Results of Experiments on Measuring Displacements and Stresses in Pressure Gauge Springs

G. I. TYZHNOV, V. K. KHRULEV
Submitted 1970 | SovietRxiv: ru-197001.09569 | Translated from Russian

Abstract Generated abstract

This paper reports experiments designed to verify existing theories for tubular Bourdon pressure gauge springs by measuring displacement sensitivity and stresses. Springs of flat oval and oval cross section, with nominal pressures from 1 to 100 kgf/cm², were tested, and measured travel per atmosphere and surface stresses at two points on the minor axis were compared with calculations from a published formula. The results show varying agreement: calculated displacement sensitivities range from substantial underestimation at low pressures to close agreement at higher pressures, while calculated stresses often differ appreciably from measured meridional, circumferential, and equivalent stresses. The data provide comparative experimental benchmarks for assessing theoretical models of pressure gauge spring deformation and strength.

Full Text

RESULTS OF EXPERIMENTS ON MEASURING DISPLACEMENTS AND STRESSES IN PRESSURE-GAUGE SPRINGS

G. I. TYZHNOV, V. K. KHRULEV

(Presented by the scientific seminar of the Department of Strength of Materials)

To verify the theories [1, 2, 3] of tubular pressure-gauge springs, experiments were carried out to measure displacements and stresses. The dimensions of the tested springs, their parameters, and the results of the experiments are summarized in the table, where $R$ is the mean radius of the spring, $h$ is the wall thickness, $a$ is the major semiaxis of the section, $b$ is the minor semiaxis, $\gamma$ is the working angle of bending of the spring (the nonworking sections at both ends, $8^\circ$ each, have been discarded [4]), and $\eta$ is the principal parameter of the spring.

Column 11 gives data on the displacement sensitivity of the springs, i.e., the amount of travel per atmosphere. Columns 12 and 13 present the results of calculating this sensitivity by the formula in [3]. Columns 14–25 contain the experimental data on stress measurements and the results of calculations of these stresses [3]. Columns 16, 19, 22, and 25 give the calculated equivalent stresses, computed according to the energy theory of strength:

$$ \sigma_{\mathrm{e}}=\sqrt{\sigma_1^2+\sigma_2^2-\sigma_1\sigma_2}. $$

Stresses were measured only at 2 points located at the ends of the minor axis of the section on the outer surface: at point $A$—on the convex side, and at point $B$—on the concave side of the spring.

The stress $\sigma_1$ is meridional, i.e., directed along the central axis of the spring, while $\sigma_2$ is circumferential, perpendicular to the central axis. To measure the strains $\varepsilon_1$, ordinary gauges with a base of 10 mm were used, and to measure the strains $\varepsilon_2$, specially made gauges with a base of 3 mm were employed.

When measuring strains on thin parts with strain gauges, it is necessary to take into account the influence of the thickness of the gauge.

The springs for a pressure of 100 atm had a modulus of elasticity $E=1.3\cdot10^4\ \text{kgf}/\text{cm}^2$; the remaining springs were made of brass, for which $E=10^4\ \text{kgf}/\text{cm}^2$. Poisson’s ratio was taken to be the same, $\mu=0.3$.

REFERENCES

  1. V. I. Feodos’ev. Calculation of thin-walled Bourdon tubes of elliptical section by the energy method. Oborongiz, 1940.

  2. V. I. Feodos’ev. Elastic Elements of Precision Instrument Engineering. Oborongiz, 1949.

  3. L. E. Andreeva. Elastic Elements of Instruments. Mashgiz, 1962.

  4. A. I. Chinarev. Investigation of the deformation of the minor axis and the opening angle of a pressure-gauge tubular spring of flat section. In: Prospects for the Development of Elastic Sensitive Elements. TsINTI, Moscow, 1961.

Nominal pressure \(p\), kgf/cm² Connection shape \(P\), mm \(h\), mm \(a\), mm \(b\), mm \(\gamma^\circ\) (working) \(\dfrac{a}{b}\) \(\dfrac{h}{b}\) \(\eta=\dfrac{Rh}{a^2}\) Sensitivity by travel, mm: experiment Sensitivity by travel, mm: calculated [3] Sensitivity by travel, mm: error of calculation, % Stress at point \(A\), kgf/cm²: from experiment \(\sigma_1\) Stress at point \(A\), kgf/cm²: from experiment \(\sigma_2\) Stress at point \(A\), kgf/cm²: from experiment \(\sigma_3\) Stress at point \(A\), kgf/cm²: calculated [3] \(\sigma_1\) Stress at point \(A\), kgf/cm²: calculated [3] \(\sigma_2\) Stress at point \(A\), kgf/cm²: calculated [3] \(\sigma_3\) Stress at point \(B\), kgf/cm²: from experiment \(\sigma_1\) Stress at point \(B\), kgf/cm²: from experiment \(\sigma_2\) Stress at point \(B\), kgf/cm²: from experiment \(\sigma_3\) Stress at point \(B\), kgf/cm²: calculated [3] \(\sigma_1\) Stress at point \(B\), kgf/cm²: calculated [3] \(\sigma_2\) Stress at point \(B\), kgf/cm²: calculated [3] \(\sigma_3\)
1 flat-oval 52,9 0,32 10,3 1,91 258 5,41 0,16 0,158 4,90 3,32 −32 122 103 114 380 306 349 −25 134 148 −252 118 327
1 flat-oval 53,4 0,30 10,3 1,97 258 5,21 0,14 0,151 5,20 3,54 −32 138 158 150 404 320 369 −82 105 162 −273 117 346
2 flat-oval 52,9 0,39 10,2 1,85 252 5,51 0,21 0,197 3,0 2,47 −17 231 285 262 579 526 555 −91 286 341 −346 249 517
2 flat-oval 52,3 0,39 10,2 1,78 255 5,75 0,21 0,194 3,1 2,52 −18 229 278 257 573 517 548 −68 357 396 −347 244 518
6 flat-oval 53,6 0,71 9,9 2,04 252 4,84 0,34 0,389 0,94 0,77 −18 368 667 578 687 900 815 68 862 828 −236 640 784
6 flat-oval 53,1 0,71 9,9 2,02 250 4,90 0,35 0,384 0,94 0,78 −16 360 664 575 687 895 814 57 854 837 −235 620 766
16 flat-oval 53,7 1,00 9,8 1,75 254 5,60 0,57 0,560 0,39 0,39 0 406 867 752 923 1447 1270 157 1077 1007 −154 1260 1340
16 flat-oval 54,6 1,03 9,8 1,73 251 5,64 0,59 0,587 0,38 0,38 0 391 853 726 870 1390 1220 156 1078 1008 −124 1095 1160
25 flat-oval 53,0 1,22 9,8 1,71 249 5,74 0,71 0,672 0,23 0,24 4 495 963 834 954 1600 1390 175 1065 990 −74 1290 1330
40 oval 53,6 1,40 9,5 2,0 256 4,75 0,70 0,843 0,14 0,15 6 692 1750 1520 807 1840 1590 499 1950 1750 247 1670 1560
60 oval 53,6 1,85 9,8 2,07 256 4,72 0,89 1,03 0,068 0,077 13 630 1680 1470 725 1750 1520 547 1930 1730 291 1630 1510
100 flat-oval 53,2 1,78 9,3 1,80 253 5,17 0,98 1,08 0,054 0,054 0 1020 2600 2270 1500 3100 2680 693 2880 2600 245 2740 2630
100 flat-oval 53,5 1,78 9,3 1,80 253 5,17 0,98 1,10 0,053 0,054 2 1060 2770 2420 1490 3080 2670 707 2840 2560 246 2750 2630

Submission history

Results of Experiments on Measuring Displacements and Stresses in Pressure Gauge Springs