The **accuracy class declared for HBM torque transducers** means that the maximum of those deviations specified as percentages is equal to or less than the value declared as the accuracy class. The sensitivity tolerance is not included.

The **accuracy class** includes the following **metrological properties** explained in detail below:

- Linearity deviation including hysteresis (
*d*)_{lh} - Relative standard deviation of repeatability (
*σ*)_{rel} - Temperature effect (per 10 K) on the zero signal (
*TK*)_{0} - Temperature effect (per 10 K) on the sensitivity (
*TK*_{c})

In transducers with two or more electrical outputs (frequency output and voltage output) the output with the highest accuracy is the **deciding factor in determining the accuracy class**. The accuracy class must not be mistaken for classification according to DIN 51309 or EA-10/14.

The span between the output signal values at nominal torque and at zero torque. Usually **two separate sensitivities** are specified for HBM torque transducers, one for **clockwise torque** and one for **counterclockwise torque**.

*Fig. 1: Sensitivity and nominal torque*

The **sensitivity C** characterizes the slope of the characteristic curve. The characteristic curve is chosen as the straight line connecting the **output signal** S_{M0} determined with mounted but unloaded torque transducer (initial torque signal) and the **output signal **S_{n} at nominal torque determined at increasing torque. This gives the simple equation

*C = S _{n} − S*

**The nominal value characterizing the transducer’s sensitivity**. Usually it is equal for clockwise and counterclockwise torque.

The nominal sensitivity is a value characterizing the respective **transducer’s type** and **measuring range**. However, the actual sensitivity of the individual is equal to the nominal sensitivity only within specified tolerances.

**The permissible deviation of the actual sensitivity from the nominal sensitivity**. It is given as a percentage with respect to the nominal sensitivity.

For **HBM torque transducers** the **actual sensitivity** of the individual is **determined before delivery**. The value is documented in the **test certificate** or **calibration certificate**. For this reason the sensitivity tolerance is not taken into consideration when determining the **accuracy class**.

The temperature effect on the sensitivity is the **variation of the actual output signal** due to a 10 K change in temperature determined at **nominal torque** and related to the **sensitivity**. The specified value is the maximum occurring in the **nominal temperature range**.

The temperature effect on the sensitivity (also called the **temperature coefficient of sensitivity**) is a measure of the temperature effect on the output signal with a load applied to the **transducer**. When determining this value, the output signal has to be **corrected by subtracting the initial torque signal** at the respective temperature. A stationary temperature state has to be established.

The **significant temperature** is the **transducer temperature**. A stationary temperature state as defined at HBM means that the **maximum temperature variation** in a 15-minute period does not exceed 0.1 K. The amount of the deviation is given as a percentage of the actual span of the **output signal** with the **respective torque applied** (in the event of loading with the nominal torque this is the sensitivity).

The **temperature effect on sensitivity** results in a change of slope of the characteristic curve (see Fig. 2). It is of particular importance when a **transducer** is operated at a temperature differing significantly from the reference temperature. For partial load ranges, however, it has very little effect because the resulting deviation acts always as a percentage of the actual output signal span.

Please note that normally the temperature effect on **sensitivity** and the temperature effect on the zero **point** (*TK _{0}*) are superimposed on each other.

Consider a** torque transducer** with 1 kN⋅m **nominal torque**, let the temperature effect on the sensitivity be specified as *TK _{C}* ≤ 0.1 %, the reference temperature as 23 °C and the

If the transducer is operated at a temperature of 33 °C (or 13 °C), the **sensitivity deviation** due to the** temperature variation** may amount to up to 0.1 %.

For a torque of 1 kN⋅m (**nominal torque**) this amounts to a deviation in the displayed value of 1 N⋅m. For a torque of 200 N⋅m, however, the deviation amounts to 0.2 N⋅m only, since the * TK_{C}* is always a

The temperature effect on the zero signal is the **variation**, due to a 10-K change in temperature, in the **unloaded transducer’s output signal** related to the nominal sensitivity. The specified value is the maximum occurring in the nominal temperature range.

The temperature effect on the zero signal (also called the** temperature coefficient of the zero signal**) is determined by measuring the variation due to a 10–K change in temperature in the unloaded transducer’s actual output signal at zero torque after re-establishment of a **stationary temperature state**. The significant temperature is the transducer temperature. A stationary temperature state as defined at HBM means that the **maximum temperature variation** in a 15-minute period **does not exceed 0.1 K**.

*Fig. 2: Temperature effect on the sensitivity TK _{C} and on the zero point TK_{0}.*

The **temperature effect on the zero** signal results in a** parallel shift** in the **characteristic curve** (see Fig. 2). It is of particular importance when a transducer is operated at a temperature differing significantly from the **reference temperature**. By taring or zero balancing at **operating temperature**, the measurement error due to the temperature effect on the zero signal can be eliminated.

Please note that normally the temperature effect on the zero point and the temperature effect on the sensitivity (*TK _{C}*) are superimposed on each other.

Consider a** torque transducer** with 1 kN⋅m** nominal torque**, let the temperature effect on the zero signal be specified as *TK _{0}* ≤ 0.05 %, the reference temperature as 23 °C and the nominal temperature range from +10 °C to +60 °C.

If the transducer is operated at a temperature of 33 °C (or 13 °C), the zero signal deviation may amount to up to 0.05 % of the nominal sensitivity. This corresponds to a **deviation in the displayed value** of 0.5 N⋅m. This deviation is **independent of the torque** with which the transducer is loaded.

Using the transducer at 43 °C may result in a maximum deviation of up to 0.1 % in the worst case.

This does not apply to usage at 3 °C, since this temperature is not within the **nominal temperature range**.

Absolute value of the **maximum deviation of a ****torque transducer****’s characteristic curve** determined with increasing load from the reference straight line which approximates the characteristic curve as a straight line. The specified value is expressed as a percentage of the sensitivity *C*.

For determining the **linearity deviation**, a series of measurements is taken with the load increasing from zero to the **nominal torque**. The reference straight line is the **best-fit straight line** through the initial point, such that the maximum deviations (upward/downward) from the measurement signal have the same amount (see Fig. 3). The specified linearity deviation is the **maximum deviation of the actual output signal from the reference straight line**. It can also be described as half the width of the tolerance band that is symmetrical about the reference straight line.

The linearity deviation has to be taken into consideration because usually when **adjusting the measurement chain**, a **characteristic curve** in the form of a straight line is assumed. It takes maximum effect when a transducer is used for a wide measuring range, in the most extreme case **from zero torque up to nominal torque**.

*Fig. 3: Determination of the linearity deviation*

The linearity deviation including hysteresis specifies the **maximum deviation** (according to absolute value) of the **output signal value** from the reference **straight line**. The reference straight line is the **best-fit straight line** through the starting point (see Fig. 5). Thus, both linearity deviation and hysteresis are taken into consideration. The specified value is expressed as a percentage of the sensitivity *C*.

The **load cycle** for determining the linearity deviation including hysteresis covers the loading of the transducer from zero up to nominal torque and the subsequent relieving down to zero torque (see Fig. 5).

The reference straight line is the best-fit straight line through the initial point, such that the maximum deviations (upward/downward) from the measurement signal have the same amount.

*Fig. 5 Determination of the linearity deviation including hysteresis d _{lh} from a load-relieve cycle*

The linearity deviation including hysteresis can also be interpreted as **half the width of the tolerance band** that is **symmetrical about the reference straight line** (see Fig. 5). The only difference to the procedure for the determination of the linearity deviation *d _{lin}* is that the load cycle here includes also the measurements at

**To determine this value, HBM proceeds as described below:**

- The transducer is
**preloaded with counterclockwise**torque in three load cycles from zero to 100 % of the nominal torque and back to zero torque. The purpose of this**preloading**is to**eliminate the influence of mounting**like settling of bolts and smoothing of contact surfaces - One
**load cycle with counterclockwise torque**and recording of the respective values for the measurement signal at the**predefined load steps**(when testing during production at HBM these steps are at torque 0 %, 50 %, 100 %, 50 % and 0 % of*M*)_{nom} - The transducer is
**preloaded with clockwise torque**in three load cycles from zero to 100 % of the nominal torque and back to zero torque - One
**load cycle with clockwise torque**and recording of the respective values for the measurement signal at the predefined torque steps - The
**best-fit straight line is calculated**according to the above definition, separately for clockwise torque and counterclockwise torque - The amount of the maximum
**deviation**from the best-fit straight line is**determined separately**for clockwise torque and counterclockwise torque

The linearity deviation including hysteresis is of **importance** because normally when adjusting the measurement chain, a characteristic curve in the form of a straight line is assumed. It takes maximum effect if a transducer is used for a wide measuring range and it is not relieved between two relevant measurements. **The most extreme case is the use from zero torque up to nominal torque**.

Consider a** ****T10FS torque flange** of which the maximum permissible linearity deviation including hysteresis is specified as *d _{lh}* ≤ 0.05 % and the nominal sensitivity amounts to 5 kHz. Provided that the

The relative reversibility error is the **difference of the output signals** when measuring the **same torque applied in increasing and decreasing steps** (see Fig. 4). The specified value is the **maximum deviation** (according to absolute value) in the measuring range. It is specified as a percentage of the sensitivity *C*.

The relative reversibility error is a **measure of hysteresis**, that is, the **difference between the characteristic curves determined with increasing and decreasing torque**. For determining the relative reversibility error, a** load cycle** from zero torque through nominal torque and back is recorded. The practical calculation is based on measurements at a number of predefined points in the load cycle (e.g. 0 %, 50 %, 100 % of *M _{nom}*).

Hysteresis describes the **dependency of the measuring signal on the transducer’s loading history**. It is of particular importance if a transducer is used for a wide measuring range and no unloading takes place between acquiring two relevant measurement points. The most extreme case is the use from **zero torque** up to **nominal torque**. The effect of hysteresis occurring during a partial load cycle is usually significantly smaller than the hysteresis during a load cycle covering the entire nominal torque range.

*Fig. 4: Determination of the relative reversibility error d _{hy} from a load-relieve cycle (here based on the load steps 0 %, 50 %, 100 % M_{nom}). The value to be specified is the maximum reversibility error of the given load steps (here d_{hy,0} and d_{hy,50})*

Repeatability describes the property that the **output signal** is the** same for all measurements of the same torque **when measured several times. During the measurements the **mounting position** of the torque transducer shall remain **unchanged** and the torque transducer shall not be mounted and

dismounted (repeat conditions). The standard deviation indicates the average deviation between all measurements of the same torque when measured several times.

The relative standard deviation of repeatability is a measure of the repeatability according to **DIN 1319**. It is defined as the standard deviation of repeatability according to DIN 1319 and is expressed as a percentage of the range of the signal span covered during the testing procedure. It is a statistic measure of

random measurement deviations. For this reason, **all those conditions are kept constant** that, if changed, might cause variations in **systematic measurement deviations** (repeat conditions to DIN 1319).

The determination of the relative standard deviation of repeatability is a **type test** carried out on a** static calibration system** as follows:

- The torque transducer is
**preloaded up to nominal torque**. The measurement signal*S*is taken at nominal torque_{1,100%} - The load is reduced to
**50 % of the nominal load**. The measurement signal*S*is taken at half the nominal torque_{1,50%} **Alternation**between 50 % and 100 % of nominal torque. The measurement signals*S*and_{i,50%}*S*are taken until 10 measured values each are available for each torque_{i,100%}- The
**equation**below is used to calculate the relative standard deviation (in mathematical terminology, the empirical standard deviation of a random sample) for each torque and relate it to the output signal span:

with *n*=10 being the number of measurements for the respective torque applied (50 % or 100 %) and the arithmetic mean of the measurement signals according to

- The technical data specifies the inferior of the two values σ
and σ_{rel,50%}_{rel,100% }.

HBM specifies the standard deviation of repeatability for its **T10F torque transducer** as *σ _{rel}* ≤ 0.03%. This value refers to the output signal span between the values of applied torque. Assuming a nominal torque of 1 kN·m, for example, this corresponds to a span of 500 N·m according to the test conditions specified above. Thus the standard deviation of repeatability in this case amounts to ≤ 0.15 N·m.

In the following example **repeatability** (quantitatively specified by the standard deviation of repeatability *σ _{rel}*)

The nominal rotation speed is the **upper limit of the speed range** starting from zero. It applies to both clockwise and counterclockwise rotation.

The nominal torque *M _{nom}* is the torque defining the upper limit of the range in which

The maximum service torque is the upper limit of the range in which there is an **unambiguous relation between output signal and torque**. If within this range torque is increased above the nominal torque the limit values declared in the specifications may be exceeded.

If the transducer has been used between nominal torque and maximum service torque, the limit values given in the specifications will be kept by the transducer when it is used again for torque values up to nominal torque. A slight shift of the zero signal may occur, but this is not considered to be a violation of

the specifications.

The torque transducer can be used for measurements up to the **maximum service torque**, though the measurement properties may prove less favorable.

The **limitation on maximum service torque** may be given by **electronic properties** (such as the modulation range of the internal amplifier electronics) or by **mechanical properties** (such as an overload stop). In the case of transducers that have neither internal electronics nor mechanical overload protection, the maximum service torque and the limit torque are frequently identical.

The limit torque is the torque up to which the** transducer’s measuring capability** will not suffer permanent damage.

If the transducer has been used between nominal torque and limit torque, the **limit values** given in the **specifications** will be kept by the transducer when it is used again for torque values up to nominal torque. A slight shift of the zero signal may occur, but this is not considered to be a violation of the specifications.

In the event of a** continuous vibrating load**, the limits discussed below in the section on **permissible oscillation bandwidth** have priority over the limit torque.

The breaking torque is the torque which **when exceeded** may lead to **mechanical destruction** of the transducer.

In the event of** torque values between limit torque and breaking torque no mechanical destruction will occur**, but the transducer may be damaged to such an extent that it will be permanently unusable.

*Fig. 6: Load limits*

The permissible oscillation bandwidth is the** oscillation amplitude** of a **sinusoidally varying torque** with which the transducer can be stressed for 10⋅10^{6} vibration cycles without causing any significant variations in its metrological properties.

The **amplitude** is specified as a **peak-to-peak value**, that is, as the difference between maximum and minimum torque. See also Fig. 7.

As well as the **permissible vibration bandwidth** it is also necessary to define a permissible upper limit for the torque which occurs. This upper limit usually coincides with the nominal torque (in both the positive and negative direction). Values which differ from this are explicitly declared in the specifications.

The concept has been taken from standard **DIN 50100**, which deals with continuous **vibration testing** (**fatigue testing**) within the context of **materials testing**, and has been transferred from mechanical stress to torque.

The deciding factor for **fatigue strength** is the number of **vibration cycles** alone. The frequency is not significant within the frequency range that is relevant to mechanical processes*). According to DIN 50100, it can be assumed to a close approximation for the case of steel materials that a mechanical component is fatigue proof under a given load if it endures the number of 10⋅10^{6} load cycles under the respective load.

The upper limit for torque in the case of **vibrational loading** replaces explicit information about the mean vibrational loading. Within the range defined by the** positive and negative limits**, both **pulsating torque** and **alternating torque** are permissible (see Fig. 7).

*Fig. 7: Terms used in connection with the oscillation bandwidth*

*----------*

**) see also: H.-J. Bargel, G. Schulze: Werkstoffkunde (Materials Science), VDI-Verlag GmbH, Düsseldorf, Germany 1988*

The axial limit force is the **maximum permissible longitudinal force** (or **axial force**), shown as *F _{a}* in Fig. 8. If the axial limit force is exceeded, the ability of the

In **HBM torque transducers** the axial limit force sets an upper limit to the service range. Torque transducers can be used for measurement if the **axial forces** do not exceed the** axial limit force**. However, there may be some effect on the measurement signal. **The upper limit for this influence is separately notified in the specifications**.

The permissible **axial force** gets smaller than the specified **axial limit force** if another irregular stress occurs (such as a bending moment, lateral force or exceeding the nominal torque). Otherwise the limit values have to be reduced. If for example 30 % of both the **bending limit moment** and the **lateral limit force** occur, only 40 % of the axial limit force is allowed in the case that the nominal torque is not exceeded. If parasitic loads occur as continuous vibrating loads, the respective permissible vibration bandwidths may differ from the respective limit loads.

The lateral limit force is the **maximum permissible lateral force** (in the case of radial force), shown as *F _{r}* in Fig. 8. If the lateral limit force is exceeded, the ability of the transducer to measure may be permanently damaged.

In **HBM torque transducers** the lateral limit force sets an **upper limit to the service range**. Torque transducers can be used for measurement if the lateral forces do not exceed the lateral limit force. However, there may be some effect on the measurement signal. The upper limit for this influence is separately notified in the specifications.

The** permissible lateral force** gets smaller than the **specified lateral limit force** if another** irregular stress** occurs (such as an axial force, bending moment or exceeding the nominal torque). Otherwise the limit values have to be reduced. If for example 30 % of both the axial limit force and the bending limit moment occur, only 40 % of the lateral limit force is allowed in the case that the nominal torque is not exceeded. If parasitic loads occur as continuous vibrating loads, the respective permissible vibration bandwidths may differ from the respective limit loads.

The bending limit moment is the **maximum permissible bending moment**, shown as *M _{b}* in Fig. 8. If the bending limit moment is exceeded, the ability of the transducer to measure may be permanently damaged.

In **HBM torque transducers** the **bending limit moment** sets an upper limit to the service range. Torque transducers can be used for measurement if the bending moments do not exceed the bending limit moment. However, there may be some effect on the measurement signal. The upper limit for this influence is separately notified in the specifications.

The** permissible bending moment** gets smaller than the specified bending limit moment if another irregular stress occurs (such as an axial force, lateral force or exceeding the nominal torque). Otherwise the limit values have to be reduced. If for example 30 % of both the axial limit force and the lateral force limit occur, only 40 % of the bending limit moment is allowed in the case that the nominal torque is not exceeded. If parasitic loads occur as continuous vibrating loads, the respective permissible vibration bandwidths may differ from the respective limit loads.

*Fig. 8: Parasitic loads - axial force F _{a}, lateral force F_{r}, bending moment M_{b}*

The reference temperature is the** ambient****temperature at which the transducer specifications apply** as far as there are no temperature ranges specifically defined in which the specifications concerned apply.

The nominal temperature range is the **ambient temperature range** within which the **transducer** can be **operated for all practical purposes** and within which it maintains the **limit values** for the metrological properties declared in the specifications.

The service temperature range is the **ambient temperature range** within which the transducer can be operated** without permanent variations occurring** in its metrological properties.

At temperatures within the service temperature range but outside the nominal temperature range, there is no guarantee that the limit values declared for the metrological properties in the specifications will be maintained.

The storage temperature range is the** ambient temperature range** within which the transducer can be **stored with no mechanical or electrical load** without permanent variations occurring in its metrological properties.

No more result to load