Custom Search

Friday, August 3, 2012

Resistance temperature detectors : Basics

The principle of resistance temperature detectors (RTD) is based on the variation of electrical resistance of metals with temperature. For this purpose several metals are used, namely, platinum, copper, nickel. When temperature increases the resistance of these metals increases. Temperature function of resistance for metals in a narrow temperature interval can be expressed by a relationship:


Rϑ and R0        - are the values of electrical resistance of a metal conductor at temperatures ϑ and 0,̊C, respectively, Ohm;
α                      - thermal coefficient of electrical resistance, 1/̊C .

For metals this coefficient is positive. Fig.1 shows relationship between resistance of platinum and copper RTD and temperature.

Platinum RTDs are used for temperature measurements from -220 to 850 oC (they are used as reference RTDs, as well), copper RTD - from -50 to 150 oC, and Nickel RTD - from -215 to 320 oC.

Figure 1: Resistance vs temperature for platinum and copper RTD.

Fig. 2 shows the assembly of RTDs. Sensitive elements of RTDs are made of a thin wire 1 with outside diameter equal to 0.025 mm (platinum RTD) and 0.1 mm (copper RTD) double wounded (non-inductive) on a micaceous or porcelain stem 2. For mechanical strength the sensitive element is placed in the ceramic insulator tube 3 filled by extremely fine granular powder; extension wires are placed in the ceramic insulator 4, and entire assembly is covered by a protective sheath of stainless steel 5. The space between the sheath and ceramic insulator is filled by ceramic packing powder 6. To avoid contact of sensitive element with environment, sensitive assembly is protected by high-temperature hermetic seal 7. The contact between the wire of the sensitive element and the ceramic encapsulation permits a rapid speed of response.

Figure 2: RTD assembly.

For measurements of resistance of RTDs several methods are used. Among them the most widely used is a method employing a Wheatstone bridge (Figure 3). In this case RTD is connected to the bridge by two connecting cables (conductors). The bridge is powered by direct current power supply in the points "a" and "b". RTD is immersed in the media, which temperature to be measured. When this bridge is in balance, then there is no voltage between points "c" and "d", and zero-indicator (ZI) shows no current. For this condition we can write the following equation:


R1 and R2                    - electrical resistance of two invariable resistors, usually, R1=R2, Ohm;
Rϑ                                - electrical resistance of RTD, Ohm;
Rc                                - electrical resistance of a connecting cable, Ohm;
Rsr                                - electrical resistance of a slide (variable) resistor, Ohm.

Figure 3.: Two-conductor connecting.   Figure 4: Three-conductor connecting.

As follows from these equations, the certain position of a slide of the variable resistor (ie, certain value of Rsr) corresponds to each value of a measuring temperature (ie, for each value of Rϑ) at any balance condition of the bridge. Therefore, the scale of the bridge may be calibrated in degrees Celsius.

For a two-conductor connecting scheme (see Fig.3), variation of an ambient temperature will effect values of an electrical resistance of connecting cables Rcand, therefore, the results of measurements will be erroneous.

With all resistance temperature detectors a three-conductor connection scheme is recommended (see Fig. 4). One conductor is common to both sides of the bridge, while other two connect the RTD to each side of the bridge. Any change in the cable temperature (as the result of variations in ambient temperature) will be cancelled because the resistance of both sides of the bridge change by the same value (providing three connecting cables are at the same temperature).
A four-conductor connection scheme is used when very accurate measurements of temperature are required, up to ±0.01 °C of accuracy.

 Derivation of a balanced condition for a Wheatstone Bridge

Below I give you the derivation of the balanced condition for a Wheatstone bridge. Figure 4a shows a circuit of five electrical resistors connected to form the Wheatstone bridge.

Figure 4a.: Wheatstone bridge.

Here we use two Kirchoff’s Laws. The first Kirchoff’s law says: the total current flowing into any junction is equal to the total current flowing out of this junction. The second Kirchoff’s law states: the total change in potential around any closed circuit loop is equal to zero.

For the second Kirchoff’s law we should be sure to include the sign of potential energy correctly: the potential decreases around a resistor in the direction of current flow and increases in the direction opposite to current flow; potential increases from negative to positive terminals of the battery.

Below I give you two different methods for the derivation of the balanced condition for a Wheatstone bridge.

Now, let’s consider several closed circuit loops and apply the above law to them.

a. First method

1. Loop            e-a-b-c-f-e :

2. Loop            a-b-g-d-a :

3. Loop            b-c-d-g-b :

Here, U is a dc voltage, and U≠ 0.

So, we have three equations with 3 unknowns - I1; I3 and I5.


Now we combine terms with I1; I3 and I5.




Now we evaluate the determinant of the matrix developed using this set of equations:


In the case of the Wheatstone bridge the resistance R5 is substituted by an ampmeter. Ampmeters have a negligibly small resistance, so we can write that R5 = 0. With this condition we can re-write (13) as follows:


Because all Ri > 0 we have that ∆ > 0 and ∆ ≠ 0.

For current I5 we have:

Now we can evaluate the value of the current, which flows through an ammeter as follows:

We know that a balanced condition is when current I5 = 0, and because ∆ > 0, and ∆ ≠ 0 and U ≠ 0, we can give an expression for the balanced condition for the Wheatstone bridge as follows:


or, finally,


b. Second method

When the bridge is balanced, ie I5 = 0, and current

1. Loop            e-a-b-c-f-e :



2. Loop            e-a-d-c-f-e :


Assume point f is at earth potential, then potential at point  e is equal to Ua = U. Potential at point b is equal to


Potential at point d is equal to


Potential difference between points b and d is equal to


Using equations (20) and (22) we can get:



Substitute equations (26) and (27) into equation (25):






Since R3 ≠ 0  and R1 ≠ 0, then


We know for balanced condition I5 = 0, then voltage Ubd = 0. Because U ≠ 0, then




So, finally, we get


Article Source:: Dr. Alexander Badalyan, University of South Australia


Basics of Instrumentation & Control

To view more posts on BASICS : CLICK HERE


To view more posts on PRESSURE : CLICK HERE


To view more posts on FLOW : CLICK HERE


To view more posts on LEVEL : CLICK HERE


To view more posts on TEMPERATURE : CLICK HERE

Analytical Instrumentation

To view more posts on Analytical Instrumentation : CLICK HERE
Related Posts Plugin for WordPress, Blogger...

About This Blog

Hai friends…welcome to my blog. This blog is exclusively for instrumentation engineering students which will provide sources for their reference and studies. As you all know Instrumentation is now a fast emerging and developing field in Engineering. This blog has different categories like PLC, SCADA, DCS, Sensors and Transducers, Computer control of process, Industrial Instrumentation, etc.

This blog will also provide an exclusive ‘ASK ME’ section where you can make any queries and share your ideas about instrumentation. The solution for your queries will be given to you by mail from best of my knowledge and reference.

So I wish this blog may be very useful for your studies and reference.

About Me

Keep In Touch

Follow Me!

Online Queries

Popular Posts