US3455152A - Method for quickly determining hydrogen embrittlement of metallic parts - Google Patents
Method for quickly determining hydrogen embrittlement of metallic parts Download PDFInfo
- Publication number
- US3455152A US3455152A US607447A US3455152DA US3455152A US 3455152 A US3455152 A US 3455152A US 607447 A US607447 A US 607447A US 3455152D A US3455152D A US 3455152DA US 3455152 A US3455152 A US 3455152A
- Authority
- US
- United States
- Prior art keywords
- strip
- parts
- hydrogen
- hydrogen embrittlement
- test
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229910052739 hydrogen Inorganic materials 0.000 title description 22
- 239000001257 hydrogen Substances 0.000 title description 22
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 title description 19
- 238000000034 method Methods 0.000 title description 6
- 238000012360 testing method Methods 0.000 description 23
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical group [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 11
- 239000000956 alloy Substances 0.000 description 4
- 150000002431 hydrogen Chemical class 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 101100008046 Caenorhabditis elegans cut-2 gene Proteins 0.000 description 1
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 229910000700 SAE 1075 Inorganic materials 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- -1 for example Chemical compound 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000005554 pickling Methods 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N33/00—Investigating or analysing materials by specific methods not covered by groups G01N1/00 - G01N31/00
- G01N33/20—Metals
- G01N33/204—Structure thereof, e.g. crystal structure
- G01N33/2045—Defects
Definitions
- Hydrogen embrittlement of ferrous and ferrous alloy parts results either in the inability to withstand dynamic shock or the propagation of existing fissures when the part is put under load, and such embrittlement requires that the hydrogen be removed or the part be rejected. It is therefore necessary to determine whether embrittlement is present, but while earlier work on this subject has shown that hydrogen embrittlement can be measured by a ductility or static load test of notched specimens, no practical way has been known to measure embrittlement by a simple, quick and inexpensive test which can be used to test production plating lots of ferrous parts.
- FIG. 1 is a plan view of a preferred form of test strip according to the invention.
- FIG. 2 is a side view of the strip shown in FIG 1;
- FIGS. 3 and 4 are, respectively, plan views of two other forms of test strips according to the invention.
- test strips have the value that, having gone through the same embrittling and baking operations as the parts, they will quickly tell the degree of hydrogen remaining in the parts.
- the exact correlation between the time of breaking of the test strips and failure of the parts from hydrogen embrittlement must be determined by actual test experience.
- the shape of the parts, any sharp discontinuities formed in them, the thicknesses of various sections, the chemistry of the material, and the stress to which the parts will be subjected in use vary greatly, and correlation between the life of the standardized test strip and the probability of part breakage must be determined by testing the test strips against actual times to part failure. In general, it may be said that the time to failure of a test strip is inversely proportional to the amount or residual hydrogen remaining in the parts.
- the test apparatus comprises bendable test strips and a rack for holding the strips immobile in U-shaped condition after the bath and baking cycles.
- Test strips which have proved to be successful are shown in FIGS. 1 to 4 and it will be seen that each compr-ises an elongated, narrow, thin, normally fiat strip of ferrous metal notched or otherwise weakened at its center.
- the preferred strip construction shown in FIGS. 1 and 2 has a U-shaped cut 2 leaving a tab 4 slightly bent outwardly from the plane of the test strip.
- the strip of FIG. 3 has a partially sheared out button 6 at the same location as the tab 4, while the strip shown in FIG. 4 has a V-shaped edge notch 8 midway of the length of the strip.
- the rack which completes the test apparatus comprises a fiat board 10 having two parallel grooves 12, 14 in its one surface which are spaced apart by such a distance that when the ends of a test strip are placed in the grooves the strip will be bent to substantially U-shape as shown in FIG. 5.
- parallel strips or the like could be used instead of grooves.
- Test strips having, respectively, the three notch types are sensitive indicators, but strips having the U-shape notch of FIGS. 1 and 2 are preferred because the notch may be produced more uniformly.
- a test strip which has proved to be successful is 7 /2 inches long, /2 inch wide and .022 inch thick, having the U-shaped cut and tab of FIGS. 1 and 2, the tab being /s inch wide, the material of the strip being 70/80 carbon steel hardened and tempered to a Rockwell 30 N scale (equivalent to Rockwell C 55/56 on the A scale).
- Such a strip is used with a rack having grooves which are spaced 3 inches apart.
Landscapes
- Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Health & Medical Sciences (AREA)
- Medicinal Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Food Science & Technology (AREA)
- Crystallography & Structural Chemistry (AREA)
- Physics & Mathematics (AREA)
- Analytical Chemistry (AREA)
- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- General Physics & Mathematics (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Description
.INVENTOR JAMES H. MAKER Jaw/ M1; JWMMM J. H. MAKER METHOD FOR QUICKLY DETERMINING HYDROGEN EMBRITTLEMENT OF METALLIC PARTS Filed Jan. 5, 1967 July 15, 1969 ATTORNEYS United States Patent 3,455,152 METHOD FOR QUICKLY DETERMINING HYDRO- GEN EMBRITTLEMENT OF METALLIC PARTS James H. Maker, Bristol, Conn., assignor to Associated Spring Corporation, Bristol, Conn., a corporation of Delaware Filed Jan. 5, 1967, Ser. No. 607,447 Int. Cl. G01n 17/00 US. Cl. 73-87 1 Claim ABSTRACT OF THE DISCLOSURE Method for testing for hydrogen embrittlement of ferrous parts which have been subjected to a process or cycle which causes the part to absorb hydrogen such as, for example, an electroplating bath, an acid cleaning bath, a pickling bath or the like, any or all of which are hereinafter referred to as a bath, and for the efficiency of a subsequent baking operation to remove hydrogen, in which an elongated ferrous strip, which is weakened at its midpoint, is subjected to the same bath and subsequent baking operation, and is then bent to U-shape and held in that condition to failure, the time to failure being measured and being inversely indicative of the extent of hydrogen embrittlement of the parts.
Summary of the invention Hydrogen embrittlement of ferrous and ferrous alloy parts results either in the inability to withstand dynamic shock or the propagation of existing fissures when the part is put under load, and such embrittlement requires that the hydrogen be removed or the part be rejected. It is therefore necessary to determine whether embrittlement is present, but while earlier work on this subject has shown that hydrogen embrittlement can be measured by a ductility or static load test of notched specimens, no practical way has been known to measure embrittlement by a simple, quick and inexpensive test which can be used to test production plating lots of ferrous parts.
It has been the principal object of the invention to provide such a test which will be simple to perform, which can be performed simultaneously with the processing and baking of springs or other parts, which will accurately measure the degree of hydrogen embrittlement due to the bath, the efficiency of the baking cycle in removing hydrogen, and which will provide results very quickly, thus permitting additional baking of the springs if this is required.
When springs or other parts made of a ferrous or ferrous alloy material are subjected to a process which causes absorption of hydrogen with consequent embrittlement, such as a bath as herein described, the hydrogen is conventionally wholly or partially removed by baking. It is desirable and necessary to know quickly the extent of residual embrittlement after baking in order to subject the parts to additional baking if this is required, and in accordance with the invention it is proposed to measure hydrogen absorption by forming a strip of standard predetermined dimensions, structure and composition subjecting this to the same bath and baking oven as the springs or other parts, then placing the strip under stress by bending it through a pre-determined arc and measuring the time to fracture, which I have determined to be inversely proportional to the degree of embrittlement.
Description of the drawings FIG. 1 is a plan view of a preferred form of test strip according to the invention;
FIG. 2 is a side view of the strip shown in FIG 1;
FIGS. 3 and 4 are, respectively, plan views of two other forms of test strips according to the invention, and
3,455,152 Patented July 15, 1969 Description of the invention In carrying out the invention there are first provided elongated flexible test strips of substantially identical construction and physical characteristics, preferably formed of SAE 1075 and carefully standardized with respect to chemical composition, hardness, shape and size, and size and sharpness of the notch forming the weakened center section. One or more of these strips is subjected to the same bath and baking operations as the parts, and then bent to substantially U-shape and held in this condition to failure. The time to failure from completion of the bath cycle, or the baking cycle if there is one, is measured and is substantially inversely proportional to the degree of hydrogen embrittlement of the parts. The test strips have the value that, having gone through the same embrittling and baking operations as the parts, they will quickly tell the degree of hydrogen remaining in the parts. The exact correlation between the time of breaking of the test strips and failure of the parts from hydrogen embrittlement must be determined by actual test experience. The shape of the parts, any sharp discontinuities formed in them, the thicknesses of various sections, the chemistry of the material, and the stress to which the parts will be subjected in use vary greatly, and correlation between the life of the standardized test strip and the probability of part breakage must be determined by testing the test strips against actual times to part failure. In general, it may be said that the time to failure of a test strip is inversely proportional to the amount or residual hydrogen remaining in the parts.
The test apparatus provided by the invention comprises bendable test strips and a rack for holding the strips immobile in U-shaped condition after the bath and baking cycles. Test strips which have proved to be successful are shown in FIGS. 1 to 4 and it will be seen that each compr-ises an elongated, narrow, thin, normally fiat strip of ferrous metal notched or otherwise weakened at its center. The preferred strip construction shown in FIGS. 1 and 2 has a U-shaped cut 2 leaving a tab 4 slightly bent outwardly from the plane of the test strip. The strip of FIG. 3 has a partially sheared out button 6 at the same location as the tab 4, while the strip shown in FIG. 4 has a V-shaped edge notch 8 midway of the length of the strip. The rack which completes the test apparatus comprises a fiat board 10 having two parallel grooves 12, 14 in its one surface which are spaced apart by such a distance that when the ends of a test strip are placed in the grooves the strip will be bent to substantially U-shape as shown in FIG. 5. Obviously, parallel strips or the like could be used instead of grooves. Test strips having, respectively, the three notch types are sensitive indicators, but strips having the U-shape notch of FIGS. 1 and 2 are preferred because the notch may be produced more uniformly.
A test strip which has proved to be successful is 7 /2 inches long, /2 inch wide and .022 inch thick, having the U-shaped cut and tab of FIGS. 1 and 2, the tab being /s inch wide, the material of the strip being 70/80 carbon steel hardened and tempered to a Rockwell 30 N scale (equivalent to Rockwell C 55/56 on the A scale). Such a strip is used with a rack having grooves which are spaced 3 inches apart.
I claim:
1. The method of testing the extent of hydrogen embrittlement of a ferrous or ferrous alloy part, such as a spring, which has been subjected to a bath in which it may absorb hydrogen and then baked to remove hydrogen, which consists in subjecting to the same bath and any subsequent baking cycle as the part an elongated, narrow, thin strip of ferrous alloy material, bending the strip about its center to substantially U-shape, holding the strip in bent position to failure, and measuring the time to failure.
OTHER REFERENCES Heeren, Marlin H., Chemical & Metallurgical Engineering, p. 2-126, 127, February 1942.
References Cited UNITED STATES PATENTS 5 RICHARD C. QUEISSER, Primary Examiner JOHN K. LUNSFORD, Assistant Examiner McClure 21 1-184 Blodee 211-184 US. Cl. X.R. Jankowsky et al 7386 7386 Schaschl 73-86 10 Lander 73--15.6 X
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US60744767A | 1967-01-05 | 1967-01-05 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3455152A true US3455152A (en) | 1969-07-15 |
Family
ID=24432321
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US607447A Expired - Lifetime US3455152A (en) | 1967-01-05 | 1967-01-05 | Method for quickly determining hydrogen embrittlement of metallic parts |
Country Status (1)
Country | Link |
---|---|
US (1) | US3455152A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1984001461A1 (en) * | 1982-09-30 | 1984-04-12 | Boeing Co | Plated structure exhibiting low hydrogen embrittlement |
US4461168A (en) * | 1982-03-08 | 1984-07-24 | Masami Kobayashi | Hydrogen embrittlement tester |
US4866999A (en) * | 1988-08-18 | 1989-09-19 | Conoco Inc. | Corrosion cracking test specimen and assembly |
EP2772756A3 (en) * | 2013-02-28 | 2017-12-13 | The Boeing Company | Method and systems for determining hydrogen embrittlement. |
US10634593B2 (en) | 2017-02-17 | 2020-04-28 | Goff Omega Holdings, Llc | Testing method for hydrogen embrittlement |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2516713A (en) * | 1947-09-20 | 1950-07-25 | L F Pease Company | Vehicle top bow clamp |
US3034340A (en) * | 1960-02-17 | 1962-05-15 | Edward J Jankowsky | Electrical crack measuring device for determining metal deterioration |
US3102419A (en) * | 1960-11-18 | 1963-09-03 | Pure Oil Co | Apparatus for detecting hydrogen embrittlement |
US3196670A (en) * | 1962-02-27 | 1965-07-27 | Union Carbide Corp | Apparatus for measuring stress-rupture properties of plastics |
US3241683A (en) * | 1964-02-27 | 1966-03-22 | Miller Herman Inc | Article retainer |
-
1967
- 1967-01-05 US US607447A patent/US3455152A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2516713A (en) * | 1947-09-20 | 1950-07-25 | L F Pease Company | Vehicle top bow clamp |
US3034340A (en) * | 1960-02-17 | 1962-05-15 | Edward J Jankowsky | Electrical crack measuring device for determining metal deterioration |
US3102419A (en) * | 1960-11-18 | 1963-09-03 | Pure Oil Co | Apparatus for detecting hydrogen embrittlement |
US3196670A (en) * | 1962-02-27 | 1965-07-27 | Union Carbide Corp | Apparatus for measuring stress-rupture properties of plastics |
US3241683A (en) * | 1964-02-27 | 1966-03-22 | Miller Herman Inc | Article retainer |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4461168A (en) * | 1982-03-08 | 1984-07-24 | Masami Kobayashi | Hydrogen embrittlement tester |
WO1984001461A1 (en) * | 1982-09-30 | 1984-04-12 | Boeing Co | Plated structure exhibiting low hydrogen embrittlement |
US4866999A (en) * | 1988-08-18 | 1989-09-19 | Conoco Inc. | Corrosion cracking test specimen and assembly |
EP2772756A3 (en) * | 2013-02-28 | 2017-12-13 | The Boeing Company | Method and systems for determining hydrogen embrittlement. |
US10634593B2 (en) | 2017-02-17 | 2020-04-28 | Goff Omega Holdings, Llc | Testing method for hydrogen embrittlement |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4746858A (en) | Non destructive testing for creep damage of a ferromagnetic workpiece | |
Perttula et al. | Recrystallisation rates in austenite measured by double compression and stress relaxation methods | |
Littmann | The influence of the grinding process on the structure of hardened steel | |
SU897122A3 (en) | Method of determining mechanical stress in metallic part | |
US11788951B2 (en) | Testing method to evaluate cold forming effects on carbon steel susceptibility to hydrogen induced cracking (HIC) | |
US20040061510A1 (en) | Monitoring of corrosion induced loss of material by means of a plurality of electrical resistance measurements (field signature method, electrical resistance tomography) | |
CN110243516B (en) | Method for testing residual stress distribution in board in real time | |
Aronofsky | Evaluation of stress distribution in the symmetrical neck of flat tensile bars | |
US12072278B2 (en) | Development of control samples to enhance the accuracy of HIC testing | |
US3455152A (en) | Method for quickly determining hydrogen embrittlement of metallic parts | |
Connors | Fatigue striation spacing analysis | |
US4078417A (en) | Test panel for evaluating inspection penetrants | |
RU2516391C1 (en) | Method to determine area of plastic deformation under fracture in sample | |
Henthorne | Corrosion testing of weldments | |
Kaufman | Progress in fracture testing of metallic materials | |
US2646679A (en) | Device for bend testing sheets | |
RU2315971C1 (en) | Damage degree of object detecting method | |
US4866999A (en) | Corrosion cracking test specimen and assembly | |
US3690157A (en) | Method and apparatus for hardness testing | |
KR940004665B1 (en) | Measuring method of stress erosion sensibility of sulfide contained in thick steel plate | |
JPH0752152B2 (en) | Weld damage detection method | |
Young | Cavitation damage of stainless steel, nickel, and an aluminum alloy in water for ASTM round robin tests | |
Jankowsky et al. | A Comparison of Various Test Methods for Detecting Hydrogen Embrittlement | |
Aboutorabi et al. | Measurement of crack profile of semi-elliptical surface cracks using the AC potential technique | |
SU1037126A1 (en) | Method of estimating fatigue strength of material |