Hydrogen Hybrid?
Im sure I read somewhere that given enough pressure, a Hydrogen/Oxygen mix can ignite itself. Would this pose a significant danger if one wanted to build a hydrogen hybrid with mixes of 5x+? Ive been looking but there seems to be no accurate pressures at which it could happen. (Im assuming there are many factors that have to be taken into account).
Update:
Just found out a 4:1 - 5:1 mix will prevent an oxidizing flame whilst still leaving the mix combustible by manual ignition.
http://en.wikipedia.org/wiki/Oxyhydrogen
Update:
Just found out a 4:1 - 5:1 mix will prevent an oxidizing flame whilst still leaving the mix combustible by manual ignition.
http://en.wikipedia.org/wiki/Oxyhydrogen
Last edited by Alster370 on Thu Jun 02, 2011 8:26 am, edited 1 time in total.
Threads from forums where "HHO" is an accepted term are not "relevant" to anything, ever. Thank you for not using it here.
Utron uses oxygen/hydrogen/buffer (where the buffer is often simply excess hydrogen) mixes at up to ~10000psi pre-ignition. While these are not pure, stoichiometric oxygen/hydrogen fuel mixes, they are at extremely high pressure compared to what you're likely to be working with. Further, the Space Shuttle's liquid fueled rocket engines also run oxygen/hydrogen, mixing high pressure gaseous hydrogen with liquid oxygen. They still need an ignition system.
Hydrogen is an excellent fuel choice, and also an excellent buffer gas for hybrid mixes (surpassed by helium in that regard for most applications). The use of rich mixes not only decreases chances of auto-ignition, it reduces likelihood of detonations and significantly improves sound speed in the propellant gases.
Utron uses oxygen/hydrogen/buffer (where the buffer is often simply excess hydrogen) mixes at up to ~10000psi pre-ignition. While these are not pure, stoichiometric oxygen/hydrogen fuel mixes, they are at extremely high pressure compared to what you're likely to be working with. Further, the Space Shuttle's liquid fueled rocket engines also run oxygen/hydrogen, mixing high pressure gaseous hydrogen with liquid oxygen. They still need an ignition system.
Hydrogen is an excellent fuel choice, and also an excellent buffer gas for hybrid mixes (surpassed by helium in that regard for most applications). The use of rich mixes not only decreases chances of auto-ignition, it reduces likelihood of detonations and significantly improves sound speed in the propellant gases.
Spudfiles' resident expert on all things that sail through the air at improbable speeds, trailing an incandescent wake of ionized air, dissociated polymers and metal oxides.
1+ on that...DYI wrote:Threads from forums where "HHO" is an accepted term are not "relevant" to anything, ever. Thank you for not using it here.
but here is what I am worried about, won't the combustion chamber be susceptible to hydrogen embrittlement?? would this be cause for concern in this applecation, or am I being paranoid...
The voices in my head may not be real, but they have some good ideas!
- Labtecpower
- Sergeant 3
- Posts: 1297
- Joined: Sat Feb 20, 2010 6:38 am
- Location: Pyongyang
- Has thanked: 5 times
- Been thanked: 13 times
Low tensile strength steel isn't susceptible to hydrogen embrittlement.
I was also thinking about a hydrogen/oxygen hybrid. I will first have to build myself a better electrolysis cell.
What power gain would it have over a conventional air/propane hybrid? the gas itself has a far higher burning speed and SOS, but a stochiometric mixture of oxygen and hydrogen will only produce water (probably as steam) as a reaction product. Will it give enough pressure to push a projectile down a barrel of about 3 m?
I was also thinking about a hydrogen/oxygen hybrid. I will first have to build myself a better electrolysis cell.
What power gain would it have over a conventional air/propane hybrid? the gas itself has a far higher burning speed and SOS, but a stochiometric mixture of oxygen and hydrogen will only produce water (probably as steam) as a reaction product. Will it give enough pressure to push a projectile down a barrel of about 3 m?
I may be in a little over my head here anyway, Im only just covered fuel metering and such. I might just try a combustion for now, to keep things simple as I doubt im going to accomplish anything other than injuring myself if I attempt a Piston hybrid. Now I imagine copper is not suitable for a hydrogen combustion due to hydrogen embrittlement? Also would i keep the Hyd/Oxg ratio 2:1 for the most pressure?
thanks
thanks
In some cases, it could be. Stainless (not usually austentitic stainless though) and high strength, low alloy steels are quite susceptible, as are many nickel or titanium based alloys. As Labtec mentioned, lower strength, softer steels are not so badly affected.Won't the combustion chamber be susceptible to hydrogen embrittlement? Would this be cause for concern in this application, or am I being paranoid...
For a given quantity of oxygen (which is what we typically measure the "mix number" by), propane mixes will produce higher pressures. However, the low propellant gas SOS in propane/air hybrids will start to cut back efficiency as you exceed 800m/s or so, and much higher than that they become less useful. Compare to 1550 m/s for 2:1 hydrogen/oxygen and 1870m/s for 4:1, which produces similar pressure per X and is less prone to detonation (and accidental ignition, of course).What power gain would it have over a conventional air/propane hybrid?
If you're trying to compare 2:1 hydrogen/oxygen to stoichiometric air/propane at the same starting pressure, the hydrogen/oxygen mix will produce very slightly higher pressure than air/propane, and for 4:1 the pressure will be almost exactly the same.
How long is a piece of string?Will it give enough pressure to push a projectile down a barrel of about 3 m?

Copper doesn't suffer from conventional embrittlement, but it can be attacked by hot hydrogen if there is sufficient oxygen content in the copper. I don't think this would be of particular concern in your application, especially when using a 2:1 ratio.Now I imagine copper is not suitable for a hydrogen combustion due to hydrogen embrittlement?
I must admit to experiencing a moment of confusion upon reading that, what with the amount of time I seem to spend trying to achieve the opposite situation... The answer is that you'll actually want about 2.3:1 for the highest pressure. Also, I highly recommend downloading GasEq. It's free software, and would allow you to investigate many of these queries for yourself.Also would I keep the Hyd/Oxg ratio 2:1 for the most pressure?
Spudfiles' resident expert on all things that sail through the air at improbable speeds, trailing an incandescent wake of ionized air, dissociated polymers and metal oxides.
Did we ever reach consensus on if it is safe to compress an stoichiometric mix of oxygen and hydrogen with a shock pump? I think it's safe to assume that a fridge compressor or other mechanical pump would be a bad idea.
POLAND_SPUD wrote:even if there was no link I'd know it's a bot because of female name
Considering the UEL of hydrogen in air is 75% (5% oxygen in the mix), you shouldn't have any trouble igniting an 83% hydrogen mix with 17% oxygen. The pre-ignition pressure will be getting pretty high here though - at 18.5 psi/X (including the oxygen), you'd better have a high pressure hydrogen source handy....or 5:1...
Spudfiles' resident expert on all things that sail through the air at improbable speeds, trailing an incandescent wake of ionized air, dissociated polymers and metal oxides.
pressure would build, and some hydrogen and oxygen would dissolve in the water. It is worth noting that you would get "wet" hydrogen and oxygen in your chamber, as opposed to "dry" gasses. This makes detonation less likely, but would reduce the temperature and pressure of the gas in your chamber. You'd have to collect the hydrogen and oxygen separately, and somehow dispose of the pressurized oxygen if you wanted anything but a 2:1 ratio.
POLAND_SPUD wrote:even if there was no link I'd know it's a bot because of female name
- Fnord
- First Sergeant 2
- Posts: 2239
- Joined: Tue Feb 13, 2007 9:20 pm
- Location: Pripyat
- Been thanked: 1 time
- Contact:
I'd think any water vapor present would act as a buffer gas, turning to steam during ignition. Of course, high concentrations may be counterproductive (I know from experience they are with propane and acetylene), but some experimentation would be necessary to see what levels you actually end up with in practice.
Also, Without doing any research at all, I remember seeing a few electrolysis rigs blowing up on youtube without an apparent source of ignition energy. Any thoughts on this?
Also, Without doing any research at all, I remember seeing a few electrolysis rigs blowing up on youtube without an apparent source of ignition energy. Any thoughts on this?

according to gaseq, if about 1/7 of the moles of gas is water vapor in a stoich mix of h2 and 02, pressure will drop from 9.56 bar to 9 bar and SoS will drop from 1553 m/s to 1450 m/s. A 4:1 ratio has about the same pressure drop, and a SoS drop of about 200m/s.Fnord wrote:I'd think any water vapor present would act as a buffer gas, turning to steam during ignition. Of course, high concentrations may be counterproductive (I know from experience they are with propane and acetylene), but some experimentation would be necessary to see what levels you actually end up with in practice.
Also, Without doing any research at all, I remember seeing a few electrolysis rigs blowing up on youtube without an apparent source of ignition energy. Any thoughts on this?
I remember seeing videos (can't find them again) comparing igniting wet hydrogen from an electrolysis cell and the ignition of dry hydrogen from a bottle. The wet stuff had a dull thump at best, but the dry gas had a sharp crack.
As to the spontaneous ignition, there are a number of possible causes. Loose electrodes causing sparks, floating debris shorting electrodes, downstream ignition and flashback.
POLAND_SPUD wrote:even if there was no link I'd know it's a bot because of female name