One of the earliest heating element designs, the enlarged cold ends of the Dumbbell style element were originally made oversized to increase cold end cross section, lowering electrical resistance, thereby lowering cold end operating temperature. Modern Dumbbell Starbars, by contrast, employ an advanced technology to keep the terminal ends cool by virtue of the decreased resistivity of the lower resistance cold end material used in the manufacturing process. Oversize cold ends are therefore no longer necessary. Non-dumbbell (RR Starbars) can be substituted for Dumbbell Starbars. Improvements in the cold-end-to-hot-zone resistance ratio between the original DB and new DB Starbar have been dramatic. The old style resistance ratio was 1:3, whereas the new DB and RR resistance ratio is a minimum of 1:15.
The first several inches of the cold ends are metalized with aluminum to provide a low-resistance contact surface. Electrical connections are made using flat aluminum braids, held in compression to the cold end circumference by stainless steel spring clamps.
DB Starbars are described by giving the overall length, the heating section length, the hot zone outer diameter and the cold end outer diameter.
As an example, DB 22 x 15 x .31/.50 is a Dumbbell Starbar 22 inches long, 15 inch hot zone, .31 hot zone OD and .50 cold end OD. In millimeters the part number would be DB 560 x 380 x 8/14.
For sizes available, please refer to Table B, DB Starbar Dimensions.
With a larger diameter, thinner wall, and clear inner diameter (ID) the TDB are used as tube heaters. An electrically insulative load tube, usually made of mullite, can be used to isolate the product from the TDB Starbar. The surface of Starbars are electrically live. See Table B, for the ID dimensions and recommended load tube diameters.
|Item #||Item Name||Hot Zone Outer Diameter||Cold End Outer Diameter||Maximum Heating Length||Maximum Overall Length|
|DB-0.31-8||Type DB Dumbbell - (Enlarged Cold End) - Silicon Carbide Heating Element||0.31 Inch |
|0.56 Inch |
|DB-0.44-12||Type DB Dumbbell - (Enlarged Cold End) - Silicon Carbide Heating Element||0.44 Inch |
|0.75 Inch |
|DB-0.56-14||Type DB Dumbbell - (Enlarged Cold End) - Silicon Carbide Heating Element||0.56 Inch |
|0.88 Inch |
|DB-0.75-18||Type DB Dumbbell - (Enlarged Cold End) - Silicon Carbide Heating Element||0.75 Inch |
|1.10 Inch |
|DB-1.00-25||Type DB Dumbbell - (Enlarged Cold End) - Silicon Carbide Heating Element||1.00 Inch |
|DB-1.18-30||Type DB Dumbbell - (Enlarged Cold End) - Silicon Carbide Heating Element||1.18 Inch |
walls or in ceramic lead-in sleeves, if used, must be large enough to ensure no physical binding of the Starbars. The alignment of the support holes through refractory walls should also guarantee that no physical binding occurs.
If ceramic fiber bulk is used to help reduce radiant energy losses around the Starbars, it must be tucked gently around the diameter of the cold end for a distance of only 12 mm (1/2 inch). The ceramic fiber should never be packed so tightly that it restricts the thermal expansion differences between the Starbar and furnace components. Aluminum braid should be kept slack so that there is no physical stress being applied to the Starbars.
Recommended Minimum Refractory Hole Size
Minimum Hole Diameter Based on Refraactory Wall Thickness
DB Starbars can operate to furnace temperatures up to 2730ºF (1500ºC). If the furnace temperature is to be 2600ºF (1425ºC) or above, the terminal end or cold end should be well protected within the refractory wall of the furnace. The hot zone material is rated to furnace temperatures up to 3100ºF (1700ºC).
The maximum operating temperature should be reduced for non-air applications with the exception of argon and helium that can be used without any reduction. Reducing atmospheres, such as hydrogen or disassociated ammonia, particularly with low dew-points, may remove the protective silicon oxide protection that forms on silicon carbide. In such atmospheres, temperature reductions are required as shown in Figure 1.
The maximum furnace temperature for a nitrogen atmosphere is 2500ºF (1370ºC) with a watt loading of 20 w/in2 to 30 w/in2 (3.1 w/cm2 to 4.6 w/cm2) maximum watt surface watt loading. Too high a surface temperature will result in formation of silicon nitride causing a thermally insulative layer to form around the Starbar resulting in over-temperature damage.
The silicon carbide Starbar is a linear type resistance heater that converts electrical energy to heat energy – Joule’s Law W = I2 x R, (W = power in watts, I = current in amperes, R = resistance on ohms).
DB STARBAR has a negative
Starbars are not sized to a specific wattage output like metallic heating elements. The amount of energy that a Starbar is capable of converting from electrical to heat energy depends on the ambient furnace temperature and atmosphere in which the Starbar
Ease of Replacement
Starbars increase gradually in resistance with use. This characteristic of increasing in resistance is called aging. Aging is a function of the following:
- Operating temperature
- Electrical loading – usually expressed in watts per square inch or watts per square centimeter of Starbar radiating surface
- Type of operation (continuous or intermittent)
- Operating and maintenance techniques
Specifications and Matching
furnace Heating Chamber
DB Starbar Spacing
Z = S ÷ 1.73 minimum for moving loads
S = 2 x Starbar hot zone diameter minimum
X – distance from the centerline of Starbar to any reflecting surface, such as a refractory wall or product
Z – distance from the centerline of the Starbar to a moving or stationary load
S – distance from centerline of the Starbar to the centerline of an adjacent Starbar