Measuring and testing – Specimen stress or strain – or testing by stress or strain... – By loading of specimen
Reexamination Certificate
2000-12-22
2003-04-01
Williams, Hezron (Department: 2855)
Measuring and testing
Specimen stress or strain, or testing by stress or strain...
By loading of specimen
C073S760000, C073S789000
Reexamination Certificate
active
06539810
ABSTRACT:
BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention relates to a method for estimating tensile properties of IN718 cast HIPed material.
2. Description of the Prior Art
Inconel Alloy 718 (IN718) has the major chemistry of Ni—Fe—Cr—Cb—Mo—Ti—Al and was developed through extensive optimization studies by H. L. Eiselstein at the International Nickel Company (INCO) in the 1950's. Alloy IN718 is a precipitation hardenable nickel based alloy with high strength and ductility at temperatures up to 704° C., good corrosion resistance, ease of formability and can be welded with good resistance to strain-age cracking. Alloy IN718 was initially developed for the aerospace industry, and it has been used for jet engine and high-speed airframe parts such as wheels, buckets, spacers, and high temperature bolts and fasteners. IN718 investment cast HIPed material is a new approach in making manifold for steam delivery system in GE H technology gas turbines.
Investment casting, often called lost wax casting, is regarded as a precision casting process to fabricate near-net-shaped metal parts from almost any alloy. The most common use of investment casting in more recent history has been the production of components requiring complex, often thin-wall castings. The investment casting process normally includes the following steps: creating a wax pattern, assembling a wax pattern cluster, “investing” a cluster with ceramic stucco/slurry; de-waxing and fire molding the ceramic for strength, melting the alloy in vacuum or air; pouring molten alloy into the mold; knocking off the shell and heat treating/machining/coating operations. An HIP process (Hot Isostatic Pressing) sometimes follows the investment casting process to consolidate shrinkage porosity internal to the casting and help homogenize the structure.
GE Power Systems introduced H technology gas turbines in 1995. H technology is a platform of combined-cycle technology that integrates the gas turbine, steam turbine, and generator into a seamless system, where each component is optimized for the highest level of performance. The centerpiece of this new technology platform is an advanced closed-loop steam cooling system in the gas turbine. This cooling system permits higher firing temperature while retaining combustion temperatures at levels consistent with low emissions. This enables the new machines to operate at firing temperatures in the 2,600F class, leading to 60% net thermal efficiency and world record output for a combined-cycle unit. Unlike aircraft engines, which only have air for cooling, a combined-cycle system has a ready steam supply. The steam is captured and used for cooling in this closed-loop system. Steam is desired because it has a higher heat capacity than air. The steam cooling system uses a manifold as a critical component. However, it is difficult to make the manifold due to its complex geometry. See FIG.
1
.
Originally, manifolds were made by machining forged alloy IN718 material to the desired shape. This process can be expensive and take a long time. Other processes were investigated to reduce the cost and cycle time. One process, HIPed (Hot Isostatic Press) investment casting process, was considered. Manifolds produced by the investment cast process of alloy IN718 have lower costs, larger yields and reduced cycle time.
Forging produces a better tensile property than casting at the same grain size since forging can produce a uniform grain size distribution in the IN718 material. Casting, on the other hand, produces an IN718 material having a wide range of grain sizes. However, in order to design and form the manifold with the HIPed investment casting process, tensile strength and ductility must be considered. These properties are usually identified by ultimate tensile strength, yield strength, and elongation. However, heretofore these properties were not directly measurable for alloy IN718 products formed by the HIPed investment cast process, rendering design of the manifold difficult.
Tensile properties can be affected by many factors, such as process parameters, grain size, and temperature. Materials made by investment casting can have varied grain sizes. For example, thin sections or areas close to the mold can have fine grains, while the center of thick sections can have coarse grain size.
Due to its manufacturing history and the lack of property data, the tensile properties of cast alloy IN718 has been estimated by using the Grain Size 3 Forging—3&sgr; rule. This rule calculates the average value of forging material with grain size ASTM3 and calculates the standard deviation a, shift the average curve down by 3&sgr;, curve obtained is called −3&sgr; curve. Some skilled in the art sometimes use a different level of conservative (for example, a −2&sgr; curve) for different applications. Although, this forging rule has been used to estimate tensile properties for casting materials, estimating tensile properties of forging materials is more accurate than casting materials.
As discussed above, the forging property data having a grain size of ASTM 3 was parallel shifted down by three times its standard deviation, and the correspondent new curve was used for the design basis for the HIPed investment cast IN718 manifold. However, this rule did not provide accurate results because the same value was assumed for all grain sizes. That is, it was assumed that the tensile properties: yield strength, elongation, etc., were dependent only on temperature, not grain size. This is not accurate. Therefore, designing and forming the manifold with cast HIPed IN718 material has been difficult because of the less than accurate tensile data available.
BRIEF SUMMARY OF THE INVENTION
The invention is directed to a method to estimate the tensile properties of HIPed cast IN718 components at various grain sizes and different operating temperatures. The invention uses transfer functions to estimate ultimate tensile strength, yield strength, and elongation.
In particular, the invention is directed to a method of estimating ultimate tensile strength (UTS) of a cast HIPed IN718 component with known local grain size and operating temperature by solving the following equation:
UTS=
(238.3−19.44
×GS+
3.355
×GS
2
−0.0889×(
T−
32)+2.28×10
−5
×(
T−
32)
2
−4.39×10
−4
×GS
×(
T−
32))×7×10
6
whereby GS is the average grain size in meters, T is temperature in degree C., and UTS is in the unit of Pascal.
The invention is further directed to a method of estimating 0.2% yield strength (0.2% YS) of a cast HIPed IN718 component with known local grain size and operating temperature by solving the following equation:
0.2%
YS=
(219.2−23.38
×GS+
4.447
×GS
2
−0.089×(
T−
32))×7×10
6
whereby GS is the average grain size in meters, T is temperature in degree C., and 0.2% YS is in the unit of Pascal.
The invention is further directed to a method of determining the 0.02% yield strength (0.02% YS) of a cast HIPed IN718 component with known local grain size and operating temperature by solving the following equation:
0.02%
YS=
(130−25.04
×GS+
5.1
×GS
2
+5.56×10
−3
×(
T−
32)−4.44×10
−4
×GS
×(
T−
32))×7×10
6
whereby GS is the average grain size in meters, T is temperature in degree C., and 0.02% YS is in the unit of Pascal.
In addition, the invention is directed to a method of determining the elongation (elong.) of a cast HIPed IN718 component with known local grain size and operating temperature by solving the following equation:
elong.=139.3+1.3
×GS−
1.421
×GS
2
−0.128×(
T−
32)+1.57×10
−3
GS
×(
T−
32)
whereby GS is the average grain size in meters, T is temperature in degree C., and elongation is in the unit of percentage %.
The estimates obtained from the transfer functions ca
Banner & Witcoff , Ltd.
General Electric Company
Harrison Monica D.
Williams Hezron
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