An ideal Brighton cycle has a pressure ratio of 15. The inlet air to the compressor is assumed to have a pressure of 100 kPa and a temperature of 340, and in a turbine inlet with a temperature of 1300. Assuming specific heat variables (using the relationships of relative pressure, relative volume and standard air table) for air, Use a heat recovery regenerator with 72% efficiency. It is desirable: • Temperature unit K • Compressors and turbines are isentropic. That is, they have 100% thermal efficiency. A) Draw approximate diagrams of T-s and P-v, calculate the pressure and temperature of the four points of the cycle B) Net output work C) Cycle after cycle ratio D) Thermal efficiency of the cycle

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
icon
Related questions
Question

S4

An ideal Brighton cycle has a pressure ratio of 15. The inlet air to the compressor is
assumed to have a pressure of 100 kPa and a temperature of 340, and in a turbine
inlet with a temperature of 1300. Assuming specific heat variables (using the
relationships of relative pressure, relative volume and standard air table) for
air, Use a heat recovery regenerator with 72% efficiency. It is desirable:
• Temperature unit K
• Compressors and turbines are isentropic. That is, they have 100% thermal
efficiency.
A) Draw approximate diagrams of T-s and P-v, calculate the pressure and
temperature of the four points of the cycle
B) Net output work
C) Cycle after cycle ratio
D) Thermal efficiency of the cycle
Transcribed Image Text:An ideal Brighton cycle has a pressure ratio of 15. The inlet air to the compressor is assumed to have a pressure of 100 kPa and a temperature of 340, and in a turbine inlet with a temperature of 1300. Assuming specific heat variables (using the relationships of relative pressure, relative volume and standard air table) for air, Use a heat recovery regenerator with 72% efficiency. It is desirable: • Temperature unit K • Compressors and turbines are isentropic. That is, they have 100% thermal efficiency. A) Draw approximate diagrams of T-s and P-v, calculate the pressure and temperature of the four points of the cycle B) Net output work C) Cycle after cycle ratio D) Thermal efficiency of the cycle
Expert Solution
steps

Step by step

Solved in 2 steps with 3 images

Blurred answer
Knowledge Booster
Stress Transformation
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Recommended textbooks for you
Elements Of Electromagnetics
Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Control Systems Engineering
Control Systems Engineering
Mechanical Engineering
ISBN:
9781118170519
Author:
Norman S. Nise
Publisher:
WILEY
Mechanics of Materials (MindTap Course List)
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:
9781337093347
Author:
Barry J. Goodno, James M. Gere
Publisher:
Cengage Learning
Engineering Mechanics: Statics
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:
9781118807330
Author:
James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:
WILEY