1
Foundation & Geotechnical Engineering, LLC Specializing in Deep Foundation Engineering” 712 East Alsobrook Street, Suite 3 · Plant City, Florida 33563 · Phone (813) 759-2426 · Fax (813) 759-2427 New Rapid Load Test FGE is proud to offer a new line of rapid load testing, simply called the RLT, capable of up to 400 tons. The innovative RLT system makes use of a patent pending load pack that converts drop energy into a long-duration load pulse and thereby availing simplified kinematic data reduction methods 1 . Fig. 1 shows results of three consecutive load cycles on a shallow footing. Note load duration exceeds 100 msec making it ideal for present data analysis methods. -50 0 50 100 150 200 250 300 0.15 0.20 0.25 0.30 0.35 0.40 0.45 Time (s) Load (tons) -445 55 555 1055 1555 2055 2555 Load (kN) Cycle 1 5' Drop Cycle 2 5' Drop Cycle 3 10' Drop Figure 1 Long-duration RLT Load Pulses The development of this device has been funded solely by FGE who contracted the University of South Florida to aid in development of key components and conduct independent verification testing. Components The RLT system has three main components which include: the load pack, a drop weight (mass) and a suspension/guide tower. Load Pack. The loading assembly, which is mounted directly to the top of the foundation, is comprised of a specially designed attenuator assembly and a series of load cells for redundant measurements. The pack design is modular allowing for future larger load ranges. The present system is suitable for 100 to 400 ton loads, with future systems approaching 2000 tons. Drop Mass. The mass assembly is modular providing for optimal shipping and cost effectiveness and in its current configuration can weigh as much as 14 tons. Specialized RLT software is used to determine the most appropriate mass configurations prior to shipping. 1 Mullins, G., Lewis, C., and Justason, M., (2002). “Advancements in Statnamic Data Regression Techniques,” Deep Foundations 2002: An International Perspective on Theory, Design, Construction, and Performance, ASCE Geo Institute, GSP No.116, Vol II, pp. 915-930. Guide Tower. The tower is used to support the mass at a desired height, as well as guide the mass during the test. It is equipped with a hydraulically actuated quick-release that safely drops the mass at the desired time. Operation Essentially, the test is conducted by suspending the mass from the tower above the loading assembly at a desired height, then releasing the mass by the use of a quick release and allowing it to impact the loading assembly. Upon impact the attenuator assembly is engaged and it transmits the force to the foundation through calibrated load cells in a controlled and relatively prolonged manner producing a load pulse, rather than an impact. The rebound hysteretic response of the attenuator assembly is very efficient at absorbing the energy resulting in drastically reduced subsequent drop heights (Fig. 2). -50 0 50 100 150 200 250 300 0.00 0.50 1.00 1.50 2.00 2.50 3.00 3.50 Time (s) Load (tons) Figure 2 Load Pulse Attenuation Regression Well-known data analysis methods directly apply to RLT data thereby producing equivalent static test results (Fig. 3). -1.50 -1.25 -1.00 -0.75 -0.50 -0.25 0.00 -200 -175 -150 -125 -100 -75 -50 -25 0 Load (tons) Displacement (in.) F_RLT F_RLT-F_ma F_Static Figure 3 Unloading Point Method Analysis 1

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Page 1: Rapid Load Test Flyer - foundations.cc Rapid Load Test Flyer.pdf · New Rapid Load Test FGE is proud to offer a new line of rapid load testing, simply called the RLT, capable of up

Foundation & Geotechnical Engineering, LLC “Specializing in Deep Foundation Engineering”

712 East Alsobrook Street, Suite 3 · Plant City, Florida 33563 · Phone (813) 759-2426 · Fax (813) 759-2427

New Rapid Load Test

FGE is proud to offer a new line of rapid load testing, simply called the RLT, capable of up to 400 tons. The innovative RLT system makes use of a patent pending load pack that converts drop energy into a long-duration load pulse and thereby availing simplified kinematic data reduction methods1.

Fig. 1 shows results of three consecutive load cycles on a shallow footing. Note load duration exceeds 100 msec making it ideal for present data analysis methods.

-50

0

50

100

150

200

250

300

0.15 0.20 0.25 0.30 0.35 0.40 0.45

Time (s)

Load

(ton

s)

-445

55

555

1055

1555

2055

2555

Load

(kN

)

Cycle 1 5' DropCycle 2 5' DropCycle 3 10' Drop

Figure 1 Long-duration RLT Load Pulses

The development of this device has been funded solely by FGE who contracted the University of South Florida to aid in development of key components and conduct independent verification testing.

Components The RLT system has three main components which include: the load pack, a drop weight (mass) and a suspension/guide tower. Load Pack. The loading assembly, which is mounted directly to the top of the foundation, is comprised of a specially designed attenuator assembly and a series of load cells for redundant measurements. The pack design is modular allowing for future larger load ranges. The present system is suitable for 100 to 400 ton loads, with future systems approaching 2000 tons. Drop Mass. The mass assembly is modular providing for optimal shipping and cost effectiveness and in its current configuration can weigh as much as 14 tons. Specialized RLT software is used to determine the most appropriate mass configurations prior to shipping.

1 Mullins, G., Lewis, C., and Justason, M., (2002). “Advancements in Statnamic Data Regression Techniques,” Deep Foundations 2002: An International Perspective on Theory, Design, Construction, and Performance, ASCE Geo Institute, GSP No.116, Vol II, pp. 915-930.

Guide Tower. The tower is used to support the mass at a desired height, as well as guide the mass during the test. It is equipped with a hydraulically actuated quick-release that safely drops the mass at the desired time. Operation Essentially, the test is conducted by suspending the mass from the tower above the loading assembly at a desired height, then releasing the mass by the use of a quick release and allowing it to impact the loading assembly. Upon impact the attenuator assembly is engaged and it transmits the force to the foundation through calibrated load cells in a controlled and relatively prolonged manner producing a load pulse, rather than an impact. The rebound hysteretic response of the attenuator assembly is very efficient at absorbing the energy resulting in drastically reduced subsequent drop heights (Fig. 2).

-50

0

50

100

150

200

250

300

0.00 0.50 1.00 1.50 2.00 2.50 3.00 3.50Time (s)

Load

(ton

s)

Figure 2 Load Pulse Attenuation

Regression Well-known data analysis methods directly apply to RLT data thereby producing equivalent static test results (Fig. 3).

-1.50

-1.25

-1.00

-0.75

-0.50

-0.25

0.00

-200-175-150-125-100-75-50-250Load (tons)

Dis

plac

emen

t (in

.)

F_RLT F_RLT-F_ma F_Static

Figure 3 Unloading Point Method Analysis1