US2077390A - Frequency comparing device for determining the force of gravity - Google Patents
Frequency comparing device for determining the force of gravity Download PDFInfo
- Publication number
- US2077390A US2077390A US659821A US65982133A US2077390A US 2077390 A US2077390 A US 2077390A US 659821 A US659821 A US 659821A US 65982133 A US65982133 A US 65982133A US 2077390 A US2077390 A US 2077390A
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- United States
- Prior art keywords
- pendulum
- tuning fork
- light
- gravity
- vibrations
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- Expired - Lifetime
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- 230000005484 gravity Effects 0.000 title description 9
- 230000010349 pulsation Effects 0.000 description 14
- 238000004804 winding Methods 0.000 description 8
- 230000010355 oscillation Effects 0.000 description 7
- 230000001131 transforming effect Effects 0.000 description 3
- 238000005286 illumination Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 2
- 229910052753 mercury Inorganic materials 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 235000014676 Phragmites communis Nutrition 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
- ACWBQPMHZXGDFX-QFIPXVFZSA-N valsartan Chemical class C1=CC(CN(C(=O)CCCC)[C@@H](C(C)C)C(O)=O)=CC=C1C1=CC=CC=C1C1=NN=NN1 ACWBQPMHZXGDFX-QFIPXVFZSA-N 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
- G01V7/00—Measuring gravitational fields or waves; Gravimetric prospecting or detecting
-
- G—PHYSICS
- G04—HOROLOGY
- G04D—APPARATUS OR TOOLS SPECIALLY DESIGNED FOR MAKING OR MAINTAINING CLOCKS OR WATCHES
- G04D7/00—Measuring, counting, calibrating, testing or regulating apparatus
- G04D7/12—Timing devices for clocks or watches for comparing the rate of the oscillating member with a standard
- G04D7/1207—Timing devices for clocks or watches for comparing the rate of the oscillating member with a standard only for measuring
Definitions
- Fig. 1 is a diagrammatic view of a tuning fork assembly
- Fig. 2 is a diagrammatic view of a pendulum assembly
- Fig. 3 is a diagrammatic view of the apparatus for making the record
- Fig. 4 is a front view of a film showing a typical record
- Fig. 5 is a front elevational view of the disk wheel.
- reference numeral l designates a tuning fork.
- a vibrating reed or any other suitable vibrating system can be used in place of the tuning fork and some of the advantages of the invention will be retained.
- the tuning fork l is electrically driven by means of electromagnets 2 and 2'.
- Theleads of the electromagnets 2 and 2' are connected to a suitable driving arrangement 3 whereby the electromagnets are energized to produce sustained vibrations of the prongs of the tuning fork.
- the electro'magnets 4 and 4' constitute the output units in the tuning fork,
- the output leads from the electromagnets 4 and 4' are connected to the primary coil 5 of an audio transformer to deliver electrical impulses from the tuning fork.
- the audio transformer has a split secondary winding one of which is designated 6 and the other is designated 1.
- the amplified electrical impulses drive a synchronous motor 9.
- a disk wheel i0 is fastened to the driving mechanism of the synchronous motor 9.
- the disk wheel I0 is provided with a slot 13 for a purpose to be later described.
- the disk wheel is geared to the motor 9 so as to give it the desired frequency of rotation.
- the secondary winding 1 of the audio transformer delivers electrical impulses from the tuning fork I to an amplifier l4 the output of which is connected across the grid and filament of a thyratron tube 16.
- a condenser i1 and the primary winding ill of an audio transformer are put into the plate filament circuit of the thyratron tube.
- the A battery of the tube 3 is designated 80, the B battery is 81 and the plate resistance is 82.
- One of the leads from the secondary winding IQ of the transformer is connected to an electrode 2
- the lower portion of the glow tube 22 contains a body of mercury 24 the upper surface 25 of which underlies the electrode 2
- the second lead 2i from the secondary winding 19 of the transformer is connected to the electrode 26.
- a third electrode 28 is disposed in the upper portion of the glow tube 22 and leads to a large condenser 29.
- the condenser 29 is connected in parallel with a battery til and in series with a A resistance St.
- the glow tube 22 operates as follows:
- the voltage drop across the transformer secondary l9 ionizes the path between the upper electrode it on the secondary and the surface 25 of the body of mercury.
- the ionization decreases the resistance of the glow tube 22 so that the voltage drop across the condenser 29 which is charged through the resistance 3
- the voltage of the battery Si is so adjusted that the glow tube 22 will not flash unless part of the path through the tube is ionized by an impulse from the thyratron tube it through the transformer secondary it.
- reference numeral designates a pendulum having a knife edge 36.
- a mirror 3i is secured to the upper surface of the pendulum 35.
- a mirror 33 is disposed above and in spaced relation to the pendulum and inclined at an angle to the mirror 37.
- a beam of light is directed from a lamp 4! to the mirror 3B and is reflected along the line 43 to the mirror 31.
- a beam of light is reflected from the mirror 31 along the line 44 to the mirror 38 and is reflected again along the line 46. Oscillation of the pendulum alters the direction of the beam of light lines.
- a screen Bl provided with a slot 48 is disposed in the path of the light rays along the line 46.
- the screen All and the mirror 38 are so arranged that the beam of light from the lamp 4
- An electric current is generated by the photoelectric cell upon illumination of the cell by the beam of light along the line 46.
- This current is conducted from the photo-electric cell 50 to a suitable amplifier such as a vacuum tube amplifier 5
- the amplified current is conducted through the output leads of the amplifier 5
- the plate-filament circuit of the thyratron tube 52 mary winding ll of an audio transformer.
- the relay It actuates a suitable counter It.
- the secondary winding 51 of the audio transformer is connected to two of the electrodes of a glow tube It the function and circuit of which are identical in all respects with the glow tube circuit previously described. and like reference numerals have been applied to like parts of the glow tube circuits.
- a battery of this circuit is designated ll, the B battery is 84 and the plate resistance is 8!.
- the mechanism for recording the pulsations of energy generated in the systems illustrated in Figs. 1 and 2 includes a sensitive film Bil carried by a recording drum it and driven in travel by any suitable means not shown.
- the flashes of light from the glow tube 22 of the tuning fork circuit are focused upon the film I! by means of a lens iii.
- the flashes of light from the glow tube 58 of the pendulum circuit are focused upon the film 58 by means of a lens 63.
- Intermittent pulsations of energy generated by the tuning fork I are recorded as follows:
- a lamp 64 is positioned behind the disk wheel Ill.
- a ray of light from the lamp 64 passes through the slot I3 of the disk wheel Ill intermittently along the line 65 during rotation of the disk wheel and is directed upon the film 59.
- Another ray of light intermittently passes through the slot l3 upon rotation of the disk wheel l0 along the line 66.
- a prism 61 intercepts this light and reflects it along the line 69 into a photo-electric cell 10.
- An electric current is generated by the photoelectric cell 10 upon illumination of the cell by the beam of light. This current is conducted from the photo-electric cell 10 through a line H to a current amplifier 12.
- the output leads of the amplifier 12 are connected to a relay 13 which actuates a counter 14.
- the lines 15 along the upper edge of the film 59 are due to the light which fell upon the film from lamp 64 through the slot iii in the disk wheel l0, and are proportional to the number of intermittent oscillations of the tuning fork Lines 16 are due to the light which similarly fell upon the film 59 from the glow tube 22, and are proportional to the number of oscillations of the tuning fork I Lines 11 and 18 are due to light which fell upon the film from the glow tube 58 and represent each beat of the pendulum.
- a tuning fork is used the frequency of which is 1,000 cycles per second.
- the disk wheel l0 rotates ten times per thousand vibrations of the tuning fork and has the one radial slot l3.
- the wheel It can be provided with ten radial slots and be rotated one time for each one thousand vibrations of the tuning fork. Consequently, there is one line 15 for each one hundred lines 16.
- the lines 11 and 18 represent the instant of time when the pendulum 35 passed through its position of equilibrium.
- the lines 15 mark 0.1 second inter- 5 vals.
- the counter 14 registers the lines 15, so that includes a relay It, a condenser I4, and the priit is only necessary to record for a few seconds at the beginning and at the end of the observation period and with such a film speed as would enable the recorder to read to one-fifteenth of the distance between the individual lines 1., thereby gaining an accuracy of one part in ten million.
- the pendulum and tuning fork apparatus above described is set up at the point which is to be used as a reference point. During the observation period of ten minutes, the pendulum having a period of approidmately one second will oscillate, say 600 times.
- the number of tuning fork vibrations for 600 pendulum oscillations will then be determined to one-fifteenth or approximately 7/l00ths of a tuning fork vibration.
- the apparatus is then moved to some other location, where a ten minute observation again yields the number of tuning fork vibrations for 600 pendulum oscillations.
- the difference between the number of tuning fork vibrations per 600 pendulum oscillations at the base station and the number of tuning fork vibrations per 600 pendulum oscillations at the second location then yield the difference in gravity by a simple computation to one part in ten millions.
- the time of observation for determining relative gravity measurements is minimized. Relative gravity measurements are obtained at spaced stations without a necessity for any sort of communication between the stations.
- a gravity responsive pendulum means for converting the beats of the pendulum into pulsations of energy, means for counting the pulsations, a source of vibrations of constant frequency, means for converting the vibrations into pulsations of energy proportional to the vibrations, means for selecting pulsations from the source proportional to predetermined multiples of the vibrations, means for counting the last mentioned pulsations, and means for recording the three sets of pulsations near the beginning and end of the observation period upon a common record for the purpose of comparing the frequencies of the pendulum and source.
- a gravity responsive pendulum means for converting the beats of the pendulum into pulsations of energy, means for counting the pulsations, means for transforming the pulsations into flashes of light, a source of vibrations of constant frequency, means for converting the vibrations into pulsations of energy proportional to the vibrations, means for transforming the pulsations from the source into flashes of light proportional to the vibrations, means for transforming the pulsations from the source into flashes of light proportional to predetermined multiples of the vibrations, means for counting the last mentioned flashes of light, and means for recording the three sets of flashes of light near the beginning and end of the observation period upon a common record for the purpose of comparing the frequencies of the pendulum and the source.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geophysics (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
Description
L. w. BLAU 2,077,390
April 20, 1937.
FREQUENCY COMPARING DEVICE FOR DETERMINING THE FORCE OF GRAVITY Filed March 6, 1933 2 Sheets-Sheet l MWM 3W ZZZMMH April 20, 1937. L. w. BLAU 2,077,390 FREQUENCY COMPARING DEVICE FOR DETERMINING THE FORCE 0F GRAVITY I Filed March a, 1935 2 Sheets-Sheet 2 A 5. 5 50 5 WM l H l M lllllllllllllll lllllllllllllll WWZBM 3M Patented Apr. 20, 1937 UNITED STATES PATENT OFFICE FREQUENCY COMPARING DEVICE FOR DE- TERMINING THE FORCE OF GRAVITY Ludwig W. Blau,
Houston,
Tex, assignor to Standard Oil Development Company, 3. 001110- ration of Delaware Application March 6, i933, Serial No. 659,821
physical gravitational prospecting.
The invention will be fully understood from the following description taken in connection with the accompanying drawings, in which latter Fig. 1 is a diagrammatic view of a tuning fork assembly;
Fig. 2 is a diagrammatic view of a pendulum assembly;
Fig. 3 is a diagrammatic view of the apparatus for making the record;
Fig. 4 is a front view of a film showing a typical record; and
Fig. 5 is a front elevational view of the disk wheel.
Referring particularly to Fig. l. of the draw ings, reference numeral l designates a tuning fork. A vibrating reed or any other suitable vibrating system can be used in place of the tuning fork and some of the advantages of the invention will be retained. The tuning fork l is electrically driven by means of electromagnets 2 and 2'. Theleads of the electromagnets 2 and 2' are connected to a suitable driving arrangement 3 whereby the electromagnets are energized to produce sustained vibrations of the prongs of the tuning fork. The electro'magnets 4 and 4' constitute the output units in the tuning fork, The output leads from the electromagnets 4 and 4' are connected to the primary coil 5 of an audio transformer to deliver electrical impulses from the tuning fork. The audio transformer has a split secondary winding one of which is designated 6 and the other is designated 1. The sec= ondary winding 6 is connected to a vacuum tube amplifier 8 whereby the electrical impulses are amplified. The amplified electrical impulses drive a synchronous motor 9. A disk wheel i0 is fastened to the driving mechanism of the synchronous motor 9. The disk wheel I0 is provided with a slot 13 for a purpose to be later described. The disk wheel is geared to the motor 9 so as to give it the desired frequency of rotation.
The secondary winding 1 of the audio transformer delivers electrical impulses from the tuning fork I to an amplifier l4 the output of which is connected across the grid and filament of a thyratron tube 16. A condenser i1 and the primary winding ill of an audio transformer are put into the plate filament circuit of the thyratron tube. The A battery of the tube 3 is designated 80, the B battery is 81 and the plate resistance is 82. One of the leads from the secondary winding IQ of the transformer is connected to an electrode 2| in an intermediate portion of a glow tube 22. The lower portion of the glow tube 22 contains a body of mercury 24 the upper surface 25 of which underlies the electrode 2| and constitutes a second electrode. The second lead 2i from the secondary winding 19 of the transformer is connected to the electrode 26. A third electrode 28 is disposed in the upper portion of the glow tube 22 and leads to a large condenser 29. The condenser 29 is connected in parallel with a battery til and in series with a A resistance St. The glow tube 22 operates as follows:
The voltage drop across the transformer secondary l9 ionizes the path between the upper electrode it on the secondary and the surface 25 of the body of mercury. The ionization decreases the resistance of the glow tube 22 so that the voltage drop across the condenser 29 which is charged through the resistance 3| by the battery till is sufficiently high to flash the tube. The voltage of the battery Si is so adjusted that the glow tube 22 will not flash unless part of the path through the tube is ionized by an impulse from the thyratron tube it through the transformer secondary it.
Referring particularly to Fig. 2, reference numeral designates a pendulum having a knife edge 36. A mirror 3i is secured to the upper surface of the pendulum 35. A mirror 33 is disposed above and in spaced relation to the pendulum and inclined at an angle to the mirror 37. A beam of light is directed from a lamp 4! to the mirror 3B and is reflected along the line 43 to the mirror 31. A beam of light is reflected from the mirror 31 along the line 44 to the mirror 38 and is reflected again along the line 46. Oscillation of the pendulum alters the direction of the beam of light lines.
A screen Bl provided with a slot 48 is disposed in the path of the light rays along the line 46. The screen All and the mirror 38 are so arranged that the beam of light from the lamp 4| is reflected through the slot 48 into a photo-electric cell 50 only when the pendulum 35 is swinging through a predetermined position, preferably the equililczium position.
An electric current is generated by the photoelectric cell upon illumination of the cell by the beam of light along the line 46. This current is conducted from the photo-electric cell 50 to a suitable amplifier such as a vacuum tube amplifier 5|. The amplified current is conducted through the output leads of the amplifier 5| across the grid and filament of a thyratron tube 52. The plate-filament circuit of the thyratron tube 52 mary winding ll of an audio transformer. The relay It actuates a suitable counter It. The secondary winding 51 of the audio transformer is connected to two of the electrodes of a glow tube It the function and circuit of which are identical in all respects with the glow tube circuit previously described. and like reference numerals have been applied to like parts of the glow tube circuits. The
A battery of this circuit is designated ll, the B battery is 84 and the plate resistance is 8!.
As illustrated in Fig. 3, the mechanism for recording the pulsations of energy generated in the systems illustrated in Figs. 1 and 2 includes a sensitive film Bil carried by a recording drum it and driven in travel by any suitable means not shown. The flashes of light from the glow tube 22 of the tuning fork circuit are focused upon the film I! by means of a lens iii. In like manner, the flashes of light from the glow tube 58 of the pendulum circuit are focused upon the film 58 by means of a lens 63. Intermittent pulsations of energy generated by the tuning fork I are recorded as follows:
A lamp 64 is positioned behind the disk wheel Ill. A ray of light from the lamp 64 passes through the slot I3 of the disk wheel Ill intermittently along the line 65 during rotation of the disk wheel and is directed upon the film 59. Another ray of light intermittently passes through the slot l3 upon rotation of the disk wheel l0 along the line 66. A prism 61 intercepts this light and reflects it along the line 69 into a photo-electric cell 10. An electric current is generated by the photoelectric cell 10 upon illumination of the cell by the beam of light. This current is conducted from the photo-electric cell 10 through a line H to a current amplifier 12. The output leads of the amplifier 12 are connected to a relay 13 which actuates a counter 14.
In the record illustrated in Fig. 4 the lines 15 along the upper edge of the film 59 are due to the light which fell upon the film from lamp 64 through the slot iii in the disk wheel l0, and are proportional to the number of intermittent oscillations of the tuning fork Lines 16 are due to the light which similarly fell upon the film 59 from the glow tube 22, and are proportional to the number of oscillations of the tuning fork I Lines 11 and 18 are due to light which fell upon the film from the glow tube 58 and represent each beat of the pendulum.
In the preferredarrangement a tuning fork is used the frequency of which is 1,000 cycles per second. The disk wheel l0 rotates ten times per thousand vibrations of the tuning fork and has the one radial slot l3. Alternatively, the wheel It can be provided with ten radial slots and be rotated one time for each one thousand vibrations of the tuning fork. Consequently, there is one line 15 for each one hundred lines 16. The lines 11 and 18 represent the instant of time when the pendulum 35 passed through its position of equilibrium. The lines 15 mark 0.1 second inter- 5 vals. The counter 14 registers the lines 15, so that includes a relay It, a condenser I4, and the priit is only necessary to record for a few seconds at the beginning and at the end of the observation period and with such a film speed as would enable the recorder to read to one-fifteenth of the distance between the individual lines 1., thereby gaining an accuracy of one part in ten million. The pendulum and tuning fork apparatus above described is set up at the point which is to be used as a reference point. During the observation period of ten minutes, the pendulum having a period of approidmately one second will oscillate, say 600 times. From the record the number of tuning fork vibrations for 600 pendulum oscillations will then be determined to one-fifteenth or approximately 7/l00ths of a tuning fork vibration. The apparatus is then moved to some other location, where a ten minute observation again yields the number of tuning fork vibrations for 600 pendulum oscillations. The difference between the number of tuning fork vibrations per 600 pendulum oscillations at the base station and the number of tuning fork vibrations per 600 pendulum oscillations at the second location then yield the difference in gravity by a simple computation to one part in ten millions. By the construction described the time of observation for determining relative gravity measurements is minimized. Relative gravity measurements are obtained at spaced stations without a necessity for any sort of communication between the stations.
Various changes and alternative arrangements may be made within the scope of the appended claims, in which it is my intention to claim all novelty inherent in the invention as broadly as the prior art permits.
I claim:
1. In an apparatus for geophysical gravitational prospecting, a gravity responsive pendulum, means for converting the beats of the pendulum into pulsations of energy, means for counting the pulsations, a source of vibrations of constant frequency, means for converting the vibrations into pulsations of energy proportional to the vibrations, means for selecting pulsations from the source proportional to predetermined multiples of the vibrations, means for counting the last mentioned pulsations, and means for recording the three sets of pulsations near the beginning and end of the observation period upon a common record for the purpose of comparing the frequencies of the pendulum and source.
2. In an apparatus for geophysical gravitational prospecting, a gravity responsive pendulum, means for converting the beats of the pendulum into pulsations of energy, means for counting the pulsations, means for transforming the pulsations into flashes of light, a source of vibrations of constant frequency, means for converting the vibrations into pulsations of energy proportional to the vibrations, means for transforming the pulsations from the source into flashes of light proportional to the vibrations, means for transforming the pulsations from the source into flashes of light proportional to predetermined multiples of the vibrations, means for counting the last mentioned flashes of light, and means for recording the three sets of flashes of light near the beginning and end of the observation period upon a common record for the purpose of comparing the frequencies of the pendulum and the source.
LUDWIG W. BLAU.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US659821A US2077390A (en) | 1933-03-06 | 1933-03-06 | Frequency comparing device for determining the force of gravity |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US659821A US2077390A (en) | 1933-03-06 | 1933-03-06 | Frequency comparing device for determining the force of gravity |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2077390A true US2077390A (en) | 1937-04-20 |
Family
ID=24646979
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US659821A Expired - Lifetime US2077390A (en) | 1933-03-06 | 1933-03-06 | Frequency comparing device for determining the force of gravity |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2077390A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2430810A (en) * | 1942-05-29 | 1947-11-11 | Automatic Elect Lab | Apparatus for recording the firing speed of rapid-fire guns |
| US2437929A (en) * | 1941-06-18 | 1948-03-16 | Hamilton Watch Co | Timing apparatus |
| US2458882A (en) * | 1945-10-04 | 1949-01-11 | Richard G Stoner | Timing device for high-speed motionpicture cameras |
| US2595092A (en) * | 1947-05-19 | 1952-04-29 | Standard Oil Dev Co | Method and apparatus for underwater gravity surveying |
| US2603886A (en) * | 1946-02-08 | 1952-07-22 | William C Hodgson | Motion controlling apparatus for fuse control training |
| US2629009A (en) * | 1948-10-14 | 1953-02-17 | Atlantic Refining Co | Apparatus for testing electric timers |
| US2694310A (en) * | 1948-03-03 | 1954-11-16 | American Mach & Foundry | Weight determining device |
| US2773389A (en) * | 1951-03-15 | 1956-12-11 | Gen Motors Corp | Balancing machine indicator |
| US2936624A (en) * | 1958-12-19 | 1960-05-17 | Sperry Rand Corp | Rotating pendulum accelerometer |
| US3548645A (en) * | 1968-01-24 | 1970-12-22 | Ryszard Tadeusz Sikorski | Device for measuring hardness of plastics by means of pendulum method |
-
1933
- 1933-03-06 US US659821A patent/US2077390A/en not_active Expired - Lifetime
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2437929A (en) * | 1941-06-18 | 1948-03-16 | Hamilton Watch Co | Timing apparatus |
| US2430810A (en) * | 1942-05-29 | 1947-11-11 | Automatic Elect Lab | Apparatus for recording the firing speed of rapid-fire guns |
| US2458882A (en) * | 1945-10-04 | 1949-01-11 | Richard G Stoner | Timing device for high-speed motionpicture cameras |
| US2603886A (en) * | 1946-02-08 | 1952-07-22 | William C Hodgson | Motion controlling apparatus for fuse control training |
| US2595092A (en) * | 1947-05-19 | 1952-04-29 | Standard Oil Dev Co | Method and apparatus for underwater gravity surveying |
| US2694310A (en) * | 1948-03-03 | 1954-11-16 | American Mach & Foundry | Weight determining device |
| US2629009A (en) * | 1948-10-14 | 1953-02-17 | Atlantic Refining Co | Apparatus for testing electric timers |
| US2773389A (en) * | 1951-03-15 | 1956-12-11 | Gen Motors Corp | Balancing machine indicator |
| US2936624A (en) * | 1958-12-19 | 1960-05-17 | Sperry Rand Corp | Rotating pendulum accelerometer |
| US3548645A (en) * | 1968-01-24 | 1970-12-22 | Ryszard Tadeusz Sikorski | Device for measuring hardness of plastics by means of pendulum method |
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