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Explore the Brayton Cycle: Fun Guide for Gas Turbines with Cool Diagrams and Formulas!

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Explore the Brayton Cycle: Fun Guide for Gas Turbines with Cool Diagrams and Formulas!
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Jessa Mae Estoque

@jessamaeestoque_qlas

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The ideal Brayton cycle for gas turbines is a thermodynamic cycle used to model gas turbine engines. This summary provides an overview of the cycle's processes, equations, applications, and efficiency calculations.

• The Brayton cycle consists of four main processes: isentropic compression, constant pressure heat addition, isentropic expansion, and constant pressure heat rejection.

• Key equations cover heat transfer, work done by compressor and turbine, pressure ratio, efficiency, and back work ratio.

• Applications include aviation, power generation, and industrial uses.

• An example problem demonstrates calculations for compressor work, turbine work, cycle efficiency, and back work ratio.

2/23/2023

11

BRAYTON CYCLE. THE IDEAL CYCLE FOR GAS-TURBINE ENGINES We /S=const Qin COMPRESSOR 1. Military aviations. 3. Electric Generation 5. Industria

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Efficiency and Additional Concepts

This page delves deeper into the Brayton cycle efficiency and introduces additional problem-solving techniques.

Efficiency Formula

The thermal efficiency of the Brayton cycle is given by:

η = 1 - T1/T2

Example: This formula shows that efficiency increases as the temperature ratio T1/T2 decreases.

Additional Problem

An example problem is presented to illustrate the application of Brayton cycle principles:

Given:

  • Air enters the compressor at 95 kPa, 22°C
  • Pressure ratio is 6:1
  • Air leaves the heat addition process at 1100K

The problem asks to determine: a. Compressor work and turbine work per unit mass flow b. Cycle efficiency c. Back work ratio

Definition: Back work ratio is the ratio of compressor work to turbine work, indicating the fraction of turbine output used to drive the compressor.

Constant Properties

The problem assumes constant properties, with:

  • Cp = (7/2)R
  • Cv = (5/2)R
  • γ = 1.4

These assumptions simplify calculations while providing a good approximation of cycle performance.

BRAYTON CYCLE. THE IDEAL CYCLE FOR GAS-TURBINE ENGINES We /S=const Qin COMPRESSOR 1. Military aviations. 3. Electric Generation 5. Industria

View

Problem Solution and Calculations

This page provides a detailed solution to the Brayton cycle efficiency calculation problem presented earlier.

Step-by-Step Solution

  1. Calculate T2 using isentropic compression equation: T1P1^((γ-1)/γ) = T2P2^((γ-1)/γ) T2 = 492.4609 K

  2. Calculate T4 using isentropic expansion equation: T3P3^((γ-1)/γ) = T4P4^((γ-1)/γ) T4 = 659.2707 K

  3. Compute compressor work (Wc): Wc = Cp(T2 - T1) = 197.9845 kJ/kg

  4. Compute turbine work (WT): WT = Cp(T3 - T4) = -442.2339 kJ/kg

  5. Calculate cycle efficiency (η): η = 1 - T1/T2 = 0.4007 or 40.07%

  6. Determine back work ratio (bwr): bwr = Wc / (-WT) = 0.4477

Highlight: The negative sign for turbine work indicates energy output from the system.

Key Results

  • Compressor work: 197.9845 kJ/kg
  • Turbine work: -442.2339 kJ/kg
  • Cycle efficiency: 40.07%
  • Back work ratio: 0.4477

Example: This problem demonstrates how to apply the Brayton cycle efficiency formula and related equations to analyze gas turbine performance.

These calculations provide valuable insights into the performance characteristics of an ideal Brayton cycle gas turbine engine, showcasing the relationship between pressure ratio, temperatures, and overall cycle efficiency.

BRAYTON CYCLE. THE IDEAL CYCLE FOR GAS-TURBINE ENGINES We /S=const Qin COMPRESSOR 1. Military aviations. 3. Electric Generation 5. Industria

View

Brayton Cycle: The Ideal Cycle for Gas-Turbine Engines

The Brayton cycle is the ideal thermodynamic cycle for gas turbine engines. This page introduces the cycle's key components, processes, and applications.

Components and Processes

The Brayton cycle consists of four main processes:

  1. Isentropic compression (1-2)
  2. Constant pressure heat addition (2-3)
  3. Isentropic expansion (3-4)
  4. Constant pressure heat rejection (4-1)

These processes occur in the compressor, combustion chamber, and turbine of a gas turbine engine.

Vocabulary: Isentropic - A process where entropy remains constant.

Key Equations

The Brayton cycle analysis involves several important equations:

  1. Heat entering and exiting:

    • Qin = H3 - H2 = Cp(T3 - T2)
    • Qout = H4 - H1 = Cp(T4 - T1)

  2. Work in compression and expansion:

    • Wc = Cp(T2 - T1)
    • WT = Cp(T3 - T4)

  3. Pressure ratio: rp = P2 / P1

Definition: Pressure ratio is the ratio of the compressor outlet pressure to the inlet pressure.

Applications

The Brayton cycle has diverse applications, including:

  1. Military aviation
  2. Commercial aviation
  3. Electric power generation
  4. Transportation (ships, tanks)
  5. Industrial processes

Highlight: The Brayton cycle's versatility makes it crucial in both aerospace and power generation industries.

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Subjects

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Chemistry

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Thermodynamics

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Thermodynamics

Explore the Brayton Cycle: Fun Guide for Gas Turbines with Cool Diagrams and Formulas!

user profile picture

Jessa Mae Estoque

@jessamaeestoque_qlas

·

9 Followers

Follow

The ideal Brayton cycle for gas turbines is a thermodynamic cycle used to model gas turbine engines. This summary provides an overview of the cycle's processes, equations, applications, and efficiency calculations.

• The Brayton cycle consists of four main processes: isentropic compression, constant pressure heat addition, isentropic expansion, and constant pressure heat rejection.

• Key equations cover heat transfer, work done by compressor and turbine, pressure ratio, efficiency, and back work ratio.

• Applications include aviation, power generation, and industrial uses.

• An example problem demonstrates calculations for compressor work, turbine work, cycle efficiency, and back work ratio.

2/23/2023

11

 

Chemistry

1

BRAYTON CYCLE. THE IDEAL CYCLE FOR GAS-TURBINE ENGINES We /S=const Qin COMPRESSOR 1. Military aviations. 3. Electric Generation 5. Industria

Efficiency and Additional Concepts

This page delves deeper into the Brayton cycle efficiency and introduces additional problem-solving techniques.

Efficiency Formula

The thermal efficiency of the Brayton cycle is given by:

η = 1 - T1/T2

Example: This formula shows that efficiency increases as the temperature ratio T1/T2 decreases.

Additional Problem

An example problem is presented to illustrate the application of Brayton cycle principles:

Given:

  • Air enters the compressor at 95 kPa, 22°C
  • Pressure ratio is 6:1
  • Air leaves the heat addition process at 1100K

The problem asks to determine: a. Compressor work and turbine work per unit mass flow b. Cycle efficiency c. Back work ratio

Definition: Back work ratio is the ratio of compressor work to turbine work, indicating the fraction of turbine output used to drive the compressor.

Constant Properties

The problem assumes constant properties, with:

  • Cp = (7/2)R
  • Cv = (5/2)R
  • γ = 1.4

These assumptions simplify calculations while providing a good approximation of cycle performance.

BRAYTON CYCLE. THE IDEAL CYCLE FOR GAS-TURBINE ENGINES We /S=const Qin COMPRESSOR 1. Military aviations. 3. Electric Generation 5. Industria

Problem Solution and Calculations

This page provides a detailed solution to the Brayton cycle efficiency calculation problem presented earlier.

Step-by-Step Solution

  1. Calculate T2 using isentropic compression equation: T1P1^((γ-1)/γ) = T2P2^((γ-1)/γ) T2 = 492.4609 K

  2. Calculate T4 using isentropic expansion equation: T3P3^((γ-1)/γ) = T4P4^((γ-1)/γ) T4 = 659.2707 K

  3. Compute compressor work (Wc): Wc = Cp(T2 - T1) = 197.9845 kJ/kg

  4. Compute turbine work (WT): WT = Cp(T3 - T4) = -442.2339 kJ/kg

  5. Calculate cycle efficiency (η): η = 1 - T1/T2 = 0.4007 or 40.07%

  6. Determine back work ratio (bwr): bwr = Wc / (-WT) = 0.4477

Highlight: The negative sign for turbine work indicates energy output from the system.

Key Results

  • Compressor work: 197.9845 kJ/kg
  • Turbine work: -442.2339 kJ/kg
  • Cycle efficiency: 40.07%
  • Back work ratio: 0.4477

Example: This problem demonstrates how to apply the Brayton cycle efficiency formula and related equations to analyze gas turbine performance.

These calculations provide valuable insights into the performance characteristics of an ideal Brayton cycle gas turbine engine, showcasing the relationship between pressure ratio, temperatures, and overall cycle efficiency.

BRAYTON CYCLE. THE IDEAL CYCLE FOR GAS-TURBINE ENGINES We /S=const Qin COMPRESSOR 1. Military aviations. 3. Electric Generation 5. Industria

Brayton Cycle: The Ideal Cycle for Gas-Turbine Engines

The Brayton cycle is the ideal thermodynamic cycle for gas turbine engines. This page introduces the cycle's key components, processes, and applications.

Components and Processes

The Brayton cycle consists of four main processes:

  1. Isentropic compression (1-2)
  2. Constant pressure heat addition (2-3)
  3. Isentropic expansion (3-4)
  4. Constant pressure heat rejection (4-1)

These processes occur in the compressor, combustion chamber, and turbine of a gas turbine engine.

Vocabulary: Isentropic - A process where entropy remains constant.

Key Equations

The Brayton cycle analysis involves several important equations:

  1. Heat entering and exiting:

    • Qin = H3 - H2 = Cp(T3 - T2)
    • Qout = H4 - H1 = Cp(T4 - T1)

  2. Work in compression and expansion:

    • Wc = Cp(T2 - T1)
    • WT = Cp(T3 - T4)

  3. Pressure ratio: rp = P2 / P1

Definition: Pressure ratio is the ratio of the compressor outlet pressure to the inlet pressure.

Applications

The Brayton cycle has diverse applications, including:

  1. Military aviation
  2. Commercial aviation
  3. Electric power generation
  4. Transportation (ships, tanks)
  5. Industrial processes

Highlight: The Brayton cycle's versatility makes it crucial in both aerospace and power generation industries.

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Knowunity is the # 1 ranked education app in five European countries

Knowunity was a featured story by Apple and has consistently topped the app store charts within the education category in Germany, Italy, Poland, Switzerland and United Kingdom. Join Knowunity today and help millions of students around the world.

Ranked #1 Education App

Download in

Google Play

Download in

App Store

Knowunity is the # 1 ranked education app in five European countries

4.9+

Average App Rating

15 M

Students use Knowunity

#1

In Education App Charts in 12 Countries

950 K+

Students uploaded study notes

Still not sure? Look at what your fellow peers are saying...

iOS User

I love this app so much [...] I recommend Knowunity to everyone!!! I went from a C to an A with it :D

Stefan S, iOS User

The application is very simple and well designed. So far I have found what I was looking for :D

SuSSan, iOS User

Love this App ❤️, I use it basically all the time whenever I'm studying