Difference between revisions of "Brayton cycle"

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The Brayton cycle is a thermodynamic cycle that can be used for power generation.
 
The Brayton cycle is a thermodynamic cycle that can be used for power generation.
 
It uses a gas a working medium.
 
It uses a gas a working medium.
An airplane turbo engine is an example of an open Brayton cycle
+
*An airplane turbo engine is an example of an open Brayton cycle
A nuclear reactor power plant using helium cooling is an example of a closed Brayton cycle.
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*A nuclear reactor power plant using helium cooling is an example of a closed Brayton cycle.
  
The ideal equation for a Brayton cycle is efficiency(ef) = 1-Tc/Th.   
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*The ideal equation for a Brayton cycle is efficiency(ef) = 1-Tc/Th.   
An actual Brayton engine has a number of inefficiencies and non-reversible, so the actual efficiency is significantly lower.
+
*An actual Brayton engine has a number of inefficiencies and non-reversible, so the actual efficiency is significantly lower.
 
So for a high efficiency Brayton cycle, Th needs to be significantly higher than Tc.
 
So for a high efficiency Brayton cycle, Th needs to be significantly higher than Tc.
  
For example, with an efficiency of 40% Tc/Th is 0,6.  If Tc is 500K, then Th is 830K.
+
*For example, with an efficiency of 40% Tc/Th is 0,6.  If Tc is 500K, then Th is 830K.
For the same example at 60% efficiency, Tc/Th=0,4, and for a TC of 500K Th is 1250K.
+
*For the same example at 60% efficiency, Tc/Th=0,4, and for a TC of 500K Th is 1250K.
  
If applied to a closed cycle used on Mars, Tc is the radiator temperature, and Th would be the temperature of the reactor core.
+
*If applied to a closed cycle used on Mars, Tc is the radiator temperature, and Th would be the temperature of the reactor core.

Revision as of 11:10, 2 October 2022

The Brayton cycle is a thermodynamic cycle that can be used for power generation. It uses a gas a working medium.

  • An airplane turbo engine is an example of an open Brayton cycle
  • A nuclear reactor power plant using helium cooling is an example of a closed Brayton cycle.
  • The ideal equation for a Brayton cycle is efficiency(ef) = 1-Tc/Th.
  • An actual Brayton engine has a number of inefficiencies and non-reversible, so the actual efficiency is significantly lower.

So for a high efficiency Brayton cycle, Th needs to be significantly higher than Tc.

  • For example, with an efficiency of 40% Tc/Th is 0,6. If Tc is 500K, then Th is 830K.
  • For the same example at 60% efficiency, Tc/Th=0,4, and for a TC of 500K Th is 1250K.
  • If applied to a closed cycle used on Mars, Tc is the radiator temperature, and Th would be the temperature of the reactor core.