Figure 1 shows the AML high temperature dilatometer used for high temperature thermal expansion tests. Round capacitor plates used for thermal expansion measurements were electrically connected via coaxial cables to an Andeen Hagerling bridge providing capacitance measurements in 10 digits with a 0.5x10− 18 farad sensitivity. The furnace and high temperature dilatometer rested upon a vibration isolation table. This minimized vibration that otherwise would cause the tube capacitor plate to move relative to the tube and rod capacitor plate to move relative to the rod. Also, that minimized vibration of the specimen that might have caused undesired movement during expansion measurements.
Figure 2 showed a plastic external sealing container filled with helium that enclosed and protected the capacitor plates. The capacitor plates measured thermal expansion with a sensitivity of 2 nanometers.
Figure 3 shows the rod capacitor plate (F) that rested upon the CTE measuring rod (A) without any clamps. The tube capacitor plate (G) rested upon the CTE measuring tube (K). It was found that clamping these plates onto the CTE measuring tube (K) and the CTE measuring rod (A) respectively caused hysteresis loops during thermal expansion tests as well as non-reproducible expansion results. Since both capacitor plates, and the rod and tube are made of fused silica, this connection arrangement prevented errors in thermal expansion measurement of the specimen as the rod slid back and forth within the tube, Fig. 4.
The CTE measuring tube was housed within a fuse silica furnace tube (L) that was sealed against the aluminum sealing disk (H) outside of the furnace. The inside of the furnace had an alumina tube that surrounded the silica tube. Due to the relatively high thermal conductivity of the alumina tube compared to the silica tube, the temperature within the high temperature dilatometer region enclosing the specimen was fairly uniform. The aluminum cooling vanes (J) kept the capacitor plates close to room temperature as well and the associated apparatus enclosed within the external sealing container (Q). Flowing helium, 10 ml/min. within that container also cooled its contents.
The tube capacitor plate, Fig. 3, had a sputtered gold film approximately 1,700 Angstroms thick over its entire surface. The tube capacitor plate was connected to the high side of the capacitor bridge. The rod capacitor plate had a circular central active area, 5.6086 cm2, connected to the low side of the capacitor bridge. Surrounding the active area was a grounded area separated from the active area by 0.0025 centimeters. Both of these areas had 1,700 Angstroms of sputtered gold. The circumferential edge of the tube capacitor plate did not have sputtered gold while the edge of the rod capacitor plate had sputtered gold. These areas were designed to minimize induced currents from other electrical apparatus.
There was a calibrated platinum thermometer (S) attached to the silica tube was 3 mm away from the specimen that accurately measured the temperature to less than a tenth of degree Celsius. The four wires of the thermometer had fused lead wires that were connected to a Lake Shore Cryotronics 805 temperature controller. This controller provided one milliamp current to the platinum thermometer which measured the voltage of both the platinum thermometer and a silicon diode thermometer (R) that was attached to the aluminum frame (P), Fig. 3. These voltages were then converted to temperatures which were automatically transferred to a computer. The platinum thermometer temperature TA was used to measure the temperature of the specimen while the silicon diode temperature TB was used to measure the temperature of the capacitor plates.
A brass plate was attached to the aluminum frame with two stainless steel screws. This plate was also attached to a bellows (D) of stainless steel. The other end of the bellows was attached to a brass ring that in turn clamped onto the CTE measuring rod via a nylon screw. In this way the bellows acted as a non-rotating spring in compression providing force upon the rod. A coil spring would cause rotation of the rod during thermal expansion tests resulting in measurement errors.
The tube had two constrictions that surrounded and supported the rod, Fig. 4, with a few thousandths of a centimeter clearance. The rod was coated with Teflon to minimize friction, coefficient of friction = 0.04, while sliding within the tube. The Teflon region was outside of the furnace so that it was not exposed to a temperature significantly different than that of room temperature.
The frame, bellows, and capacitor plates were housed inside an air tight external sealing container (Q) within which helium gas flowed via the inlet valve (N) at 10 ml/minute during the thermal expansion tests. Aluminum cooling vanes (J) were used to keep the contents within the external sealing container near room temperature while flowing helium gas also provided cooling during expansion tests. The container was attached at one side of an aluminum sealing disk (H) while the other side of the disk had the furnace silica tube attached. Neoprene “O” rings provided air tight seals. Helium gas was used to purge the contents within the silica tube prior to thermal expansion tests, but no helium flowed in that tube or the CTE measuring tube or the CTE measuring rod during testing. The reason for this is that gas flow would cause significant temperature differences between adjacent surfaces of the CTE measuring tube and CTE measuring rod, the specimen, and the platinum thermometer. Positive helium pressure caused by flowing helium within the air tight container prevented air from entering the silica tube contents.
Calibration and corrections
The high temperature dilatometer was calibrated with NIST fused silica 739 and NIST stainless steel SRM 738. The reason for calibrating with these two materials was that the pure silicon thermal expansion was 2074.0 µstrain which was between the two NIST specimens used for calibration. The total thermal expansion of pure silicon at 6000C was 2,107.2 µstrain using only the NIST fused silica 739 calibration data. The maximum difference between the NIST reported value for thermal expansion and measured thermal expansion between 293K and 873K for fused silica was 1.07 µstrain and for stainless steel it was 2.8 µstrain, see Tables 1 and 2.
Table 1
Comparison between NIST fused silica 739 and AML calibration curve
Temperature, 0K
|
Total thermal expansion, ΔL/L293, microstrain
|
NIST fused silica
|
AML calibration
|
Difference
|
293
|
0
|
0
|
0
|
320
|
13.5
|
13.42
|
-0.08
|
340
|
24.5
|
24.03
|
-0.47
|
380
|
36
|
35.63
|
-0.37
|
420
|
72
|
71.58
|
-0.20
|
460
|
97
|
96.67
|
-0.33
|
500
|
122
|
121.89
|
-0.11
|
560
|
159
|
159.97
|
0.97
|
640
|
206
|
206.88
|
0.88
|
720
|
249
|
247.93
|
-1.07
|
800
|
288
|
288.27
|
0.27
|
840
|
307
|
306.91
|
-0.09
|
Table 2
Comparison between NIST stainless steel SRM 738 and AML calibration curve
Temperature, 0K
|
Total thermal expansion, ΔL/L293, microstrain
|
NIST stainless steel
|
AML calibration
|
Difference
|
293
|
0
|
0.58
|
0.58
|
300
|
69
|
68.99
|
-0.01
|
340
|
466
|
465.5
|
-0.5
|
380
|
872
|
872.8
|
0.8
|
420
|
1288
|
1289.5
|
1.5
|
460
|
1714
|
1715.7
|
1.7
|
500
|
2149
|
2150
|
1.3
|
540
|
2593
|
2593.6
|
0.6
|
580
|
3048
|
3045.8
|
-2.2
|
620
|
3511
|
3508.2
|
-2.8
|
660
|
3984
|
3981.7
|
-2.3
|
700
|
4467
|
4468.2
|
1.2
|
The standard deviation for the difference between the AML calibration and the NIST fused silica is 0.5860 µstrain and 1.5904 µstrain for the NIST stainless steel.
The cylindrical specimens of NIST fused silica 739 and the NIST stainless steel SRM738 each had a length of 2.525 centimeters and a diameter of 0.635 centimeters. The rate of warming and cooling was controlled by the furnace controller at 10C/minute and thermal expansion measurements were made every three degrees Celsius which was the minimum rate of the furnace controller. Below 2000C the rate of cooling was slower due to the heat capacity of the furnace and the low rate of heat transfer between the furnace and surrounding air. Two calibration runs were made for the fused silica and three for the stainless steel. The expansion results were generated by a computer program using the measured calibration data, see Tables 1 and 2. The reason for using both NIST fused silica and NIST stainless steel was to calibrate the dilatometer over a large range of thermal expansion that bracketed the thermal expansion for silicon.
Corrections were made for tilt angle between the capacitor plates and the tilt angle was kept constant for all test at 0.0049 radians by measuring the separation of the plates top and bottom with a microscope. The angular position of the capacitance plates was kept the same for each test. Corrections were made using the bellows force, with a spring force of 786 grams/mm with a spring constant of 3.82 grams/µm, and the elastic constants of the fused quartz rod and tube and specimen during thermal expansion changes. Changes in thermal expansion of the capacitor plates were also corrected using the temperature measurements made by the diode thermometer. The line capacitance was 0.001066 pF and the conductive loss was 0.0019 nanosiemens for a capacitance of 13pF. Fringing fields were considered negligible. There were 14 error tests performed with two NIST quartz calibration tests, two silicon tests, and ten silicon carbide tests. At around 320K the average closure error in thermal expansions was 6.086 microstrain with a standard deviation of 4.355 microstrain. With the error between tests of the same material was 10.87 microstrain with a standard deviation of 3.210 microstrain. The maximum difference between the warming and cooling curves was within 7 microstrain. This small hysteresis difference indicates that the frictional forces between the CTE measuring rod and tube were minimal as well as a small temperature difference between the specimen and platinum thermometer while heating compared to cooling. Calculations for the thermal expansion error due to the frictional force created by movement between the rod and tube was 7x10− 6.
Experimental procedure
The dilatometer was taken out of the surrounding silica tube that remained in the furnace and the external sealing container (Q) was removed. It was found that the friction between the sides of the specimen and tube was high if the specimen (M) rested on the CTE measuring tube. Therefore, two Teflon shims, each 0.005 centimeters thick, were placed at the base of the opening of the tube and then the specimen was placed on top of the shims between the CTE measuring rod and the CTE measuring tube.
Two stainless screws were loosened so that a brass shim 0.0518 centimeters thick could be placed between the aluminum plate (B) and frame (P). Then the screws were tightened. The nylon screw in the brass ring (E) was loosened so that the rod could move freely in both axial and radial directions. The rod was rotated until a scribed mark on the rod aligned with a scribed mark on the rod capacitor plate. In this way the radial orientation remained the same for every test. The rod was then pressed against the specimen and the nylon screw was tightened. The stainless screws (B) were then loosened and the brass shim was removed. Then the screws tightened the aluminum plate against the frame providing a clamping force of 410 grams upon the specimen via the bellows and CTE measuring rod. The Teflon shims were then removed, bottom one first, leaving the specimen suspended between the round end of the rod (A) and the tube (K), thereby minimizing the chance of moving the specimen. This procedure eliminated hysteresis loops during thermal expansion tests. The rod capacitor plate was then gently moved until the capacitance was between 12 and 14 pf resulting in a plate separation between 0.041 and 0.035 cm.
The external sealing container was replaced and the entire contents within the container and furnace tube was purged with helium gas. Then the contents within the furnace tube was then sealed with helium under pressure and inserted into the furnace. This resulted in no flow of helium gas within the specimen chamber. It was discovered that the flow of helium gas surrounding the specimen caused significant errors in temperature measurements resulting in a large hysteresis between heating and cooling data. The furnace was increased and decreased in temperature 10C/minute with the furnace controller. Thermal expansion measurements were made for every 30C temperature change.