U.S. patent number 3,607,250 [Application Number 05/002,432] was granted by the patent office on 1971-09-21 for high-temperature alloys and articles.
This patent grant is currently assigned to Blaw-Knox. Invention is credited to Ray H. English, Martin N. Ornitz.
United States Patent |
3,607,250 |
English , et al. |
September 21, 1971 |
HIGH-TEMPERATURE ALLOYS AND ARTICLES
Abstract
A new high-temperature alloy having high creep resistance and
improved load fracture properties at temperatures of 2,000.degree.
F. and above comprising about 0.35% to 0.75% carbon, at least about
0.2% manganese, up to about 2% silicon, about 40% to 55% nickel,
about 22% to 33% chromium, about 4% to 6% tungsten, about 1% to
4.5% cobalt and the balance iron with usual impurities in ordinary
amounts.
Inventors: |
English; Ray H. (McCandless
Township, Allegheny County, PA), Ornitz; Martin N.
(Pittsburgh, PA) |
Assignee: |
Blaw-Knox (N/A)
|
Family
ID: |
21700735 |
Appl.
No.: |
05/002,432 |
Filed: |
January 12, 1970 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
|
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623746 |
Mar 16, 1967 |
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Current U.S.
Class: |
420/454;
420/581 |
Current CPC
Class: |
C22C
19/053 (20130101) |
Current International
Class: |
C22C
19/05 (20060101); C22c 019/00 (); C22c
019/04 () |
Field of
Search: |
;75/170,171
;148/32,32.5 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Lovell; Charles N.
Parent Case Text
This application is a continuation-in-part of out copending
application Ser. No. 623,746 filed Mar. 16, 1967 now abandoned.
Claims
We claim:
1. An alloy having new creep and load fracture properties at very
high temperature in the range of 2,000.degree. F. and above
consisting of about 0.35% to 0.75% carbon, at least about 0.2%
manganese, up to about 2% silicon, about 40% to 55% nickel, about
27% to 33% chromium, about 4% to 6% tungsten, about 2% to 4.5%
cobalt and the balance iron with ordinary impurities in usual
amounts.
2. The alloy as claimed in claim 1 wherein the carbon is 0.45%,
manganese 1.25%, silicon 0.75%, nickel 48%, chromium 27%, tungsten
5%, cobalt 3% and the balance iron with ordinary impurities in
usual amounts.
3. A refractory metal furnace part having high creep and load
fracture properties cast from an alloy consisting of about 0.35% to
0.75% carbon, at least about 0.2% manganese, up to about 2%
silicon, about 40% to 55% nickel, about 27% to 33% chromium, about
4% to 6% tungsten, about 2% to 4.5% cobalt and the balance iron
with usual impurities in ordinary amounts and characterized by
creep resistance, corrosion resistance and improved load fracture
properties at operating temperatures in the range of 2,000.degree.
F. in the as cast condition without heat treatment, age hardening
and like treatments.
Description
This invention relates to high-temperature alloys and articles and
particularly to high-temperature alloys having a unique balance of
load resistance to elongation at elevated temperatures. There has
been a continual demand for alloys having high creep resistance.
The fields of high-temperature furnace components such as radiant
tubes and shafts, gas turbines, jet engines, crucibles, internal
combustion engines and turbo superchargers are but a few of the
fields in which such materials are useful. Various alloys have
heretofore been proposed having various compositions and areas of
usefulness but in general all such alloys have some drawbacks. One
alloy which has been successfully used in a variety of instances
which high load resistance and creep were essential, particularly
in combination with resistance to corrosion in oxygen, is that
disclosed and claimed in out U.S. Pat. No. 2,540,107 and sold by
Blaw-Knox Company under the trademark "22H."
The present alloy is markedly superior to 22H in limiting creep
stress values at 2,000.degree. F. and in increasing the load
fracture time at temperatures above 2,100.degree. F. For example at
2,000.degree. F. the limiting creep stress (1 percent elongation in
10,000 hours) for 22H is 1,050 p.s.i. whereas for the present alloy
it is 1,600 p.s.i. At 2,100.degree. F., at a 700 p.s.i. load the
sample of 22H failed at 1,200 hours whereas the present alloy was
tested for 3,080 hours and still remained intact when the test was
stopped. The 1,900.degree. F. limiting creep stress to produce 1
percent elongation in 10,000 hours for 22H is 1,200 p.s.i. and for
the present alloy is 2,000 p.s.i.
Properties which are important in materials for this purpose are
resistance to oxidation and stability of shape under load. As the
temperatures increase, metals tend to burn more readily and also to
have greater plastic deformation or creep over a period of time.
Many metals which might be quite strong at high temperatures cannot
be exposed to even mildly corrosive or oxidizing atmospheres at
such temperatures without rapidly being consumed, while other
compositions which are resistant to burning do not have
rigidity.
Corrosion of alloys in hot gases is dependent, of course, on the
atmosphere as well as the alloy. The behavior of metals maintained
constantly under high temperature is characteristically a
progressive burning away of the surface at a substantially constant
rate, which is measured in inches penetration per year.
The behavior of specimen metals under constant stress below the
elastic limit at high temperature is characterized by three stages
of deformation, namely:
1. A period of internal stress distribution taking place in a
relatively short time and characterized by an initial high and
diminishing rate of deformation. This stage is made up of elastic
and plastic flow.
2. A period of constant rate of deformation lasting over long
periods of time. This phenomenon is known to metallurgists as
creep, and is usually measured in terms of elongation per hour
under a given tension, although it is equally characteristic of
other deformations and we prefer to compare specimens in bending
rather than in direct tension, and to express creep in terms of
angular deflections per hour.
3. A final increasing rate of deformation leading to necking and
failure.
The rate of deformation per unit time in stage 2 is a suitable
measure of rigidity or permanence of shape of the material at the
load and temperature. It is customary to select the allowable unit
stress for a particular metal at a particular high temperature on
the basis of the creep considered permissible at that temperature.
The time to reach and pass through the different stages to creep is
of importance and is influenced by the material, temperature and
load or unit stress.
Our alloy has high mechanical strength, low creep and also high
resistance to corrosion at very high temperatures in the as cast
condition without heat treatment, age hardening or any of the like
treatments. The material can, however, be further worked and
treated if desired. Our alloy is equal or superior in these
respects to other known alloys at lower temperatures, its relative
advantages and superiority become strikingly apparent at the higher
temperatures for which it is peculiarly adaptable; e.g. at
temperatures such as 2,300.degree. F. It is an alloy of nickel
containing as essential alloying constituents chromium, tungsten,
cobalt and carbon, the balance being substantially iron along with
the controlled amounts of manganese and silicon and the usual
impurities in ordinary amounts. We have found that cobalt
additions, previously considered deleterious, are in the narrow
range of out invention actually beneficial. Peculiarly higher
amounts of cobalt causes embrittlement of the alloy on cooling from
high temperatures while lower amounts reduce the corrosion
resistance without affecting any significant improvement in other
areas.
The alloy of the present would have in a preferred embodiment the
following composition:
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Carbon 0.45 Manganese 1.25 Silicon 0.75 Nickel 48.0 Chromium 27.0
Tungsten 5.0 Cobalt 3.0 Iron Balance with usual impurities
__________________________________________________________________________
Our alloy may, however, extend over a range and still retain its
desirable and unique characteristics. Such a range would be as
follows:
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C 0.35 0.75 Mn-at least 0.2 Si-up to about 2.0% Ni 40 55 Cr 22 33
Co 1 4.5 W 4 6 Fe Balance with usual impurities
__________________________________________________________________________
The uniqueness of the invention can perhaps best be understood by
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reference to the following test data comparing 22H with the present
alloy:
TABLE I
Stress Rupture Data
Temp. Stress Creep Rate
__________________________________________________________________________
22H 2,100.degree. F. 700 p.s.i. 0.0024%/hr. 1,270 hrs. to fracture
Alloy of 2,100.degree. F. 700 p.s.i. 0.0003%/hr. 3,080 hrs. No
Invention fracture- test discontinued
__________________________________________________________________________
##SPC1##
A series of tests were run to check the effect of varying cobalt
concentrations while maintaining the balance of alloy substantially
constant. The results are tabulated below and are illustrated in
the
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accompanying Figure:
TABLE III
Co Temp. Cantilever Load Radians/hr.
__________________________________________________________________________
2,200 500 0.000100 2.4 2,200 500 0.000044 4.5 2,200 500 0.000050
5.8 2,200 500 0.000056 2.0 2,200 500 0.000050
__________________________________________________________________________
While we have described and disclosed a preferred embodiment of our
invention, it will be understood that this invention may be
otherwise embodied within the scope of the following claims.
* * * * *