How difficult will it be to build a 'hybrid' Jet engine?

Click For Summary
SUMMARY

The discussion centers on the feasibility of developing a hybrid turbofan jet engine capable of utilizing both kerosene and gaseous hydrogen as fuel. The proposed concept involves using excess electricity generated by the engine's turbines to produce hydrogen through electrolysis, which would then be used to power the engine after kerosene. Despite the innovative idea, participants express skepticism regarding the practicality and efficiency of modifying existing engine designs to accommodate this dual-fuel system, with concerns about the sufficient supply of hydrogen and the overall viability of such technology.

PREREQUISITES
  • Understanding of turbofan engine architecture
  • Knowledge of fuel types and combustion processes
  • Familiarity with electrolysis and hydrogen production methods
  • Insights into energy efficiency and thermodynamics
NEXT STEPS
  • Research advancements in hybrid propulsion systems
  • Explore current developments in hydrogen fuel technology
  • Investigate modifications in existing turbofan engines for dual-fuel capabilities
  • Examine case studies on energy efficiency in aerospace engineering
USEFUL FOR

Aerospace engineers, propulsion system designers, and researchers interested in alternative fuel technologies for aviation.

royp
Messages
55
Reaction score
22
PMM and Over-Unity mechanisms are not discussed at PF
TL;DR
Can we build a jet engine which will be able to handle both Kerosene and (gaseous) Hydrogen as fuel? After burning the kerosene for a while, Hydrogen will take over as the fuel, burning to produce the exhaust gas and resulting thrust.
Hi,
Here is a question - somewhat futuristic and at the moment, hypothetical.
How difficult will it be to build a 'hybrid' Jet (turbofan) engine? The engine should be able to handle both Kerosene and (gaseous) Hydrogen as fuel. After burning the kerosene for a while, Hydrogen will take over as the fuel, burning to produce the exhaust gas and resulting thrust. Let me clarify. Imagine, there are excess electricity produced by the turbine(s) of the engine(s). This electricity will be used to produce Hydrogen by electrolysis of water and Hydrogen gas (so produced), in turn, will be fed into the engine. There is obviously the question of feasibility of producing enough Hydrogen .But the focus of my question really is: assuming there are enough supply, can an engine (with current design/architecture) be suitably modified to achieve this?
 
Physics news on Phys.org
I used to do consulting work with a local patent attorney. Almost all of the attempts gain efficiency were a "partial" perpetual motion machine. I remember very well elderly farmer who was convinced he could add an air compressor to his system and regeneratively run it to his advantage. I convinced him this was unlikely and saved him some money...although maybe he would have been happier working on it...
Anyhow your jet seems very unlikely to be useful...convince me otherwise.

'/
 
  • Like
Likes russ_watters and berkeman
Thread closed for Moderation...
 
hutchphd said:
...convince me otherwise.
Not at PF. That kind of discussion is not allowed here. Thread will remain closed.
 
  • Like
Likes hutchphd

Similar threads

  • · Replies 5 ·
Replies
5
Views
3K
Replies
2
Views
3K
  • · Replies 9 ·
Replies
9
Views
8K
Replies
2
Views
1K
  • · Replies 3 ·
Replies
3
Views
3K
  • · Replies 4 ·
Replies
4
Views
6K
  • · Replies 20 ·
Replies
20
Views
5K
  • · Replies 37 ·
2
Replies
37
Views
6K
Replies
39
Views
5K
  • · Replies 4 ·
Replies
4
Views
8K