Brayton Cycle Thermodynamic Analysis

In summary, the conversation discussed a problem in thermodynamics involving a gas turbine operating under a modified brayton cycle. The individual sought help with checking their equations, procedures, and results. The conversation included a review of the attempted solutions and a discussion of suggestions for improvement, including double checking equations and including more details and assumptions for the maximum power calculation.
  • #1
Salagon
1
0
Hi! I'd appreciate some help solving the thermodynamic's problem. I am sorry if the problem statement isn't 100% clear, as I've translated it from my native language.

I'd really like if you could help me check my equations/procedure/results.

In the following link both my attempted solutions and problem diagram can be found.
https://drive.google.com/folderview...VLdjRzV19saUtZTHhlSlk5OTFINEEwa3M&usp=sharing

1. Homework Statement

A gas turbine operating under a modified brayton cycle.
Air is compressed at a ratio of 9.
Air enters the compressor at 273K and 100kPa.
The cycle's maximun temperature is 1600K.
Assume that the turbines and compressor operate adiabaticaly and reversibly.
The first turbine is used to power the compressor.
air mass flow is 100kg/s

Homework Equations


Determine temperature and pressure at state 4
determine net power
determine maximum power by exergy analysis

The Attempt at a Solution


I've solved the problem using both ideal and real methods. I'm concerned that while some of the data between the two is very similar (work from compressor and HP turbine), other stuff is quite different (heat lost and introduced, max power)Thanks!
 
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  • #2


Hello!

I would be happy to assist you with your thermodynamics problem. I have reviewed your attempted solutions and problem diagram and I have a few suggestions for you.

First, for the ideal method, it looks like you have correctly calculated the temperatures and pressures at states 2, 3, and 4. However, for the real method, it seems like you have used the same equations for both the compressor and turbine, which may not be accurate. I recommend double checking your equations and making sure you are using the correct ones for each component.

Additionally, for the net power calculation, it looks like you have correctly calculated the work done by the compressor and the turbines. However, you also need to take into account the work done by the first turbine on the compressor. This will affect the overall net power output.

Lastly, for the maximum power calculation using exergy analysis, it would be helpful to see your calculations and assumptions. This will allow me to better understand the differences between the ideal and real methods.

Overall, your approach and equations seem reasonable. I would recommend double checking your equations and making sure you are using the correct ones for each component. Also, including more details and assumptions for the maximum power calculation would be helpful in understanding the differences between the two methods.

I hope this helps and please let me know if you have any other questions or concerns. Good luck with your problem!
 

What is the Brayton Cycle?

The Brayton Cycle is a thermodynamic cycle that describes the operation of a gas turbine engine. It is used to convert the energy from a fuel into mechanical work, which can then be used to power various machines.

How does the Brayton Cycle work?

The Brayton Cycle consists of four main processes: compression, combustion, expansion, and exhaust. In the compression process, air is compressed and heated. Then, fuel is injected and combusted, releasing energy. The expanding hot gases then pass through a turbine, producing mechanical work. Finally, the exhaust gases are released into the atmosphere.

What is the purpose of a thermodynamic analysis of the Brayton Cycle?

A thermodynamic analysis of the Brayton Cycle allows engineers to understand the efficiency and performance of the gas turbine engine. It helps identify areas for improvement and optimization, leading to more efficient and reliable engines.

What factors affect the thermodynamic efficiency of the Brayton Cycle?

The thermodynamic efficiency of the Brayton Cycle is affected by several factors, including the compression ratio, turbine inlet temperature, and pressure losses in the compressor and turbine. These factors can be optimized to improve the overall efficiency of the engine.

What are some real-world applications of the Brayton Cycle?

The Brayton Cycle is used in a variety of applications, including aircraft engines, power generation plants, and marine propulsion systems. It is also used in industrial processes, such as natural gas compression and refrigeration systems.

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