitude of the serrated grain boundary in the alloy was 1.1 μm.
The Inconel 617 nickel-based superalloy with the same chemical composition as in Example 1 was used for controlled cooling heat treatment. The alloy was placed in a heat treating furnace, held for 1.5 h at 1,100° C., cooled to 700° C. at a cooling rate of 6° C./min, held for 6 h, taken out and cooled to room temperature with water. The grain boundary structure was analyzed by SEM, and the results showed that the average amplitude of the serrated grain boundary in the alloy was 1.1 μm. The Inconel 617 nickel-based superalloy forging after controlled cooling heat treatment was processed into M10 threaded rods, and the mechanical properties were tested with reference to GB/T 228.1 Metallic Materials—Tensile Testing—Part 1: Method after of Test at Room Temperature. The results are shown in Table 2.
Table 2. Mechanical properties of Inconel 617 nickel-based superalloy in the second controlled cooling heat treatment
After the Inconel 617 nickel-based superalloy forging in this example was subjected to the controlled cooling heat treatment (holding for 1.5 h at 1,100° C., cooling to 700° C. at a cooling rate of 6° C./min and holding for 6 h, taking out and cooling to room temperature with water), some straight grain boundaries were transformed into serrated grain boundaries. The average amplitude of the serrated grain boundary was 1.1 μm. The room temperature mechanical properties of the alloy were not influenced while introducing the serrated grain boundaries.
It was basically the same as Example 1. There were the following differences: the controlled cooling heat treatment was holding for 1 h at 1,150° C., cooling to 650° C. at a cooling rate of 8° C./min, holding for 4 h, taking out and cooling to room temperature with water; and the average amplitude of the serrated grain boundary in the alloy was 1.2 μm.
The Inconel 617 nickel-based superalloy with the same chemical composition as in Example 1 was used for controlled cooling heat treatment. The alloy was placed in a heat treating furnace, held for 1 h at 1,150° C., cooled to 650° C. at a cooling rate of 8° C./min, held for 4 h, taken out and cooled to room temperature with water. The grain boundary structure was analyzed by SEM, and the results showed that the average amplitude of the serrated grain boundary in the alloy was 1.2 μm. The Inconel 617 nickel-based superalloy forging after controlled cooling heat treatment was processed into M10 threaded rods, and the mechanical properties were tested with reference to GB/T 228.1 Metallic Materials—Tensile Testing—Part 1: Method after of Test at Room Temperature. The results are shown in Table 3.
Table 3. Mechanical properties of Inconel 617 nickel-based superalloy in the third controlled cooling heat treatment
After the Inconel 617 nickel-based superalloy forging in this example was subjected to the controlled cooling heat treatment (holding for 1 h at 1,150° C., cooling to 650° C. at a cooling rate of 8° C./min and holding for 4 h, taking out and cooling to room temperature with water), some straight grain boundaries were transformed into serrated grain boundaries. The average amplitude of the serrated grain boundary was 1.2 μm. The room temperature mechanical properties were not influenced while introducing the serrated grain boundaries.
The results of the examples show that the objective of the present disclosure can be achieved within the range of the technical parameters of the technical solution of the present disclosure. Some straight grain boundaries of the forging are transformed into serrated grain boundaries, and room temperature mechanical properties are not influenced while introducing the serrated grain boundaries.
The present disclosure has been described in detail above with reference to the accompanying drawings and examples, and those skilled in the art can make various modifications to the present disclosure according to the above description. Therefore, some details in the examples should not be construed as limiting the present disclosure, and the present disclosure will take the scope defined by the appended claims as the protection scope of the present disclosure.
| Number | Date | Country | Kind |
|---|---|---|---|
| 202210241473.5 | Mar 2022 | CN | national |
