How Does Fuel Expansion and Contraction Work in Pulse Jet Engines?

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SUMMARY

The discussion focuses on the mechanics of fuel expansion and contraction in pulse jet engines, specifically addressing the combustion process of a gasoline/air mixture with a ratio of 15:1. It highlights that upon ignition, the fuel expands, creating exhaust gases that exit through a 2-inch diameter exhaust pipe, while the combustion chamber is typically 4 inches in diameter. The ideal gas law, represented as PV = nRT, is essential for calculating the volume of the combustion chamber, which is influenced by the burning temperature and pressure. Additionally, the interaction between the expanding gases and the engine design plays a crucial role in the overall efficiency of the pulse jet engine.

PREREQUISITES
  • Understanding of pulse jet engine mechanics
  • Familiarity with the ideal gas law (PV = nRT)
  • Knowledge of fuel/air mixture ratios in combustion
  • Basic principles of thermodynamics related to gas expansion and contraction
NEXT STEPS
  • Research the effects of temperature on combustion efficiency in pulse jet engines
  • Explore advanced calculations for combustion chamber volume using the ideal gas law
  • Investigate the design considerations for optimizing pulse jet engine performance
  • Learn about the differences between pulse jet engines and internal combustion engines
USEFUL FOR

Aerospace engineers, mechanical engineers, and students studying propulsion systems will benefit from this discussion, particularly those interested in the dynamics of pulse jet engines and combustion processes.

gary350
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When a fuel/air mixture burns it expands. How much does it expand? Is there a formula or known volume increase?

After a fuel burns it contracts. How much does it contract? Is there a formula or known volume that it contracts?

Gasoline/Air mixture ratio is 15 to 1 for jet engines.

A fuel is injected into a pulse jet combustion chamber and mixes with the air in the chamber at atmosphereic pressure 14.7 psi. The fuel ignites and burns and the expanding gas goes out the exhaust tail pipe. The burned fuel then produces a vacuum that sucks fresh air in through the intake valves that mixes with more fuel and it ignites and burns. The cycle repeats over and over. The combustion chamber is typically 2 times the diameter of the exhaust pipe. A 2" diameter exhaust pipe will have a 4" diameter combustion chamber. The cross sectional area of the combustion chamber is 3 times larger than the exhaust pipe. Pretty simple so far but now we need to calculate the volume of the combustion chamber?
 
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Depends on the temperature at which the given fuel burns at the particular pressure in the cylinder. You can get a fairly accurate result by applying the ideal gas law, PV = nRT.
 
don't know about jets but
do not omit the fact that in the IC engine, once the fuel/ air mix is lit, it begins to do work by moving the piston. this expands the combustion chamber volume, drops temperature, reduces initial ignition pressure immediately.
 
Ranger Mike said:
don't know about jets but
do not omit the fact that in the IC engine, once the fuel/ air mix is lit, it begins to do work by moving the piston. this expands the combustion chamber volume, drops temperature, reduces initial ignition pressure immediately.

...and the volume to which the gas expands is, by definition, dictated by the engine design.
 
exactly
brewnog..you are a valuable asset on this forumn
 

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