Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

In \(1903,\) Aegidius Elling of Norway designed and built an 11 -hp gas turbine that used steam injection between the combustion chamber and the turbine to cool the combustion gases to a safe temperature for the materials available at the time. Currently there are several gas-turbine power plants that use steam injection to augment power and improve thermal efficiency. For example, the thermal efficiency of the General Electric LM5000 gas turbine is reported to increase from 35.8 percent in simple-cycle operation to 43 percent when steam injection is used. Explain why steam injection increases the power output and the efficiency of gas turbines. Also, explain how you would obtain the steam.

Short Answer

Expert verified
Answer: Steam injection increases the power output and efficiency of gas turbines by increasing the mass flow rate through the turbine, expanding the hot combustion gases, and enhancing kinetic energy recovery. This process also improves the thermal efficiency by reducing the peak combustion temperature and utilizing waste heat from exhaust gases. The steam is typically obtained using a heat recovery steam generator (HRSG), which captures waste heat from the gas turbine's exhaust gases and produces steam for injection.

Step by step solution

01

Understand the basic working principle of gas turbines

Gas turbines convert the chemical energy stored in fuel into mechanical energy by burning the fuel in a continuous flow process. The main components of a gas turbine are the compressor, combustion chamber, and turbine. The compressed air from the compressor mixes with the fuel in the combustion chamber and ignites. The hot combustion gases then expand and drive the turbine, which in turn drives the compressor and generates mechanical power.
02

Explain the effect of steam injection on power output

Steam injection increases the power output of gas turbines by increasing the mass flow rate through the turbine. Injecting steam into the combustion chamber or between the combustion chamber and the turbine expands the hot combustion gases, which increases the total volume and pressure of the gases. This, in turn, increases the work done by the turbine, hence increasing the power output. Moreover, the higher mass flow rate of gases through the turbine also leads to a higher exhaust gas velocity, which enhances the kinetic energy recovery and further boosts the turbine's power output.
03

Explain the effect of steam injection on thermal efficiency

The thermal efficiency of a gas turbine is the ratio of the useful output power to the input heat energy from the fuel. Steam injection improves the thermal efficiency of gas turbines in two main ways. First, it reduces the peak combustion temperature, which reduces the energy lost as heat to the surroundings and allows the use of lower-cost materials. Second, the extra energy added through steam injection comes from the waste heat recovered from the exhaust gases, which would otherwise be lost to the environment. This heat recovery and utilization result in better utilization of the input heat energy, thus improving the overall thermal efficiency of the gas turbine.
04

Explain how to obtain steam

A common method to obtain steam for injection in gas turbines is by using a heat recovery steam generator (HRSG). The HRSG is a heat exchanger that captures the waste heat from the gas turbine's exhaust gases and uses it to produce steam. This steam is then injected into the combustion chamber or turbine, or used to drive a separate steam turbine, in what is known as a combined cycle power plant. This way, the otherwise wasted heat is utilized to produce additional power and improve the overall efficiency of the power generation process.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

An air-standard Stirling cycle operates with a maximum pressure of \(3600 \mathrm{kPa}\) and a minimum pressure of \(50 \mathrm{kPa}\) The maximum volume is 12 times the minimum volume, and the low-temperature reservoir is at \(20^{\circ} \mathrm{C}\). Allowing a \(5^{\circ} \mathrm{C}\) temperature difference between the external reservoirs and the air when appropriate, calculate the specific heat added to the cycle and its net specific work.

An air-standard cycle, called the dual cycle, with constant specific heats is executed in a closed piston-cylinder system and is composed of the following five processes: \(1-2 \quad\) Isentropic compression with a compression ratio \(r=V_{1} / V_{2}\) \(2-3 \quad\) Constant volume heat addition with a pressure ratio, \\[ r_{p}=P_{3} / P_{2} \\] \(3-4 \quad\) Constant pressure heat addition with a volume ratio \\[ r_{c}=V_{4} / V_{3} \\] \(4-5 \quad\) Isentropic expansion while work is done until \(V_{5}=V_{1}\) \(5-1 \quad\) Constant volume heat rejection to the initial state (a) Sketch the \(P\) -V and \(T\) -s diagrams for this cycle. (b) Obtain an expression for the cycle thermal efficiency as a function of \(k, r, r_{c},\) and \(r_{p}\) (c) Evaluate the limit of the efficiency as \(r_{p}\) approaches unity and compare your answer with the expression for the Diesel cycle efficiency. (d) Evaluate the limit of the efficiency as \(r_{c}\) approaches unity and compare your answer with the expression for the Otto cycle efficiency.

A gas-turbine power plant operates on the simple Brayton cycle with air as the working fluid and delivers \(32 \mathrm{MW}\) of power. The minimum and maximum temperatures in the cycle are 310 and \(900 \mathrm{K},\) and the pressure of air at the compressorexit is 8 times the value at the compressor inlet. Assuming an isentropic efficiency of 80 percent for the compressor and 86 percent for the turbine, determine the mass flow rate of air through the cycle. Account for the variation of specific heats with temperature.

A spark-ignition engine has a compression ratio of 8 an isentropic compression efficiency of 85 percent, and an isentropic expansion efficiency of 95 percent. At the beginning of the compression, the air in the cylinder is at 13 psia and \(60^{\circ} \mathrm{F} .\) The maximum gas temperature is found to be \(2300^{\circ} \mathrm{F}\) by measurement. Determine the heat supplied per unit mass, the thermal efficiency, and the mean effective pressure of this engine when modeled with the Otto cycle. Use constant specific heats at room temperature.

For a specified compression ratio, is a diesel or gasoline engine more efficient?

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free