Perfect Accelerometer Mounting Check (AMC)

The Accelerometer Mounting Check (AMC) – based on Brüel & Kjær’s patented technology – provides an easier and faster way of testing accelerometer mounting and verifying, that your transducers mounted correctly, replacing lengthy visual and manual inspection. Let’s dive into the details.

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Table of content

Achieving accuracy
Perfect Accelerometer Mounting
Analysing the Mounted Resonance Frequency
Benefits of Accelerometer Mounting Check
- How Accelerometer Mounting Check Works

Achieving accuracy

To achieve accuracy in all measurements, the physical mounting of accelerometers on a test structure is the first, and often most problematic link in the measurement chain. Problems here will corrupt the measurement and cannot be corrected later.

The Accelerometer Mounting Check (AMC) – based on Brüel & Kjær’s patented technology – provides an easier and faster way of testing accelerometer mounting and verifying, that your transducers are mounted correctly, replacing lengthy visual and manual inspection.

Let’s dive into the details.

Perfect Accelerometer Mounting

The Theory Behind The Technology

We model an accelerometer mounted on a structure as a mass-spring-damper system where m_s, m_b and m_t are the seismic mass of the accelerometer, the mass of its base and the mass associated with the test object, respectively (Figure 1). The two first masses are connected by a spring with stiffness k_PZ that represents the piezoelectric element.

Figure 1: Type 4533-S and mass-spring-damper system

A spring/damper element k_Mis added to model the influence of the test object. The masses can move along the vertical axis, and their coordinates are x_s, x_band x_t, respectively. The easiest way to derive the equations of motion is to use Lagrange’s equations.

First we construct the Lagrangian L=T-V, where T and V are kinetic and potential energy of the system:

With no external forces acting on the system and omitting dissipation.

The Lagrange equation is:

Where x_j is one of the coordinates x_s, x_b and x_t. Differentiation yields three equations of motions.

In matrix notation these are:

Or in a more compact format:

The system has three degrees of freedom (DOF), one of them being the rigid-body motion of the assembly. Following the AMC approach, a periodic electrical charge is applied to the piezoelectric element, making it contract and expand. This applies forces (denoted by the grey arrows in Figure 1) acting on the seismic mass and base.

Simultaneously, AMC measures the response of the accelerometer, which is proportional to the deformation of the piezoelectric element (x_s- x_b) and calculates the AMC FRF between the response and applied charge.

It is possible to obtain the AMC FRF analytically. As the elements of the matrix [α(ω)]=([K]-ω² [M])^-1 are the FRFs between the corresponding DOFs, the AMC FRFs can be combined from the elements of [α(ω)] = ([K] - ω² [M])^-1 are the FRFs between the corresponding DOFs, the AMC FRFs can be combined from the elements of [α(ω)].

Figure 2 illustrates AMC FRFs computed for three important scenarios: A properly mounted accelerometer, a free hanging accelerometer and the accelerometer properly mounted on a structure made of a light material (like wood) or on thin metal or plastic plate. Comparing the measured curves, AMC is able to detect the mounting quality.

Figure 2: AMC frequency response functions

Analysing the Mounted Resonance Frequency

The plot sketches the AMC FRF (yellow curve) when the accelerometer is perfectly mounted on an infinitely heavy object (k_M→ ∞, m_t→ ∞). The FRF has a peak at mounted resonance frequency, ω_MR²= k_PZ/m_s. The grey curve represents the FRF of free hanging accelerometer (k_M→ 0); it has a peak at ω_FH²= k_PZ (m_b+ m_s) / (m_s m_b). For a typical accelerometer m_b≈ m_s, and ω_FH≈ √2 ω_MR, [Ref. 2].

Before initiating AMC, one needs to make sure that the accelerometer is properly mounted on the structure. When initiated, AMC looks up the value of the mounted resonance frequency in the transducer database and generates a swept sine excitation in the range around ω_MR (the white region).

The measured AMC FRF, which should be close to the yellow curve, is stored as a reference. Occasionally, the procedure is repeated, and the newly measured AMC FRF is compared with the reference curve.

If during the test, an accelerometer falls off the structure, its AMC FRF will rather look like the grey curve that corresponds to the free hanging accelerometer; the algorithm detects if the two curves significantly differ in the white region and asks the user to check the accelerometer mounting.

If the accelerometer is mounted on a structure made of light material, the reference AMC FRF may look like the blue curve (k_M→ ∞, m_t small). In the white region, it is almost impossible to distinguish it from the free hanging AMC FRF, and thus the AMC can fail.

To prevent this, the BK Connect™ software introduces a pre-test wizard to recognize such situations.