US2004048211A1PendingUtilityA1
Catalytic combustion device with liquid fuel vaporisation on hot walls
Priority: Dec 11, 2000Filed: Dec 5, 2001Published: Mar 11, 2004
Est. expiryDec 11, 2020(expired)· nominal 20-yr term from priority
F23C 13/00F23D 9/00F23R 3/30F23R 3/40
36
PatentIndex Score
0
Cited by
0
References
0
Claims
Abstract
The present invention relates to a catalytic combustion device comprising a main combustion zone ( 20, 200 ) including at least one catalytic section ( 5, 103 ) and at least one air/fuel mixing zone ( 11, 117 ), said mixing zone comprising at least one pressurized air inlet ( 1, 101 ) and injection means ( 12, 105 ) for injecting a liquid fuel. According to the invention, injection means ( 12, 105 ) project the liquid fuel onto a hot wall ( 13, 15, 107 ) of said device so as to allow vaporization of said fuel on contact with this wall.
Claims
exact text as granted — not AI-modified1 ) A catalytic combustion device comprising a main combustion zone ( 20 , 200 ) including at least one catalytic section ( 5 , 103 ), at least one air/fuel mixing zone ( 11 , 117 ), said mixing zone comprising at least one pressurized air inlet ( 1 , 101 ), and liquid fuel injection means ( 12 , 105 ), characterised in that injection means ( 12 , 105 ) project the liquid fuel onto a wall heated by the combustion of the air/fuel mixture main combustion zone ( 13 , 15 , 107 ) so as to allow vaporization of said fuel on contact with said wall.
2 ) A device as claimed in claim 1 , characterised in that the fuel is projected substantially perpendicular to hot wall ( 13 , 15 , 107 ).
3 ) A device as claimed in claim 1 or 2 , characterised in that said hot wall ( 15 ) consists at least partly of at least one of the walls of main combustion zone ( 20 ).
4 ) A device as claimed in claim 1 or 2 , further comprising a combustion initiation zone ( 4 , 102 ), characterised in that said hot wall ( 13 ) consists at least partly of at least one of the walls of combustion initiation zone ( 4 ).
5 ) A device as claimed in any one of claims 1 or 2 , wherein at least one postcombustion zone ( 14 , 108 ) is arranged downstream from main combustion zone ( 20 , 200 ), characterised in that hot wall ( 15 , 107 ) consists at least partly of at least one of the walls of said postcombustion zone.
6 ) A device as claimed in any one of the previous claims, characterised in that the means allowing injection of the liquid fuel are injectors ( 12 , 105 ) providing primary spraying such that the size of the droplets coming from said injectors ( 12 , 105 ) ranges between 5 and 60 μm, preferably between 10 and 40 μm
7 ) A device as claimed in any one of the previous claims, characterised in that hot wall ( 13 , 15 , 107 ) of the zone opposite said injection means has a substantially plane shape.
8 ) A device as claimed in any one of claims 1 to 6 , characterised in that hot wall ( 13 , 15 , 107 ) of the zone opposite the injectors has a concave curved shape.
9 ) A device as claimed in any one of the previous claims, characterised in that the temperature of said hot wall ( 13 , 15 , 107 ) of said device is substantially equal to or higher than the maximum boiling temperature of the liquid fuel on said wall.
10 ) A device as claimed in any one of the previous claims, characterised in that wall ( 107 ) receiving the impact of the fuel jets is equipped with means allowing to increase the heat transfer from the hot zone to the spraying zone.
11 ) A device as claimed in any one of the previous claims, characterised in that wall ( 107 ) is covered at least partly with an insulating material, except for a zone ( 120 ) receiving the impact of the fuel jets.
12 ) Application of the device as claimed in any one of the previous claims to gas turbines provided with a heat recuperator.
13 ) Application of the device as claimed in any one of claims 1 to 11 to combustion chambers of annular geometry.Join the waitlist — get patent alerts
Track US2004048211A1 — get alerts on status changes and closely related new filings.
We store only your email — no account needed. See our privacy policy.