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Consider the ideal Diesel, Ericsson, and Carnot cycles operating between the same temperature limits. How would you compare the thermal efficiencies of these three cycles?

Short Answer

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Question: Rank the thermal efficiencies of the Diesel cycle, Ericsson cycle, and Carnot cycle operating between the same temperature limits. Answer: The order of thermal efficiencies, under ideal conditions, is Carnot cycle > Ericsson cycle > Diesel cycle. However, the exact ordering may change depending on specific conditions, and the Carnot cycle, despite being the most efficient, cannot be achieved in real life due to practical constraints.

Step by step solution

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1. Diesel Cycle

The Diesel cycle is an internal combustion process used in Diesel engines. It consists of four processes: adiabatic compression (isentropic), constant-pressure heat addition, adiabatic expansion (isentropic), and constant-volume heat rejection. The cycle has two isentropic processes and two isobaric processes, which makes its efficiency formula: Efficiency (η_Diesel) = 1 - [ (V3/V2)^(γ-1) ] where V2 and V3 are the volumes of the working fluid at different points in the cycle, and γ is the ratio of specific heats.
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2. Ericsson Cycle

The Ericsson cycle is an external combustion process. It consists of two main processes: isothermal compression and expansion, which are accompanied by constant-pressure heat addition and rejection. The efficiency for an Ericsson cycle is: Efficiency (η_Ericsson) = 1 - (T1 / T2) where T1 and T2 are the temperature limits of the cycle.
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3. Carnot Cycle

The Carnot cycle is a hypothetical cycle composed of two adiabatic and two isothermal processes, which are reversible in nature. The efficiency of a Carnot cycle is considered as the benchmark for any heat engine cycle. It is given by: Efficiency (η_Carnot) = 1 - (T_cold / T_hot) where T_cold and T_hot are the temperature limits of the cycle.
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4. Comparison of Thermal Efficiencies

Since all three cycles operate between the same temperature limits, we can compare their thermal efficiencies as: 1. η_Diesel: Depends on the volume ratios V3/V2 and the ratio of specific heats γ, which can make this cycle less efficient than Carnot and Ericsson cycles depending on these factors. 2. η_Ericsson: Formula is similar to η_Carnot, as both depend on the temperature limits. However, the Ericsson cycle would have practical limitations such as difficulty in maintaining isothermal conditions while transferring heat, which might make it less efficient than the Carnot cycle in real situations. 3. η_Carnot: The Carnot cycle is considered as the most efficient heat engine cycle between two given temperature limits because of its reversible nature. However, it is an ideal cycle that cannot be achieved in reality due to practical constraints. In conclusion, the efficiencies can be compared in the following order: Carnot cycle > Ericsson cycle > Diesel cycle (although the exact ordering may change depending on specific conditions). The Carnot cycle sets the upper limit for the efficiency of a heat engine operating between the given temperature limits, but it is not achievable in real life.

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Key Concepts

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

Diesel Cycle
The Diesel cycle is integral to the function of Diesel engines, known for their efficiency and power. The cycle comprises four distinct parts: starting with a piston compressing air (adiabatic compression), followed by fuel injection and constant-pressure heat addition as the fuel burns. Then, the gasses expand without heat exchange (adiabatic expansion), and finally, the cycle ends with constant-volume heat rejection.

The interplay between volume changes, particularly the initial and final volumes of air in the cylinder, denoted by V2 and V3, affects the cycle's efficiency. The specific heats ratio, γ, also plays a pivotal role. A higher compression ratio (V2/V3) typically results in greater efficiency, allowing the Diesel cycle to perform well, especially for heavy-duty applications.
Ericsson Cycle
Revolving around external combustion, the Ericsson cycle is characterized by its two isothermal processes – compression and expansion – which occur alongside constant-pressure heat exchange.

Notably, the cycle aims for efficiency that mirrors the esteemed Carnot cycle, leveraging constant temperature processes that theoretically could yield high efficiencies. However, ensuring truly isothermal conditions is a daunting task, hindered by the sluggish heat transfer in live applications, thus curtailing the Ericsson cycle's practical efficiency.
Carnot Cycle
The Carnot cycle is a paragon of thermodynamic processes, composed of two isentropic and two isothermal transitions, revered for its theoretical maximal efficiency. Its conceptual elegance poses as a benchmark, as no real engine can surpass the Carnot cycle's efficiency framed by a given temperature range.

The cycle's efficiency hinges solely on the high and low temperature limits, T_hot and T_cold, underscoring the importance of temperature gradients in heat engines. Nevertheless, the Carnot cycle's practical application remains unattainable due to insurmountable real-world hurdles such as friction and non-instantaneous heat transfer.
Heat Engine Cycles
Heat engine cycles like the Diesel, Ericsson, and Carnot cycles transform thermal energy into mechanical work using a working fluid or gas. These cycles showcase the core principles of thermodynamics through a series of processes, including compression, heat addition, expansion, and heat rejection.

Each cycle's nuances profoundly impact their efficiency and suitability for different applications. Be it internal combustion for robust power delivery or idealized models aiming for maximal efficiency, these cycles embody the intricate dance of energy conversion.
Isentropic Processes
An isentropic process is a reversible adiabatic transformation, meaning it involves no heat transfer with the surroundings, and thus entropy remains constant. Found in idealized engines, these processes represent the compression and expansion phases where the efficiency of energy usage is maximized.

Both the Diesel and Carnot cycles include isentropic steps, exemplifying how these cycles utilize the inherent energy in the working fluid, providing insight into the thermodynamic ideals that guide engine design.
Isothermal Processes
Isothermal processes unfold at a constant temperature, distinguishing themselves as crucial components in cycles like Ericsson and Carnot. Through slow, controlled heat exchange, these processes theoretically manage to fully utilize the heat energy provided to or removed from the system.

The realization of isothermal conditions in a physical engine presents numerous technical obstacles, reflecting the disparity between thermodynamic theory and engineering practicality.
Thermodynamic Cycles Efficiency
The efficiency of thermodynamic cycles is a measure of how effectively a cycle converts heat into work, encapsulating the essence of engine performance. Real-world engines differ significantly in their adherence to ideal conditions, reflecting the importance of understanding these thermodynamic principles.

The comparison between the theoretical efficiencies of Diesel, Ericsson, and Carnot cycles unveils the intrinsic constraints of thermal systems and challenges in achieving maximal efficiency. This theoretical hierarchy helps in contextualizing the performance of actual engines and underscores the role of temperature, volume ratios, and heat capacities in determining a cycle's practical efficacy.

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Most popular questions from this chapter

A gas turbine for an automobile is designed with a regenerator. Air enters the compressor of this engine at \(100 \mathrm{kPa}\) and \(30^{\circ} \mathrm{C}\). The compressor pressure ratio is \(10 ;\) the maximum cycle temperature is \(800^{\circ} \mathrm{C} ;\) and the cold air stream leaves the regenerator \(10^{\circ} \mathrm{C}\) cooler than the hot air stream at the inlet of the regenerator. Assuming both the compressor and the turbine to be isentropic, determine the rates of heat addition and rejection for this cycle when it produces 115 kW. Use constant specific heats at room temperature.

Helium is used as the working fluid in a Brayton cycle with regeneration. The pressure ratio of the cycle is 8 the compressor inlet temperature is \(300 \mathrm{K},\) and the turbine inlet temperature is \(1800 \mathrm{K}\). The effectiveness of the regenerator is 75 percent. Determine the thermal efficiency and the required mass flow rate of helium for a net power output of \(60 \mathrm{MW},\) assuming both the compressor and the turbine have an isentropic efficiency of \((a) 100\) percent and \((b) 80\) percent.

An ideal Stirling cycle filled with air uses a \(75^{\circ} \mathrm{F}\) energy reservoir as a sink. The engine is designed so that the maximum air volume is \(0.5 \mathrm{ft}^{3},\) the minimum air volume is \(0.06 \mathrm{ft}^{3},\) and the minimum pressure is 15 psia. It is to be operated such that the engine produces 2 Btu of net work when 5 Btu of heat are transferred externally to the engine. Determine the temperature of the energy source, the amount of air contained in the engine, and the maximum air pressure during the cycle.

A gas-turbine plant operates on the regenerative Brayton cycle with two stages of reheating and two-stages of intercooling between the pressure limits of 100 and 1200 kPa. The working fluid is air. The air enters the first and the second stages of the compressor at \(300 \mathrm{K}\) and \(350 \mathrm{K},\) respectively, and the first and the second stages of the turbine at \(1400 \mathrm{K}\) and \(1300 \mathrm{K},\) respectively. Assuming both the compressor and the turbine have an isentropic efficiency of 80 percent and the regenerator has an effectiveness of 75 percent and using variable specific heats, determine ( \(a\) ) the back work ratio and the net work output, \((b)\) the thermal efficiency, and \((c)\) the secondlaw efficiency of the cycle. Also determine ( \(d\) ) the exergies at the exits of the combustion chamber (state 6 ) and the regenerator (state 10 ) (See Fig. \(9-43\) in the text).

An ideal Ericsson engine using helium as the working fluid operates between temperature limits of 550 and \(3000 \mathrm{R}\) and pressure limits of 25 and 200 psia. Assuming a mass flow rate of \(14 \mathrm{lbm} / \mathrm{s}\), determine (a) the thermal efficiency of the cycle, \((b)\) the heat transfer rate in the regenerator, and \((c)\) the power delivered.

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