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I was taught in A&P school that the earliest jets burned avgas, which had the bad effects of coating the internals of the engine with toxic baked on fuel additives, notably tetraethyl lead. This negatively affected the aerodynamics of burner cans and turbine blades, as well as heat dissipation. We had a J34 at school that had hung for several years under the wing of a P2V7 Neptune and burned 115/145. The hot section looked like it was made of some brown ceramic material.Producing many thousands of gallons of kerosene for jets would leave you with twice as much gasoline that you did not have a use for. So they invented JP-4, which is a mixture of kerosene and gasoline, and thus makes better use of the fuels you can get out of a barrel of oil.
Like hard-deposits?I was taught in A&P school that the earliest jets burned avgas, which had the bad effects of coating the internals of the engine with toxic baked on fuel additives, notably tetraethyl lead.
Wait, I thought jet-fuel was less volatile than gasoline? As for the Oriskany and Forrestal, I thought they were using JP-5 at that point?Enter JP4, a mixture of kerosene and plain additive free gasoline. Good atomization, no baked on additives, starts well, good energy density. Only trouble is, it's volatile as all hell and has to be handled even more carefully than straight avgas. For the Air Force and shoreside uses, that was a more or less acceptable solution, but at sea, Oriskany, Forrestal, and other shipboard disasters proved it wasn't.
As I stated in my post, the entire hot section looked like it was made of a smooth, hard, brownish tan ceramic material.Like hard-deposits?
Today's Jet A and JP5 are less volatile than avgas, and I've heard that JP4 has reduced its gasoline component over the years as well. But, as with so many choices in aviation, it's a trade-off between performance and safety. Kerosene has less energy density than gasoline, but is also less volatile.Wait, I thought jet-fuel was less volatile than gasoline? As for the Oriskany and Forrestal, I thought they were using JP5 at that point?
It had to wait until the early type turbine engines were mostly gone. Their fuel nozzles just couldn't achieve the small droplet, fine mist spray with kerosene that they could with gasoline and JP4. A fuel nozzle has to inject a carefully shaped high velocity fog into the center of the burner can which will support a flame suspended in the middle of the space. If the flame comes in contact with the chamber walls you've got an instant over temp. This is what happens in a hot start. If fuel pressure at the nozzle isn't high enough and/or the air velocity too low, the fuel "fog" doesn't stay in suspension but starts to pool on the floor of the chamber, guaranteeing an over temp start, which can lead to crack$ in the burner can$. $$$$!So it was phased in from around 1952 (first tested) to around 1967?
It had to wait until the early type turbine engines were mostly gone. Their fuel nozzles just couldn't achieve the small droplet, fine mist spray with kerosene that they could with gasoline and JP4. A fuel nozzle has to inject a carefully shaped high velocity fog into the center of the burner can which will support a flame suspended in the middle of the space. If the flame comes in contact with the chamber walls you've got an instant over temp. This is what happens in a hot start. If fuel pressure at the nozzle isn't high enough and/or the air velocity too low, the fuel "fog" doesn't stay in suspension but starts to pool on the floor of the chamber, guaranteeing an over temp start, which can lead to crack$ in the burner can$. $$$$!