Gaseous oxygen resonance igniter
View Patent ↗A gaseous oxygen resonance igniter includes a body with a first inlet for gaseous oxygen incorporating a supersonic nozzle. An outlet from the body incorporates an orifice of predetermined size to maintain a desired pressure in the body. An aperture in the body opposite the first inlet provides a port to a ceramic resonance cavity. A ceramic bleed disc is engaged at a second end of the resonance cavity. An end cap incorporates a plenum adapted to receive high temperature oxygen flow from the resonance cavity through the bleed disc. An exhaust port is connected to the plenum for the high temperature oxygen which flows to a mixing chamber which introduces pilot fuel for ignition as a combustion initiation torch.
1. A gaseous oxygen resonance igniter comprising:
a body having a first inlet for gaseous oxygen, the inlet incorporating a supersonic nozzle, and an outlet incorporating an orifice of predetermined size to maintain a desired pressure in the body, the body further having an aperture opposite the first inlet;
a ceramic resonance cavity engaged at a first end in the aperture of the body;
a ceramic bleed disc engaged at a second end of the resonance cavity;
an end cap having a plenum adapted to receive high temperature oxygen flow from the resonance cavity through the bleed disc and having an exhaust port connected to the plenum; and,
means for mixing high temperature oxygen from the exhaust port with fuel for ignition as a combustion initiation torch.
2. A gaseous oxygen resonance igniter as defined in claim 1 further comprising a sleeve intermediate the body and the plenum having a bore in which the ceramic resonance cavity is received.
3. A gaseous oxygen resonance igniter as defined in claim 2 further comprising a plurality of tensioning bolts securing the end cap and sleeve to the body.
4. A gaseous oxygen resonance igniter as defined in claim 3 wherein the plurality of bolts are circumferentially spaced about the resonance cavity and extend through the end cap and sleeve to be received in threaded holes in the body.
5. A gaseous oxygen resonance igniter as defined in claim 1 further comprising means for sealing the resonance cavity to the body.
6. A gaseous oxygen resonance igniter as defined in claim 2 further comprising means for sealing the resonance cavity to the sleeve.
7. A gaseous oxygen resonance igniter as defined in claim 2 wherein the ceramic bleed disc is secured intermediate the end cap the sleeve.
8. A gaseous oxygen resonance igniter as defined in claim 7 further comprising means for sealing the ceramic bleed disc to the sleeve and end cap.
9. A gaseous oxygen resonance igniter as defined in claim 2 wherein the body, sleeve and end cap are stainless steel.
10. A gaseous oxygen resonance igniter as defined in claim 9 wherein the plenum of the end cap is coated with a thermal barrier.
11. A gaseous oxygen resonance igniter as defined in claim 1 wherein the ceramic resonance cavity is aluminum silicate.
12. A gaseous oxygen resonance igniter as defined in claim 1 wherein the ceramic bleed disc is aluminum silicate.
13. A gaseous oxygen resonance igniter as defined in claim 1 wherein the ceramic for the resonance cavity is selected from the group consisting of silicon nitride, carbon/silicon carbide, aluminum silicate, glass-mica, aluminum/zirconia, and mullite.
14. A gaseous oxygen resonance igniter as defined in claim 1 wherein the ceramic for the bleed disc is selected from the group consisting of silicon nitride, carbon/silicon carbide, aluminum silicate, glass-mica, aluminum/zirconia, and mullite.
15. A gaseous oxygen resonance igniter as defined in claim 1 wherein the mixing means comprises a pilot mixing chamber connected to the exhaust port and having a reactant supply port for mixing fuel with the oxygen and an exhaust orifice for a pilot torch and further comprising a reactant source.
16. A gaseous oxygen resonance igniter as defined in claim 15 further comprising:
a second mixing chamber connected to the body outlet to receive oxygen flow and connected to the exhaust orifice to receive the pilot torch; and
a reactant manifold connected to the second mixing chamber for introduction of fuel for mixture with the oxygen.
17. A gaseous oxygen resonance igniter as defined in claim 15 wherein the fuel is selected from hydrogen, methane, ethane and propane.
18. A gaseous oxygen resonance igniter as defined in claim 15 wherein the fuel is a hydrocarbon fuel.
19. A gaseous oxygen resonance igniter as defined in claim 16 wherein the fuel is selected from hydrogen, methane, ethane and propane.
20. A gaseous oxygen resonance igniter as defined in claim 16 wherein the fuel is a hydrocarbon fuel.