US2670624A - Apparatus for measurement of low rate deformability - Google Patents
Apparatus for measurement of low rate deformability Download PDFInfo
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- US2670624A US2670624A US153832A US15383250A US2670624A US 2670624 A US2670624 A US 2670624A US 153832 A US153832 A US 153832A US 15383250 A US15383250 A US 15383250A US 2670624 A US2670624 A US 2670624A
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/20—Investigating strength properties of solid materials by application of mechanical stress by applying steady bending forces
Definitions
- bituminous pavements are particularly characterized by their ability to undergo deformation, i. e. bend without breaking, in transmitting traffic loads to the foundation and natural sub-grade.
- bituminous paving may be regarded as an abrasion-resistant weather-impervious protective coating withstanding theinitial force of stresses which include certain longtime factors afiecting deformability. Isolated properties of penetration, softening point, etc., as commonly determined for bituminous materials, are not sufficiently informative as to the overall behavior which may be expected of a given material in actual service life.
- Fig. 1 is a side elevational view of apparatus in accordance with the invention.
- Fig. 2 is a fragmentary sectional view taken on a plane substantially indicated by line 2, Fig. 1.
- test pieces or samples are to be made up to standardized dimensions, and their deformability is then determined under standardized conditions for comparison.
- the size of test pieces varies with the kind of material to be tested, but for,
- the asphalt or bituminous material in amount of 10 per cent by weight is thoroughly mixed at 250 F. with 15 per cent by weight of limestone dust (200 mesh) and 75 per cent by weight of sand (40-80 mesh).
- the mixed material is then molded into test pieces of a fixed volume, in order to obtain a test piece density of about 2. 10,000-15,000 pounds per square inch.
- a generally desirable dimension for the test piece is a form by /2 by 5 inches. cooled in the mold, and removed, and finally is tested at a standardized temperature. As there is a rather considerable time element in the testin the temperature is to be accurately controlled, and. standardized.
- a testing temperature of F. is advantageous.
- the testing apparatus accordingly is enclosed in a temperature-control housing. This may be of general character as known, and, for
- a temperature-control chamber or housing equipped with thermostat and a controlled refrigerant source, such convenientlyias a circulating blower system and a. Dry Ice compartment in circuit with the cham-;
- spaced supports or knife edges 3 serve to support the piece to be tested T.
- An opposed knife edge memher 4 is arranged intermediate to knife edges 3 to apply pressure against the supported test piece, and this member is driven forward at a constant speed, which however is of low rate. The rate This requires pressure of.
- the test piece is of travel of the deforming knife edge may be set as appropriate for any kind of material to be tested.
- a forward feed rate of 0.07 inch per hour is particularly advantageous as afiording a generally satisiactory comparable basis of testing, to afford-direct comparison as to service performance that may be expected from the material when put into pavement usage.
- the driving of the pressure member 4 may be provided by suitable constant-drive means. m the fo'rr'nf illus trated, a low constant speed motor 6 suitably attached to the housing, has reduction gearing I, which through a pinion 8 drives a rack bar 9 in constant slow progression.
- the rackbar may be mounted to travel in guides ID on the reduction gear box or otherwise suitably supported, w with particular convenience, the pinion 8 may be of re-set or disengageable type as commercially available.
- the springheld pinion splined on the shaft [2 may be manuallyslid out of. engagement with the rack after completion of the test, and the rack may be raised back to its upper position and the pinion then be slid back into mesh.
- A' peculiarity of the connection between the pressure member 4 and the driving rack 9 is that it embodies a lost-motion connection, and the purpose is to provide a timeelment control:
- the rack member 9 may telescopingly engage into the pressure member 4, and a coil spring I4 may be interposed, whereby the rack 9 is driven down by a small amount, compressing the spring, before it efigages against the pressure member 4 and applies its pressure thereto.
- the pressure member 4 1s a bracket l carries switch l6 having contacts normally separated,- and being in an electric circuit with a time-indicator IS.
- the rack bar 9 by a bracket l9 carries an adjustable tripper for the switch.
- This may be an adjustable screw 20 which can be set such that it pushes the switch arm to make contact as the rack bar starts the ressure on the member 4.
- the time-indicator may be of the electric clock type available commercially, and as seen, it functions to indicate the time of the starting of applying of pressure to the test piece, and then when the test piece breaks and no longer opposes resistance, the spring I4 separates the pressure member 4 sufficiently from the drive and rack bar 9 to allow the switch to break contact and stop the timer clock, whereupon the total time of the application of the deformingpressure is known. And; since the rate'of movement of the rack bar is a known constant; such time measurement provides a precisioh micrometer space-traverse measure.
- test piece be molded to twice the length necessary for the spacing between the support knife edges 3, :it permits the placingof the test piece first such that the intermediate pressure knifeedge 4 strikesit midway.
- the first test then breaks the sample into two equal halves, "and each half may then be successively run through a similar test, and thus three readings on the samepiece may be had, for extreme accuracy.
- test procedure As illustrative of the test procedure:
- the ratio of distance travelled and test piece thickness may be determined with a drive rate suitable on a basis of temperature, size; etc; as appropriate for the kind of material to betested.
- a temperature control housing spaced edges therein to support a piece to be tested, a movable opposed edge member intermediate said edges, and an electric switch carried by said member, the combination of a rack bar having an end telescoping with said opposed edge member for limited movement relative thereto, an adjustable tripper carried by said rack bar for actuating said electric switch, a spring between said rack ba'rand said edge men'rber normally maintaining the tripper out of operative contact with the switch, a timing clock controlled by said switch, and means for driving said rack bar at a constant low rate of speed, said means including anaxially movable pinion for meshing and unmeshing with said rack bar, and a drive motor and reducing gearing connected to said pinion.
- a temperature control housing spaced edges therein to support apiece to be tested, a movable opposed edge member intermediate said edges, an electric switch carried by said member, a rack bar having lost-motion connection to said -opposed "edge member, an adjustable tripper carried by said rack bar for actuating said switch, a spring normally maim taining the tripper out of operating contact with the switch, a timer in circuit with said switch, and means for driving said rack bar at a constant low rate of speed.
- a temperature control housing spaced edges therein to support a piece to be tested, a movable opposed edge member intermediate said edges, means for determining the beginning and the end of movement thereof against the piece being tested, including an electric switch carried by said member, and a driving bar having lost-motion connection with said opposed edge member, together with an adjustable tripper carried by said bar for actuating said switch, and a spring normally maintaining the tripper out of operating contact with the switch, and means for driving said bar and opposed edge member at a constant low rate of speed.
- a temperature control housing spaced edges therein to support a piece to be tested, a movable opposed edge member intermediate said edges, means for determining the beginning and the end of movement thereof against the piece being tested, including a driving bar with lost-motion connection to said movable opposed edge member, and an electric switch at the lost-motion connection, means for driving said bar and opposed edge member at a constant low rate of speed, and means controlled by closing and opening of the switch by the bar movement relative to said opposed edge member for measuring the time of travel.
Description
M rch 2, 1 R. B. FARls, JR., ET AL 2,670,624
APPARATUS FOR MEASUREMENT OF LOW RATE DEFORMABILIT Y Filed April 4, 1950 CIRCUIT CONN ECTOR ELECTRIL TIMER 18 TEST PIECE latented Mar. 2,
APPARATUS FOR- MEASUREMENT OF LOW RATE DEFORMABILITY Robert B. Earis, Jr., Solon, Harley F. Hardman, Wickliffe, and Melvin M. Fink, Parma, Ohio, assignors to The Standard Oil Company, Cleveland, Ohio, a corporation of Ohio Application April 4, 1950, Serial No. 153,832
, I 4 Claims. 1
The performance of some materials which are on the order of semi-plastic or pseudo-plastic substances, that is, materials having some elasticity and slow flow or creep, cannot be determined by customary methods of tensile strength or shear-breakage testing. Their peculiar properties rather involve factors requiring a very considerable time element, as opposed to the rapid type of testing in tensile strength determinations. Also, there is a temperature factor which enters in the case of certain materials. One illustrative instance is the comparative measurement of asphalts as applicable to a determination of their characteristics for service life in pavements and the like. For instance, asphalt in exposure in pavement-usage is subjectedto stresses more particularly brought about by thermal expansion and contraction as caused by ambient temperature changes, freezing and thawing, etc. And, bituminous pavements are particularly characterized by their ability to undergo deformation, i. e. bend without breaking, in transmitting traffic loads to the foundation and natural sub-grade. In one sense, thus, bituminous paving may be regarded as an abrasion-resistant weather-impervious protective coating withstanding theinitial force of stresses which include certain longtime factors afiecting deformability. Isolated properties of penetration, softening point, etc., as commonly determined for bituminous materials, are not sufficiently informative as to the overall behavior which may be expected of a given material in actual service life. Such fundamental variables as viscosity, elasticity, and yield point enter, but extensive investigation has shown that these fundamental variables may move counter to each other with changes in temperature, etc., such that these individual characteristics are of little value in judging relative behavior of different materials. Deformation, however, embodies the essential factors to such an extent that measurement of deformability becomes more convenient and practical as a basis of comparison. The present invention accordingly provides means by which deformability, at low constant deformation rate, of asphalt, and materials generally which exhibit slow flow characteristics, may be relatively evaluated in a practical manner. 'Other objects and advantages will appear from the following description.
To the accomplishment of the foregoing and related ends, said invention then comprises the features hereinafter fully described and particularly pointed out in the claims, the following description and the annexed drawing setting forth in detail certain illustrative embodiments of the invention, these being indicative, however, of but a few of the various ways in which the principle of the invention may be employed.
In said annexed drawing:
Fig. 1 is a side elevational view of apparatus in accordance with the invention; and
Fig. 2 is a fragmentary sectional view taken on a plane substantially indicated by line 2, Fig. 1.
In the case of asphalts or bituminous materials,
it is now found that the serviceability or operatin life of the materials can best be determined in terms of maximum deformation or amount of bending at breaking. And, such testing is to be applied in terms of pressure at a constant but low rate of advance against the test piece. Test pieces or samples are to be made up to standardized dimensions, and their deformability is then determined under standardized conditions for comparison. The size of test pieces varies with the kind of material to be tested, but for,
illustration in the case of asphalts may advantageously be as follows: The asphalt or bituminous material in amount of 10 per cent by weight, is thoroughly mixed at 250 F. with 15 per cent by weight of limestone dust (200 mesh) and 75 per cent by weight of sand (40-80 mesh). The mixed material is then molded into test pieces of a fixed volume, in order to obtain a test piece density of about 2. 10,000-15,000 pounds per square inch. A generally desirable dimension for the test piece is a form by /2 by 5 inches. cooled in the mold, and removed, and finally is tested at a standardized temperature. As there is a rather considerable time element in the testin the temperature is to be accurately controlled, and. standardized. In the case of bituminous materials for paving applications, we have found that a testing temperature of F. is advantageous. The testing apparatusaccordingly is enclosed in a temperature-control housing. This may be of general character as known, and, for
instance we desirably employ a temperature-control chamber or housing equipped with thermostat and a controlled refrigerant source, such convenientlyias a circulating blower system and a. Dry Ice compartment in circuit with the cham-;
her. And, within the chamber 2, Fig. 1, spaced supports or knife edges 3 serve to support the piece to be tested T. An opposed knife edge memher 4 is arranged intermediate to knife edges 3 to apply pressure against the supported test piece, and this member is driven forward at a constant speed, which however is of low rate. The rate This requires pressure of.
The test piece is of travel of the deforming knife edge may be set as appropriate for any kind of material to be tested. In the case of paving asphalts, we have found that a forward feed rate of 0.07 inch per hour is particularly advantageous as afiording a generally satisiactory comparable basis of testing, to afford-direct comparison as to service performance that may be expected from the material when put into pavement usage. The driving of the pressure member 4 may be provided by suitable constant-drive means. m the fo'rr'nf illus trated, a low constant speed motor 6 suitably attached to the housing, has reduction gearing I, which through a pinion 8 drives a rack bar 9 in constant slow progression. The rackbar may be mounted to travel in guides ID on the reduction gear box or otherwise suitably supported, w with particular convenience, the pinion 8 may be of re-set or disengageable type as commercially available. For instance, as in Fig. 2, the springheld pinion splined on the shaft [2 may be manuallyslid out of. engagement with the rack after completion of the test, and the rack may be raised back to its upper position and the pinion then be slid back into mesh. A' peculiarity of the connection between the pressure member 4 and the driving rack 9 is that it embodies a lost-motion connection, and the purpose is to provide a timeelment control: For instance, the rack member 9 may telescopingly engage into the pressure member 4, and a coil spring I4 may be interposed, whereby the rack 9 is driven down by a small amount, compressing the spring, before it efigages against the pressure member 4 and applies its pressure thereto. The pressure member 4 1s a bracket l carries switch l6 having contacts normally separated,- and being in an electric circuit with a time-indicator IS. The rack bar 9 by a bracket l9 carries an adjustable tripper for the switch. This may be an adjustable screw 20 which can be set such that it pushes the switch arm to make contact as the rack bar starts the ressure on the member 4. The time-indicator may be of the electric clock type available commercially, and as seen, it functions to indicate the time of the starting of applying of pressure to the test piece, and then when the test piece breaks and no longer opposes resistance, the spring I4 separates the pressure member 4 sufficiently from the drive and rack bar 9 to allow the switch to break contact and stop the timer clock, whereupon the total time of the application of the deformingpressure is known. And; since the rate'of movement of the rack bar is a known constant; such time measurement provides a precisioh micrometer space-traverse measure. Thus for example, if the rack bar drive rate has been set for 0.1 in; per 60 minutes, each minute becomes a space measure of 0.1/60; and so on in accordance with whatever rack drive rate has been adopted. And in general thus the time measure at constant rate gives a direct determinati'o'nof the space traverse or the movement or the rack bar.
If the test piece be molded to twice the length necessary for the spacing between the support knife edges 3, :it permits the placingof the test piece first such that the intermediate pressure knifeedge 4 strikesit midway. The first test then breaks the sample into two equal halves, "and each half may then be successively run through a similar test, and thus three readings on the samepiece may be had, for extreme accuracy.
As illustrative of the test procedure:
asphalt from Mid-Continent crude, pe'ntra 4 tion 63 at 77 F., in amount of 10 per cent by weight, was mixed at 250 F. with 15 per cent by weight of limestone ground to 200 mesh, and 75 parts by weight of sand of 40-80 mesh, and the well mixed material was molded at 20,000 pounds per square inch a inch by inch by 5 inch mold, and after cooling was removes and placed on the support knife edges in the temperature-control chamber. After allowing the test piece to come to the temperature of the chamber, 0? the iiiotor was started, and as the rack bar was forced down, compressing the lost-motion spring; the tripper operated the timer switch and the time indicator was started. With aconstar-it speed of advance of 0.07 inch per hour, the upper mire edge was driven forward against the test piece. After about 25 minutes, through the glassfront of the housing, a small crack was seen in the lower edge of the test piece. With further lapse of time, this crack extended, and finally the sample tore apart, and the lost-motiohspring caused the: switch to open and stop the timer. The total time was found to be 40.45 minutes, and so at the rack drive rate per minute as set for this test the distance travelled in the deformation in that time equalled 0.043 inch. Hence; the maximum deformability shown by this sample equals distance travelled divided by test piece thickness or 0043/05 or 86 per cent. This percentage result can be compared directly with results similarly obtained on other asphalts, and as fore-noted,- the deformability correlates to the practical performance which may be expected of a particular asphalt in actual pavement service.
Similarly,- for any other material where it is desired to test the deformability by a constant advance rate of pressure knife edge,- the ratio of distance travelled and test piece thickness may be determined with a drive rate suitable on a basis of temperature, size; etc; as appropriate for the kind of material to betested.
Other modes of applying the principle of the invention may be employed, change being made as regards the details described; provided the features stated in any of the following claims or the equivalent of such be employed.
We therefore particularly point out and distinctly claim as our invention:
1; In testing apparatus, a temperature control housing, spaced edges therein to support a piece to be tested, a movable opposed edge member intermediate said edges, and an electric switch carried by said member, the combination of a rack bar having an end telescoping with said opposed edge member for limited movement relative thereto, an adjustable tripper carried by said rack bar for actuating said electric switch, a spring between said rack ba'rand said edge men'rber normally maintaining the tripper out of operative contact with the switch, a timing clock controlled by said switch, and means for driving said rack bar at a constant low rate of speed, said means including anaxially movable pinion for meshing and unmeshing with said rack bar, and a drive motor and reducing gearing connected to said pinion.
2. In testing apparatus, a temperature control housing, spaced edges therein to support apiece to be tested, a movable opposed edge member intermediate said edges, an electric switch carried by said member, a rack bar having lost-motion connection to said -opposed "edge member, an adjustable tripper carried by said rack bar for actuating said switch, a spring normally maim taining the tripper out of operating contact with the switch, a timer in circuit with said switch, and means for driving said rack bar at a constant low rate of speed.
3. In testing apparatus, a temperature control housing, spaced edges therein to support a piece to be tested, a movable opposed edge member intermediate said edges, means for determining the beginning and the end of movement thereof against the piece being tested, including an electric switch carried by said member, and a driving bar having lost-motion connection with said opposed edge member, together with an adjustable tripper carried by said bar for actuating said switch, and a spring normally maintaining the tripper out of operating contact with the switch, and means for driving said bar and opposed edge member at a constant low rate of speed.
4. In testing apparatus, a temperature control housing, spaced edges therein to support a piece to be tested, a movable opposed edge member intermediate said edges, means for determining the beginning and the end of movement thereof against the piece being tested, including a driving bar with lost-motion connection to said movable opposed edge member, and an electric switch at the lost-motion connection, means for driving said bar and opposed edge member at a constant low rate of speed, and means controlled by closing and opening of the switch by the bar movement relative to said opposed edge member for measuring the time of travel.
ROBERT B. FARIS, JR.
HARLEY F. HARDMAN.
MELVIN M. FINK.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 1,225,438 Howard May 8, 1917 1,827,805 Watts Oct. 20', 1931 2,122,203 Gogan June 28, 1938 2,185,340 Howe Jan. 2, 1940 2,293,488 Bays Aug. 18, 1942 2,338,338 Kieckhefer Jan. 4, 1944 2,346,981 Manjoine et a1 Apr. 18, 1944 2,377,869 Elliot June 12, 1945 2,404,584 Liska et al July 23, 1946 2,426,390 DeForest Aug.-26, 1947 2,504,985 Kallas et a1 .Apr. 25, 1950
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Cited By (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2729967A (en) * | 1954-05-27 | 1956-01-10 | Kellogg M W Co | Method and apparatus for determining the characteristics of a thermoplastic material |
US2763149A (en) * | 1953-11-23 | 1956-09-18 | Roger A Long | Hydraulic tensile testing apparatus for material |
US2764889A (en) * | 1953-05-12 | 1956-10-02 | Standard Oil Co | Apparatus for determining the brittle temperature of plastic materials |
US2807163A (en) * | 1955-02-01 | 1957-09-24 | Uselis Alfonsas | Hair wave processing indicator |
US2817232A (en) * | 1954-07-14 | 1957-12-24 | Richard A Flinn | Apparatus for stressing and viewing metallurgical specimens |
US2931220A (en) * | 1957-10-21 | 1960-04-05 | Northrop Corp | Deflection measuring apparatus |
US2990953A (en) * | 1958-10-21 | 1961-07-04 | Mosaic Tile Company | Machine for detecting cracked ceramic tiles |
US3289460A (en) * | 1965-02-02 | 1966-12-06 | William M Anderson | Melting point determining apparatus |
US3313147A (en) * | 1964-04-27 | 1967-04-11 | Dow Chemical Co | Non-destructive testing of structures |
US3350929A (en) * | 1964-09-09 | 1967-11-07 | Johns Manville | Method for testing paving materials |
US3381526A (en) * | 1965-05-10 | 1968-05-07 | Babcock & Wilcox Co | Fatigue testing apparatus and method |
US3404562A (en) * | 1966-01-19 | 1968-10-08 | Army Usa | High-strain-rate tester |
US3774440A (en) * | 1972-01-10 | 1973-11-27 | Stanford Research Inst | Instrument for determining polymer deflection temperatures |
US4107979A (en) * | 1976-03-11 | 1978-08-22 | Showa Denko K.K. | Method and device for measurement of environmental stress cracking |
US4405243A (en) * | 1980-12-26 | 1983-09-20 | Hoxan Corporation | Cryogenic impact testing method and machine |
US4566335A (en) * | 1984-08-16 | 1986-01-28 | Shell Oil Company | Method and apparatus for testing fiber reinforced plastic laminates |
US4653323A (en) * | 1985-10-09 | 1987-03-31 | Westinghouse Electric Corp. | Apparatus for moving an object in an isolated environment |
US4763529A (en) * | 1987-08-18 | 1988-08-16 | The United States Of America As Represented By The Secretary Of The Air Force | In-situ beta alumina stress simulator |
US4813287A (en) * | 1986-11-03 | 1989-03-21 | Bayer Aktiegesellschaft | Testing device for determining mechanical properties of a granulated material |
US4976152A (en) * | 1989-11-13 | 1990-12-11 | The Perkin Elmer Corporation | 3 point bending measuring system |
US5187987A (en) * | 1991-11-19 | 1993-02-23 | The Pennsylvania Research Corporation | Bending beam creep test device with piston having a gas bearing |
FR2686977A1 (en) * | 1992-02-04 | 1993-08-06 | Commissariat Energie Atomique | Device for creep testing a sample |
FR2735235A1 (en) * | 1995-06-12 | 1996-12-13 | Aerospatiale | Mechanical flexion testing appts for polymer and metal samples |
US20060169110A1 (en) * | 2002-09-25 | 2006-08-03 | Chiao-Chung Huang | Test piece splitting device |
US7089803B1 (en) | 2005-10-28 | 2006-08-15 | Huber Engineered Woods Llc | Panel performance testing system |
US20080210015A1 (en) * | 2007-02-02 | 2008-09-04 | Shenzhen Futaihong Precision Industry Co., Ltd. | Failure analysis system and method using the same |
US20090260450A1 (en) * | 2007-12-20 | 2009-10-22 | Commissariat A L'energie Atomique | Method for measuring the creep of a thin film inserted between two rigid substrates, with one cantilever end |
US20110136239A1 (en) * | 2009-12-08 | 2011-06-09 | National Oilwell Varco, L.P. | Corrosion testing apparatus and methods |
DE102010040268A1 (en) * | 2010-09-03 | 2012-03-08 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Creep test stand for e.g. compression test to determine creep behavior of sample material i.e. plastic, has supporting device engaged at holding device and/or testing mass to temporarily ablate weight of testing mass |
US20120186358A1 (en) * | 2008-12-17 | 2012-07-26 | Nardi Aaron T | Apparatus for evaluation of coated parts |
FR2991050A1 (en) * | 2012-05-23 | 2013-11-29 | Meco Concept | Portable device for measuring effort resistance of e.g. bricks, used in construction field, has shearing bar exerting vertical force from top to bottom till rupture of specimens during continuous descending motion of shearing bar |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1225438A (en) * | 1915-06-21 | 1917-05-08 | William B Howard | Automatically-timed asphalt-tester. |
US1827805A (en) * | 1930-04-16 | 1931-10-20 | George G Pomeroy | Transverse testing machine |
US2122203A (en) * | 1936-04-18 | 1938-06-28 | Gogan Joseph | Continuous hardness tester |
US2185340A (en) * | 1938-10-01 | 1940-01-02 | Ind Developments Inc | Ductility testing apparatus |
US2293488A (en) * | 1938-04-06 | 1942-08-18 | Stanolind Oil & Gas Co | Apparatus for determining permeability |
US2338338A (en) * | 1942-12-05 | 1944-01-04 | Kieckhefer Container Company | Stiffness testing device |
US2346981A (en) * | 1940-12-05 | 1944-04-18 | Westinghouse Electric & Mfg Co | Tensile machine |
US2377869A (en) * | 1942-11-17 | 1945-06-12 | Myron A Elliott | Apparatus and method for measuring work |
US2404584A (en) * | 1944-12-30 | 1946-07-23 | Firestone Tire & Rubber Co | Bending modulus test apparatus |
US2426390A (en) * | 1944-11-17 | 1947-08-26 | Baldwin Locomotive Works | Straightening apparatus |
US2504985A (en) * | 1945-04-28 | 1950-04-25 | Danos H Kallas | Heat-distortion testing apparatus |
-
1950
- 1950-04-04 US US153832A patent/US2670624A/en not_active Expired - Lifetime
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1225438A (en) * | 1915-06-21 | 1917-05-08 | William B Howard | Automatically-timed asphalt-tester. |
US1827805A (en) * | 1930-04-16 | 1931-10-20 | George G Pomeroy | Transverse testing machine |
US2122203A (en) * | 1936-04-18 | 1938-06-28 | Gogan Joseph | Continuous hardness tester |
US2293488A (en) * | 1938-04-06 | 1942-08-18 | Stanolind Oil & Gas Co | Apparatus for determining permeability |
US2185340A (en) * | 1938-10-01 | 1940-01-02 | Ind Developments Inc | Ductility testing apparatus |
US2346981A (en) * | 1940-12-05 | 1944-04-18 | Westinghouse Electric & Mfg Co | Tensile machine |
US2377869A (en) * | 1942-11-17 | 1945-06-12 | Myron A Elliott | Apparatus and method for measuring work |
US2338338A (en) * | 1942-12-05 | 1944-01-04 | Kieckhefer Container Company | Stiffness testing device |
US2426390A (en) * | 1944-11-17 | 1947-08-26 | Baldwin Locomotive Works | Straightening apparatus |
US2404584A (en) * | 1944-12-30 | 1946-07-23 | Firestone Tire & Rubber Co | Bending modulus test apparatus |
US2504985A (en) * | 1945-04-28 | 1950-04-25 | Danos H Kallas | Heat-distortion testing apparatus |
Cited By (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2764889A (en) * | 1953-05-12 | 1956-10-02 | Standard Oil Co | Apparatus for determining the brittle temperature of plastic materials |
US2763149A (en) * | 1953-11-23 | 1956-09-18 | Roger A Long | Hydraulic tensile testing apparatus for material |
US2729967A (en) * | 1954-05-27 | 1956-01-10 | Kellogg M W Co | Method and apparatus for determining the characteristics of a thermoplastic material |
US2817232A (en) * | 1954-07-14 | 1957-12-24 | Richard A Flinn | Apparatus for stressing and viewing metallurgical specimens |
US2807163A (en) * | 1955-02-01 | 1957-09-24 | Uselis Alfonsas | Hair wave processing indicator |
US2931220A (en) * | 1957-10-21 | 1960-04-05 | Northrop Corp | Deflection measuring apparatus |
US2990953A (en) * | 1958-10-21 | 1961-07-04 | Mosaic Tile Company | Machine for detecting cracked ceramic tiles |
US3313147A (en) * | 1964-04-27 | 1967-04-11 | Dow Chemical Co | Non-destructive testing of structures |
US3350929A (en) * | 1964-09-09 | 1967-11-07 | Johns Manville | Method for testing paving materials |
US3289460A (en) * | 1965-02-02 | 1966-12-06 | William M Anderson | Melting point determining apparatus |
US3381526A (en) * | 1965-05-10 | 1968-05-07 | Babcock & Wilcox Co | Fatigue testing apparatus and method |
US3404562A (en) * | 1966-01-19 | 1968-10-08 | Army Usa | High-strain-rate tester |
US3774440A (en) * | 1972-01-10 | 1973-11-27 | Stanford Research Inst | Instrument for determining polymer deflection temperatures |
US4107979A (en) * | 1976-03-11 | 1978-08-22 | Showa Denko K.K. | Method and device for measurement of environmental stress cracking |
US4405243A (en) * | 1980-12-26 | 1983-09-20 | Hoxan Corporation | Cryogenic impact testing method and machine |
US4566335A (en) * | 1984-08-16 | 1986-01-28 | Shell Oil Company | Method and apparatus for testing fiber reinforced plastic laminates |
US4653323A (en) * | 1985-10-09 | 1987-03-31 | Westinghouse Electric Corp. | Apparatus for moving an object in an isolated environment |
US4813287A (en) * | 1986-11-03 | 1989-03-21 | Bayer Aktiegesellschaft | Testing device for determining mechanical properties of a granulated material |
US4763529A (en) * | 1987-08-18 | 1988-08-16 | The United States Of America As Represented By The Secretary Of The Air Force | In-situ beta alumina stress simulator |
US4976152A (en) * | 1989-11-13 | 1990-12-11 | The Perkin Elmer Corporation | 3 point bending measuring system |
EP0428010A2 (en) * | 1989-11-13 | 1991-05-22 | The Perkin-Elmer Corporation | 3 point bending measuring system |
EP0428010A3 (en) * | 1989-11-13 | 1991-11-27 | The Perkin-Elmer Corporation | 3 point bending measuring system |
US5187987A (en) * | 1991-11-19 | 1993-02-23 | The Pennsylvania Research Corporation | Bending beam creep test device with piston having a gas bearing |
FR2686977A1 (en) * | 1992-02-04 | 1993-08-06 | Commissariat Energie Atomique | Device for creep testing a sample |
FR2735235A1 (en) * | 1995-06-12 | 1996-12-13 | Aerospatiale | Mechanical flexion testing appts for polymer and metal samples |
US20060169110A1 (en) * | 2002-09-25 | 2006-08-03 | Chiao-Chung Huang | Test piece splitting device |
US7089803B1 (en) | 2005-10-28 | 2006-08-15 | Huber Engineered Woods Llc | Panel performance testing system |
US20080210015A1 (en) * | 2007-02-02 | 2008-09-04 | Shenzhen Futaihong Precision Industry Co., Ltd. | Failure analysis system and method using the same |
US7543507B2 (en) * | 2007-02-02 | 2009-06-09 | Shenzhen Futaihong Precision Industry Co., Ltd. | Failure analysis system for printed circuit board and method using the same |
US20090260450A1 (en) * | 2007-12-20 | 2009-10-22 | Commissariat A L'energie Atomique | Method for measuring the creep of a thin film inserted between two rigid substrates, with one cantilever end |
US8152364B2 (en) * | 2007-12-20 | 2012-04-10 | Commissariat A L'energie Atomique | Method for measuring the creep of a thin film inserted between two rigid substrates, with one cantilever end |
US20120186358A1 (en) * | 2008-12-17 | 2012-07-26 | Nardi Aaron T | Apparatus for evaluation of coated parts |
US8443678B2 (en) * | 2008-12-17 | 2013-05-21 | Hamilton Sundstrant Corporation | Apparatus for evaluation of coated parts |
US20110136239A1 (en) * | 2009-12-08 | 2011-06-09 | National Oilwell Varco, L.P. | Corrosion testing apparatus and methods |
US8513020B2 (en) * | 2009-12-08 | 2013-08-20 | National Oilwell Varco, L.P. | Corrosion testing apparatus and methods |
DE102010040268A1 (en) * | 2010-09-03 | 2012-03-08 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Creep test stand for e.g. compression test to determine creep behavior of sample material i.e. plastic, has supporting device engaged at holding device and/or testing mass to temporarily ablate weight of testing mass |
FR2991050A1 (en) * | 2012-05-23 | 2013-11-29 | Meco Concept | Portable device for measuring effort resistance of e.g. bricks, used in construction field, has shearing bar exerting vertical force from top to bottom till rupture of specimens during continuous descending motion of shearing bar |
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