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Heat resistant super alloy and its use

a super alloy and heat resistance technology, applied in the direction of engines, mechanical equipment, machines/engines, etc., can solve the problems of relative unfavorable costs of alloys, and achieve the effect of reducing costs and improving vibration stress properties

Inactive Publication Date: 2005-10-27
BORGWARNER INC POWERTRAIN TECHN CENT
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0004] It is an object of the invention to provide an alloy having improved vibration stress properties and, if possible, can be made at reduced costs.

Problems solved by technology

This renders this alloy relative unfavorable as to costs.

Method used

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  • Heat resistant super alloy and its use
  • Heat resistant super alloy and its use

Examples

Experimental program
Comparison scheme
Effect test

example 2

[0029] A second alloy of the following composition (in percent in weight) has been used, the remainder being nickel:

CCrAlTiMoWNbBZrHfLa0.099.55.52.52131.750.0250.080.450.005

[0030] This resulted, thus, in a proportion of nickel of 65.1 percent in weight. It should be pointed out that this alloy had, therefore, a total contents of hafnium and lanthanum of 0.455 percent in weight, a total contents of tungsten and molybdenum of 15 percent in weight, and a total contents of aluminum and titanium of 8 percent in weight, the sum of the contents of titanium, niobium and aluminum totaling 9.75 percent in weight. Thus, no tantalum had been used in this example.

[0031] Subsequently, the alloy thus formed was subjected to the same tests as in example 1 wherein the elasticity was slightly improved as compared with example 1.

example 3

[0032] A third alloy of the following composition (in percent in weight) has been used, the remainder being nickel:

CCrAlTiMoWNbBZrHfLaTa0.128.54.53.52.7511.52.30.010.030.60.0040.6

[0033] This resulted, thus, in a proportion of nickel of 65.586 percent in weight. It should be pointed out that this alloy had, therefore, a total contents of hafnium and lanthanum of 0.604 percent in weight, a total contents of tungsten and molybdenum of 15 percent in weight, and a total contents of aluminum and titanium of 8 percent in weight, the sum of the contents of titanium, niobium and aluminum totaling 10 percent in weight.

[0034] The tests carried as in example 1 showed slightly increased ductility. When, however, a long-time test in a corrosive atmosphere (combustion gas of a gasoline engine at about 900° C.) was carried out, a slightly reduced corrosion resistance was found as compared to a similar test of the samples of examples 1 and 2.

example 4

[0035] This example, after the previous good results with alloys of the examples 1 to 3, served mainly the purpose to be able to assess the tendency resulting from somewhat more extreme proportions of the elements. Therefore, an alloy of the following composition (in percent in weight) was used, the remainder being nickel:

CCrAlTiMoWNbBZrHfLa0.128.54.53.52.7511.52.30.010.030.60.004

[0036] This resulted, thus, in a proportion of nickel of 67.45 percent in weight. It should be pointed out that this alloy had, therefore, a total contents of hafnium and lanthanum of 0.82 percent in weight, a total contents of tungsten and molybdenum of 12 percent in weight, and a total contents of aluminum and titanium of 8 percent in weight, the sum of the contents of titanium, niobium and aluminum totaling 9.5 percent in weight. In this example too, one had abstained from using tantalum.

[0037] It should be stated that the samples produced from this alloy did not lead to any additional improvement as ...

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Abstract

A heat resistant super alloy suffices the following conditions: carbon0.01-0.2percent in weightchromium8-10percent in weightaluminum4-6percent in weighttitanium2-4percent in weightmolybdenum1.5-2.8percent in weighttungsten10-13.5percent in weightniobium1.5-2.5percent in weightboron0 < B ≦ 0.04percent in weightzircon0 < Zr ≦ 0.15percent in weightthe contents of hafnium and lanthanum together amounts to 0 < Hf + La ≦ 1.5 percent in weight, optionally traces of tantalum, the remainder being nickel. Such an alloy is preferably used for turbine wheels and particularly for turbochargers.

Description

FIELD OF THE INVENTION [0001] The present invention relates to a heat resistant super alloy, particularly on a nickel basis. Such alloys are used in turbines for a variety of components, but also for other parts, for example for components of furnaces or appliances to be installed in furnaces and kilns. The invention relates also to a special use of this super alloy. BACKGROUND OF THE INVENTION [0002] As mentioned above, a variety of alloys is known for similar purposes, as may be seen from U.S. Pat. Nos. 3,466,171; 4,236,921 or 5,439,640. The alloy MAR 247 LC on the market is also known and is particularly used in turbine wheels for achieving higher vibration strength. It consists of eleven elements, among them a large amount of cobalt, but also relative large proportions of tantalum and hafnium. This renders this alloy relative unfavorable as to costs. [0003] In the field of use mentioned above, it will generally be a high corrosion resistance with respect to hot gases, a high ser...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): C22C19/05F01D5/28
CPCC22C19/057F05D2300/10F05C2203/00F01D5/28
Inventor SCHALL, GERALD
Owner BORGWARNER INC POWERTRAIN TECHN CENT