/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 61 A gas turbine rotor has 54 AISI ... [FREE SOLUTION] | 91Ó°ÊÓ

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A gas turbine rotor has 54 AISI 302 stainless steel blades of dimensions \(L=6 \mathrm{~cm}\), \(A_{c}=4 \times 10^{-4} \mathrm{~m}^{2}\), and \(\mathscr{P}=0.1 \mathrm{~m}\). When the gas stream is at \(900^{\circ} \mathrm{C}\), the temperature at the root of the blades is measured to be \(500^{\circ} \mathrm{C}\). If the convective heat transfer coefficient is estimated to be \(440 \mathrm{~W} / \mathrm{m}^{2} \mathrm{~K}\), calculate the heat load on the rotor internal cooling system.

Short Answer

Expert verified
The heat load on the rotor internal cooling system is 5.7024 kW.

Step by step solution

01

Understand the Problem and Given Data

We are given data about a gas turbine rotor with 54 blades made of AISI 302 stainless steel. The blade dimensions are length \(L = 6 \text{ cm}\), cross-sectional area \(A_c = 4 \times 10^{-4} \text{ m}^2\), and perimeter \(\mathscr{P} = 0.1 \text{ m}\). We are told the temperatures: the gas stream at \(900^{\circ} \text{C}\) and the blade root at \(500^{\circ} \text{C}\). The convective heat transfer coefficient \(h\) is \(440 \text{ W/m}^2 \text{ K}\). We need to find the heat load on the rotor internal cooling system.
02

Identify the Heat Transfer Equation

The heat transfer along the length of the blades is by conduction and convection. The heat load can be found using the equation:\[Q = L \cdot q',\]where \(q'\) is the rate of heat transfer per unit length, given by the convective transfer across the surface of the blade:\[q' = h \cdot \mathscr{P} \cdot (T_s - T_{\infty}).\]Here \(T_s = 500^{\circ} \text{C}\) and \(T_{\infty} = 900^{\circ} \text{C}\), so the heat load \(Q\) on one blade will be required next.
03

Calculate the Heat Transfer Rate (q')

Using the given temperatures and heat transfer coefficient:\[q' = 440 \text{ W/m}^2 \text{ K} \times 0.1 \text{ m} \times (500 - 900) \text{ K}.\]Calculate:\[q' = 440 \times 0.1 \times (-400) = -1760 \text{ W/m}.\]
04

Calculate Heat Load on One Blade (Q)

Use the heat transfer rate per unit length to determine the heat load on one blade:\[Q = L \times q' = 0.06 \text{ m} \times (-1760 \text{ W/m}).\]Calculate:\[Q = -105.6 \text{ W}.\]Note that the negative sign indicates the direction of heat flow, but for heat load magnitude, we consider the absolute value.
05

Calculate Total Heat Load on All Blades

Multiply the heat load on one blade by the number of blades to get the total heat load on the rotor:\[Q_{\text{total}} = 54 \times 105.6 \text{ W}.\]Calculate:\[Q_{\text{total}} = 5702.4 \text{ W} = 5.7024 \text{ kW}.\]

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Understanding Gas Turbines
Gas turbines are powerful engines that are used in a wide variety of applications. They convert natural gas or other fuels into mechanical energy. This mechanical energy is then used to produce electricity, run jet engines, or even drive industrial machines. This process occurs in three main steps:
  • Compression of incoming air
  • Mixing of air with fuel and ignition, which produces high-temperature, high-pressure exhaust gases
  • Expansion of these gases through a turbine, which spins and creates mechanical power
At the core of this machine is the rotor, which spins and generates the majority of the power. The blades attached to the rotor are critical because they interact directly with the reacting gases to convert thermal energy to mechanical energy.
To endure the intense environment inside a gas turbine, these blades are often made of materials capable of withstanding high temperatures and significant mechanical stress, such as AISI 302 stainless steel.
Understanding Convective Heat Transfer Coefficient
The convective heat transfer coefficient, often represented by the symbol \(h\), is a measure of the heat transfer rate between a solid and a fluid in motion across its surface. It is expressed in the units \(\text{W/m}^2 \text{K}\).
This coefficient is critical in calculations involving heat transfer, such as when determining how effectively a gas turbine blade dissipates heat. For gas turbine applications, the convective heat transfer coefficient can be affected by factors like:
  • The speed of the gas flowing over the blades
  • The surface roughness of the blades
  • The temperature difference between the blade surface and the gas
In the example exercise, a coefficient of \(440 \text{ W/m}^2 \text{K}\) means that every square meter of the blade can transfer 440 watts of heat per degree Kelvin (or Celsius) difference between the blade surface and the gas. The larger the value, the more effective the blade is at transferring heat away from itself through convection.
Why AISI 302 Stainless Steel?
AISI 302 stainless steel is a type of high-strength material used in demanding environments, such as in the construction of gas turbine blades. It has several attractive properties that make it suitable for this purpose:
  • **Corrosion Resistance**: Being a stainless steel, AISI 302 offers excellent resistance to corrosion which is essential in the high-temperature, oxidizing environments of a gas turbine.
  • **High Strength**: This material can withstand significant mechanical stress, which is crucial since rotor blades experience high centrifugal forces.
  • **Good Thermal Conductivity**: Although metals generally conduct heat well, AISI 302 has a suitable balance of thermal properties that allow for efficient heat dissipation via conduction and convection.
The choice of material is pivotal as it directly impacts the durability and efficiency of the turbine's performance.
Cooling Systems in Gas Turbines
Cooling systems are crucial for maintaining the efficiency and longevity of gas turbines. During operation, the turbine blades encounter very high temperatures due to the combustion process. These systems work to manage heat effectively, preventing damage and maintaining optimal performance.
The cooling of turbine blades generally involves a few key strategies:
  • **Air Cooling**: The simplest form involves directing a flow of air to contact the blades, thereby reducing the blade temperature via convective heat transfer.
  • **Advanced Techniques**: In more sophisticated systems, air from the compressor section of the turbine is bled off and used to cool the blade from the inside. This technique enhances the cooling efficiency and allows the turbine to operate at higher temperatures.
  • **Material Choice**: As discussed earlier, using materials like AISI 302 stainless steel helps in managing the thermal loads and extending the blade life.
Efficient cooling is essential to mitigate thermal fatigue, reduce wear, and prevent failures, thereby ensuring the gas turbine operates reliably and efficiently.

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Most popular questions from this chapter

An electrical current is passed through a \(1 \mathrm{~mm}\)-diameter, \(20 \mathrm{~cm}\)-long copper wire located in an air flow at \(290 \mathrm{~K}\). If the ends of the wire are maintained at \(300 \mathrm{~K}\), determine the maximum current that can be passed if the midpoint temperature is not to exceed \(400 \mathrm{~K}\). The convective heat transfer coefficient is estimated to be 20 \(\mathrm{W} / \mathrm{m}^{2} \mathrm{~K}\). For the copper wire, take \(k=386 \mathrm{~W} / \mathrm{m} \mathrm{K}, \varepsilon=0.8\). and an electrical resistance of \(2.2 \times 10^{-2} \Omega / \mathrm{m}\).

Two air flows are separated by a \(2 \mathrm{~mm}\)-thick plastic wall. A \(20.2 \mathrm{~cm}\)-long, \(2 \mathrm{~cm}\)-diameter aluminum rod transfers heat from one flow to the other as shown. The hot air flow is at \(70^{\circ} \mathrm{C}\), and the convective heat transfer coefficient to the rod is \(48 \mathrm{~W} / \mathrm{m}^{2} \mathrm{~K}\); the cold air flow is at \(20^{\circ} \mathrm{C}\) and is at a lower velocity, giving a heat transfer coefficient of only \(24 \mathrm{~W} / \mathrm{m}^{2} \mathrm{~K}\). Determine the rate of heat transfer and the temperature of the midsection of the rod. Take \(k=190 \mathrm{~W} / \mathrm{m} \mathrm{K}\) for the aluminum.

A steel heat exchanger tube of \(2 \mathrm{~cm}\) outer diameter is fitted with a steel spiral annular fin of \(4 \mathrm{~cm}\) outer diameter, thickness \(0.4 \mathrm{~mm}\), and wound at a pitch of 3 \(\mathrm{mm}\). If the outside heat transfer coefficient is \(20 \mathrm{~W} / \mathrm{m}^{2} \mathrm{~K}\) on the original bare tube and \(15 \mathrm{~W} / \mathrm{m}^{2} \mathrm{~K}\) on the finned tube, determine the reduction in the outside thermal resistance achieved by adding the fins. Take \(k_{\text {steel }}=42 \mathrm{~W} / \mathrm{m} \mathrm{K}\).

Heat is generated uniformly in a \(8 \mathrm{~cm}\)-thick slab at a rate of \(450 \mathrm{~kW} / \mathrm{m}^{3} .\) One face of the slab is insulated and the other is cooled by water at \(20^{\circ} \mathrm{C}\), giving a heat transfer coefficient of \(800 \mathrm{~W} / \mathrm{m}^{2} \mathrm{~K}\). If the conductivity of the slab is \(12.0 \mathrm{~W} / \mathrm{m} \mathrm{K}\), determine the maximum temperature in the slab.

A heat sink assembly capable of mounting 36 power transistors may be idealized as a \(15 \mathrm{~cm}\) cube containing four rows of 24 aluminum fins per row, each fin being \(15 \mathrm{~cm}\) wide, \(2.5 \mathrm{~cm}\) high, and \(2 \mathrm{~mm}\) thick. A fan is an integral part of the assembly and blows air at a velocity that gives a heat transfer coefficient of \(50 \mathrm{~W} / \mathrm{m}^{2} \mathrm{~K} .\) If the manufacturer's transistor temperature limit is \(360 \mathrm{~K}\), specify the allowable power dissipation per transistor. The mean air temperature is \(310 \mathrm{~K}\). If the rise in air temperature is limited to \(10 \mathrm{~K}\), specify the required capacity of the fan in \(\mathrm{m}^{3} / \mathrm{min}\).

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