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Tests of steel arch and rock bolt support resistance to static and dynamic loading induced by suspended monorail transportation

INFORMAZIONI SU QUESTO ARTICOLO

Cita

Introduction

At present, suspended monorail systems constitute a very common means of transportation in the Polish hard coal mines.[1,2] The main advantages of the suspended monorail include the independence of the route from the working floor surface irregularities and the possibility to transport cargo of significant mass and size.

The masses and dimensions of machines and devices transported via monorail have increased considerably in recent times. This is particularly related to the transport of longwall system elements and road support elements. For the most part, the mass of the transported cargo loads the frame of the ŁP support, and in some cases, also the rock bolts that are used as support reinforcement elements. Fig. 1 presents an example view of a route of a suspended monorail with a transport of steel arches that load the ŁP yielding steel arch support frame.[3]

Figure 1

Example view of a route of a suspended monorail with a transport of steel arches that load the ŁP yielding steel arch support frame.

Fig. 2 presents the mine working diagram with suspended monorail. The dynamic influence of the vibrating transported cargo on the support elements is particularly visible during the sudden braking of the monorail. Experience shows that the vibrations of the transported cargo occur not only in the travel direction of the monorail, which results primarily in deformations of the monorail route,[4] but also in the direction of gravity.

Figure 2

Mine working diagram with transportation via suspended monorail.

The influence of loads on the support in the direction of gravity may affect the support elements in various ways, such as: support frame camber beam deformation,[5] significant yields in the joints, as well as the tension, bending and shearing of the rock bolts reinforcing the ŁP support camber beams. This is why the article focuses on the analysis of the operational characteristics of the support frame sliding joint and the yielding bolts subjected to static and dynamic loads, in order to present the various influence that loading may have on the support. Fig. 3 presents an example diagram of the loading of a sliding joint of an ŁP yielding support frame reinforced by means of rock bolts via short joists with a force F that results in its yield.

Figure 3

Loading diagram of the ŁP yielding support frame joint and bolts.

In Poland, the maximum speed of suspended monorail travel is 2 m/s. Due to the fact that preparations are currently underway to increase the maximum speed above 2 m/s, it is necessary to inspect what influence it will have on work safety and mining support stability.

Current operational experience and tests have shown that dynamic loads induced by suspended monorail transportation have a significant influence on the roadway support stability and working protection durability and on the monorail operators.[4,5] This is particularly true during the emergency braking of a suspended monorail by means of a braking trolley, where the overloads reach 3g.

Bench tests of selected steel arch and rock bolt support elements utilised in the Polish hard coal mines were conducted in order to determine the resistance of steel arch and rock bolt supports to static and dynamic loads.

The article presents the results of tests conducted on a steel arch support in the form of the sliding joints[6,7,8] of an ŁP/V29 (ŁP-type yielding steel arch support frame constructed from a V29 section), which is commonly employed in the Polish hard coal mines. Tests of elements of threaded bolts with trapezoidal threads over the entire rod length were conducted as well. The tests were conducted under static and dynamic loading.

Instrumentation of an existing GIG drop hammer (test method with the free fall of mass) facility for steel arch and rock bolt support tests[9,10,11] was carried out as well, together with the development of a methodology enabling the testing of bolt rods under dynamic bending and shearing loads.

Bench Test Methodology and Results
Bolt rod tensile strength under static load

Bolt rod tests were conducted according to the applicable Polish standards[12,13] in a tensile testing machine with digital force and displacement registration. The tests under static load were carried out using a ZD100Pu-type static testing machine. The force measurements were carried out via a strain gauge force sensor (accuracy class 0.5), while displacement measurements were carried out via a potentiometric sensor (accuracy class 1). The measuring sensors were connected to a measuring amplifier (accuracy class 0.03) coupled to a computer. The measurement data was recorded on the computer with a sampling frequency fs=10 Hz.

The following elements of the bolt (Fig. 4) were tested:

Figure 4

Bolt rod and nut: (a) – view of the rod with the nut; (b) – drawing of the rod with a trapezoidal thread and sectional view.

bolt rod with a trapezoidal thread (13 mm thread pitch) over the entire 2 m length, 21.3 ÷ 21.8 mm minor diameter and 25.1 mm maximum trapezoidal thread outer diameter,

50 mm tall nut (13 mm thread pitch).

The result of the bolt rod test under static tensile loading is presented in Fig. 5.

Figure 5

Bolt rod test under static tensile loading: (a) – loading course as a function of bolt rod elongation; (b) – ruptured rod after the test.

The length of the studied bolt rod during testing was approx. 2000 mm. The maximum force registered during the test was Fsmax = 271 kN, while the rupture occurred at an elongation of L = 112 mm.

In order to determine the load capacity of the rod-and-nut assembly, tests were conducted according to Fig. 6.

Figure 6

Test stand diagram for bolt tests under static load.

Results of the three rod-and-nut assembly load capacity tests are presented in Fig. 7 and Table 1.

Figure 7

Courses of load as a function of elongation under static load.

Results of the rod-and-nut assembly load capacity tests.

Test numberMaximum load value Fsmax kNBolt elongation f corresponding to Lmax mmPost-test inspection
124756.9Bolt nut
223438.1thread shearing
323643.3

Nut thread shearing was observed during the tests, which was the main cause of bolt load capacity loss. At the same time, it was determined that the bolt rod thread exhibited slight superficial marks after the test, generated as a result of the shearing. This suggests that it may be possible to obtain greater bolt-and-nut assembly load capacity by using nuts with better mechanical properties and by fitting the rod-and-thread nut contact areas better (the rod coarse thread was produced by rolling).

Bolt rod tensile strength under dynamic load

The bolt tests were conducted at a drop hammer test facility, depicted as a diagram in Fig. 8.

Figure 8

Test facility diagram.

The principle of the bolt tensile strength tests under dynamic loading is the free fall of the mass m1 = 4000 kg onto the cross-bar with a mass m2 = 3300 kg (statically loading the tested bolt) from a height h.

The bolt impact velocity v during the test is calculated from the following formula:

v=2gh,m/s$$v=\sqrt{2gh},\,{m}/{s}\;$$

where: g – gravitational acceleration 9.81 m/s2.

During bolt tests under tensile impact loads, the bolt dynamic resistance force Fd and rod elongation L are registered with a sampling frequency fs = 9600 Hz. The maximum value Fdmax of the bolt dynamic resistance force Fd at a given impact velocity v is determined during the test.

Each tested bolt is subjected to a series of dynamic loads, starting from a drop height h = 1 cm; then h = 2 cm, and so on, until its failure.

The bolt test results are presented in Fig. 9 and in Table 2.

Figure 9

Courses of load as a function of time under dynamic tensile loading of the bolt rods.

The result of the bolt rod test under dynamic tensile loading.

Test numberDrop mass m1, kgCross-bar mass m2, kgDrop height h, mImpact velocity v, m/sMaximum load value Fdmax, kN Post-test inspection
1400033000.010.44110The rod and nut were not
20.020.63136destroyed
30.030.77164
40.040.89200
50.050.99204Bolt nut thread shearing and cracking

A chart depicting the relation of the maximum force Fdmax as a function of impact velocity v is presented in Fig. 10.

Figure 10

Relation of the maximum force as a function of impact velocity.

Failure of the bolt nut as a result of the dynamic force’s shearing of the thread occurred at Fdmax = 204 kN and impact velocity v = 1 m/s. Thread wear marks on the inside of the nut indicate an uneven distribution of the thread loading, which is typical for this kind of threaded bolt with a rolled thread not covering the entire rod circumference. The results indicate a 16% decrease in bolt strength parameters under dynamic loading (average load capacity is 200 kN) compared to static load (average load capacity is 239 kN).

Bolt rod shear strength under static and dynamic load

Bolt rod shear tests under static and dynamic loads were conducted at a test stand presented as a diagram in Fig. 11. The tests used the same shearing instrument, which was in accordance with the applicable Polish standard.[13] The bolt samples for shear tests were 250 mm long. The shear load was exerted on the segment of the bolt by means of a punch with a diameter of 75 mm.

Figure 11

Diagram of the test stand for bolt rod shear tests under: (a) – static load; (b) – dynamic load.

The principle of the bolt shear strength test under dynamic loading is the free fall of the mass m1 = 2500 kg directly onto the bolt rod from a height h.

The bolt impact velocity v during the test is calculated from the formula (1).

During bolt tests under shear impact loads, the bolt dynamic resistance force Fd and phenomenon time t are registered with a sampling frequency fs = 19200 Hz. The maximum value Fdmax of the bolt dynamic resistance force Fd at a given impact velocity v is determined during the test. The result of the bolt rod test under static shear loading is presented in Fig. 12.

Figure 12

Relation of load as a function of bolt rod displacement during its shearing (maximum shearing force Fsmax = 229 kN).

The average maximum shearing force obtained during the shear tests under static load was Fasmax = 225 kN.

The result of the bolt rod test under dynamic shear loading is presented in Fig. 13, while a result compilation is presented in Table 3. They are comparable with the average bolt rod static shearing force.

Figure 13

Relations of load as a function of time under dynamic shear loading of the bolt rods.

The result of the bolt rod test under dynamic shear loading.

Test numberDrop mass m1, kgCross-bar mass m2, kgDrop height h, mImpact velocity v, m/sMaximum load value Fdmax kNPost-test inspection
1250000.071.17194the rod was not shorn
20.081.25213the rod was shorn
30.091.33227
40.11.40228
50.121.53229

A chart depicting the relation of the maximum force Fdmax as a function of impact velocity v is presented in Fig. 14.

Figure 14

Relation of the maximum shearing force and impact velocity.

The rod was not shorn at impact velocities up to v = 1.17 m/s, while the maximum force amounted to Fdmax = 194 kN. Rod shearing occurred at impact velocity v = 1.25 m/s, while maximum shearing force amounted to 213 kN. The force increased slightly at higher impact velocities until it reached approximately 230 kN.

Bolt rod bending strength under static and dynamic load

Bolt rod bending strength tests under static load were conducted in a test stand presented in Fig. 15, while the stand for tests under dynamic load is presented in Fig. 16.

Figure 15

Test stand for bolt rod bending strength tests under static load.

Figure 16

Test stand for bending strength tests under dynamic load: (a) – rod bending by an angle smaller than 90°; (b) – rod bending by 90°.

The tests used the same bending instrument. A 200 mm long bolt rod sample is propped in the testing device on the surfaces of the device, which produce an angle of 90°. Static and dynamic load is applied to the bolt until the rod bends by 90°. The main objective of the tests was to inspect whether the steel bar used to form the bolt rods would rupture.

The principle of the bolt bending strength test under dynamic load is the free fall of the mass m1 = 2500 kg directly onto the bolt rod from a height h.

The bolt impact velocity v during the test is calculated from the formula (1). The load is applied by a 60 mm diameter roll.

During bolt tests under bending impact loads, the bolt dynamic resistance force Fd and phenomenon time t are registered with a sampling frequency fs = 4800 Hz. The maximum value Fdmax of the bolt dynamic resistance force Fd at a given impact velocity v is determined during the test.

The result of the bolt rod bending test under static load, with bending by 90°, is presented in Fig. 17.

Figure 17

Course of load as a function of bolt rod displacement during its bending (maximum bending force Fsmax = 26.3 kN).

The average maximum bending force obtained during the bending tests under static load was Fasmax = 28.1 kN.

The result of the bolt rod test under dynamic bending loading is presented in Fig. 18, while a result compilation is presented in Table 4. They are comparable with the average bolt rod static bending force. The differences occur only in the first peak for the dynamic load, the value of which is greater than the load corresponding to the yield stress at static load.

Figure 18

Courses of load Fd as a function of time t under dynamic bending loading of the bolt rods.

The result of the bolt rod test under dynamic bending loading.

Test numberDrop mass m1, kgCross-bar mass m2, kgDrop height h, mImpact velocity v, m/sMaximum load value Fdmax kNPost-test inspection
1250000.010.4429.7The rod was not bent by 90° The sample did not rupture
20.020.6329.4The rod was bent by 90°
30.030.7732.1The samples did not rupture
40.040.8930.2
ŁPV29 support frame sliding joint load capacity under static and dynamic load

V29 sliding joint static load capacity tests were conducted according to the applicable standard[14] in a tensile testing machine for static testing where loading is applied by means of a hydraulic actuator. The strain gauge force sensor (accuracy class 1) and potentiometric displacement sensor (accuracy class 1) were connected to a measuring amplifier (accuracy class 0.03) coupled to a computer. The measurement data was recorded on the computer with a sampling frequency fs = 5 Hz.

The principle of the V29 sliding joint dynamic resistance test is the free fall of the drop mass (ram) m1 = 4000 kg from a height h onto a cross-bar with a mass m2 = 3300 kg, which applies static load to the joint mounted in the test facility. The height h was progressively increased until the total sliding joint yield was achieved. Fig. 19 presents a sliding joint constructed from two segments of a V29 section, coupled in an approx. 0.6 m long overlap by means of two SDO29-type shackles (the tightening torque of the shackle screws was Md = 350 Nm). The total height of the coupled V29 sections was 4.8 m.

Figure 19

Diagram (left) and view (right) of the facility for sliding joint tests under dynamic load.

The test result for the joint constructed from V29 sections under static load is presented in Fig. 20.

Figure 20

Course of load as a function of joint displacement under static load (maximum loading force Fsmax = 213 kN).

After the first force peak of 213 kN, a systematic decrease in load capacity to approximately 160 kN occurs, which is an adverse effect signifying the loosening of shackle screws.

A similar effect occurs during testing under dynamic load. Results of the tests of joints constructed from V29 sections are presented in Fig. 21, while a result compilation is presented in Table 5.

Figure 21

Course of load Fd as a function of time t under dynamic load of the joint at heights: h = 10 cm (a) and h = 30 cm (b).

The test result for the joint constructed from V29 sections under dynamic load.

Test numberDrop height h, mImpact velocity v, m/sSectionNumber of shacklesNut tightening torque, NmMaximum load capacity Fdmax , kN Comments
10.11.4V292350197the joint stopped after
approx. 10 cm
20.22.8206total joint yield
30.34.2197

The maximum impact velocity that does not produce total yield should not exceed v = 1.4 m/s. This is confirmed by the course depicted in Fig. 21(a), where the dotted lines indicate the tendency of the force Fd that is subjected to damping. Greater impact velocities depicted in Fig. 21(b) result in total joint yield, caused primarily by the loosening of the shackle screws. Joint load capacity, visible in the form of high peaks (Fig. 21(b)), often decreases to approximately 100 kN, while at times it can decrease to nearly zero, which is a result of the loss of contact between the prop and the cross-bar and ram that exert load upon it.

In the case of an impact mass m = m1 + m2 = 7700 kg acting dynamically upon the sliding joint formed of a V29 section with two shackles, at velocities v ≥ 2.8 m/s (course in Fig. 19(b) and Fig. 21(b), the sliding joint is not able to stop the momentum of the impact mass.

Summary

The conducted resistance tests of steel arch and rock bolt support elements under static and dynamic load have shown that dynamic load has decisive influence on the support’s retaining of its stability. Support element stability decreases along with the increase of the impact velocity. This concerns both the steel arch support and the rock bolt support.

The results of rock bolt tests under dynamic tensile loading with an impact velocity v = 1 m/s demonstrate a decrease of the strength parameters of the bolts by 16% in relation to static loading.

At impact velocities of up to v = 1.17 m/s, the bolt rod was not shorn. The shearing of the rod occurred only at an impact velocity v = 1.25 m/s, while the maximum shearing force was 213 kN. At greater impact velocities, the force increased slightly until it reached a value Fdmax = 229 kN, which was equal to the maximum force Fsmax obtained under static loading.

The results of bolt rod tests under dynamic bending loads were comparable to the average static bending force exerted on the bolt rods. Differences occurred only at the first peak during dynamic loading, the value of which was greater than the load corresponding to the yield point under static loading. None of the bolt rod samples ruptured during testing.

The tests of a sliding joint under dynamic loading demonstrated that the beginning of the yield occurred at a force lower than that required under static loading. The maximum impact velocity not resulting in total yield should not exceed v = 1.4 m/s. Impact velocities v ≥ 2.8 m/s lead to total joint yield, resulting primarily from the loosening of the shackle screw nuts. Such a state can lead to a loss of support stability and result in the caving of a mine working as well as a major accident during transport via suspended monorail.

In order to guarantee safety during suspended monorail travel at speeds exceeding the currently permitted Vmax = 2 m/s, it is recommended to carry out a selection of a support by a scientific research body, which will select the support and prepare an optimal technical solution for the intended maximum travel speed.

Further, resistance tests of steel arch and rock bolt support elements to static and dynamic loads are planned for the future, in order to determine their operational characteristics at various load rates.

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