Claims Analysis
Total Claims: 13
Claim 1
Independent Claim
214 words
A combustion process for a nitrogen-bearing fuel comprising the steps of: (a) introducing said fuel into a first combustion zone; (b) combusting said fuel in said first combustion zone under a condition of fuel-rich stoichiometry at an oxygen to fuel stoichiometric ratio of from 0.45 to 0.80 and at a temperature in the range of from 1500 K to 1800 K whereby fuel-rich combustion products are produced and undesirable nitrogenous compounds are reduced to low levels; (c) passing said fuel-rich combustion products into a two-stage final combustion zone; (d) combusting said fuel-rich combustion products in the first stage of said final combustion zone under a condition of fuel-rich stoichiometry at an oxygen to fuel stoichiometric ratio of from 0.80 to 1.0 and at a temperature in the range of from 1500 K to 2200 K to produce combustion products having nitrogenous oxide levels reduced substantially to near zero while substantially burning out combustibles virtually free from generation of any additional thermal nitrogenous oxides; and (e) thereafter, combusting said combustion products in the second stage of said final combustion zone at an oxygen to fuel stoichiometric ratio of greater than 1.0 and at a temperature of less than 1500 K to facilitate substantially complete fuel burnout in the second stage of said final combustion zone.
Claim 2
Dependent Claim
214 words
A combustion process for a nitrogen-bearing fuel comprising the steps of: (a) introducing said fuel into a first combustion zone; (b) combusting said fuel in said first combustion zone under a condition of fuel-rich stoichiometry at an oxygen to fuel stoichiometric ratio of from 0.45 to 0.80 and at a temperature in the range of from 1500 K to 1800 K whereby fuel-rich combustion products are produced and undesirable nitrogenous compounds are reduced to low levels; (c) passing said fuel-rich combustion products into a two-stage final combustion zone; (d) combusting said fuel-rich combustion products in the first stage of said final combustion zone under a condition of fuel-rich stoichiometry at an oxygen to fuel stoichiometric ratio of from 0.80 to 1.0 and at a temperature in the range of from 1500 K to 2200 K to produce combustion products having nitrogenous oxide levels reduced substantially to near zero while substantially burning out combustibles virtually free from generation of any additional thermal nitrogenous oxides; and (e) thereafter, combusting said combustion products in the second stage of said final combustion zone at an oxygen to fuel stoichiometric ratio of greater than 1.0 and at a temperature of less than 1500 K to facilitate substantially complete fuel burnout in the second stage of said final combustion zone.
Claim 3
Dependent Claim
29 words
The process defined in claim 1, wherein to said first combustion zone is added a finely dispersed particulate material which enhances conversion of undesirable nitrogenous compounds to molecular nitrogen.
Claim 4
Dependent Claim
27 words
The process defined in claim 2, wherein said particulate material is selected from the group comprising calcium sulphide, calcium oxide, iron sulphide, iron oxide and mixtures thereof.
Claim 5
Dependent Claim
27 words
The process defined in claim 1, wherein the condition of fuel-rich stoichiometry in said first combustion zone comprises an oxygen/fuel stoichiometric ratio of from 0.55 to 0.70.
Claim 6
Dependent Claim
267 words
A combustion process for a sulphur- and nitrogen bearing fuel comprising the steps of: (a) introducing said fuel into a first combustion zone; (b) combusting said fuel in the presence of a sulphur-capture compound in said first combustion zone under a condition of fuel-rich stoichiometry and at a temperature whereby a combustion mixture is produced including fuel-rich gases, solid sulphur-bearing flash and slag; (c) passing said combustion mixture to a second combustion zone; (d) combusting said combustion mixture in said second combustion zone under a condition of fuel-rich stoichiometry at an oxygen to fuel stoichiometric ratio of from 0.45 to 0.80 and at a temperature range of from 1500 K to 1800 K whereby fuel-rich combustion products are produced and undesirable nitrogenous compounds are reduced to a low level; (e) passing said fuel-rich combustion products into a two-stage final combustion zone; (f) combusting said fuel-rich combustion products in the first stage of said final combustion zone under a condition of fuel-rich stoichiometry at an oxygen to fuel stoichiometric ratio of from 0.80 to 1.0 and at a temperature in the range of from 1500 K to 2200 K to produce combustion products having nitrogenous oxide levels reduced substantially to near zero while substantially burning out combustibles virtually free from generation of any additional thermal nitrogenous oxides; and (g) thereafter, combusting said combustion products in the second stage of said final combustion zone at an oxygen to fuel stoichiometric ratio of greater than 1.0 and at a temperature of less than 1500 K to facilitate substantially complete fuel burnout in the second stage of said final combustion zone.
Claim 7
Dependent Claim
267 words
A combustion process for a sulphur- and nitrogen bearing fuel comprising the steps of: (a) introducing said fuel into a first combustion zone; (b) combusting said fuel in the presence of a sulphur-capture compound in said first combustion zone under a condition of fuel-rich stoichiometry and at a temperature whereby a combustion mixture is produced including fuel-rich gases, solid sulphur-bearing flash and slag; (c) passing said combustion mixture to a second combustion zone; (d) combusting said combustion mixture in said second combustion zone under a condition of fuel-rich stoichiometry at an oxygen to fuel stoichiometric ratio of from 0.45 to 0.80 and at a temperature range of from 1500 K to 1800 K whereby fuel-rich combustion products are produced and undesirable nitrogenous compounds are reduced to a low level; (e) passing said fuel-rich combustion products into a two-stage final combustion zone; (f) combusting said fuel-rich combustion products in the first stage of said final combustion zone under a condition of fuel-rich stoichiometry at an oxygen to fuel stoichiometric ratio of from 0.80 to 1.0 and at a temperature in the range of from 1500 K to 2200 K to produce combustion products having nitrogenous oxide levels reduced substantially to near zero while substantially burning out combustibles virtually free from generation of any additional thermal nitrogenous oxides; and (g) thereafter, combusting said combustion products in the second stage of said final combustion zone at an oxygen to fuel stoichiometric ratio of greater than 1.0 and at a temperature of less than 1500 K to facilitate substantially complete fuel burnout in the second stage of said final combustion zone.
Claim 8
Dependent Claim
27 words
The process defined in claim 5, wherein the condition of fuel-rich stoichiometry in said first combustion zone comprises an oxygen/fuel stoichiometric ratio of less than about 0.50.
Claim 9
Dependent Claim
29 words
The process defined in claim 5, wherein the condition of fuel-rich stoichiometry in said first combustion zone comprises an oxygen/fuel stoichiometric ratio of from about 0.25 to about 0.40.
Claim 10
Dependent Claim
27 words
The process defined in claim 7, wherein the condition of fuel-rich stoichiometry in said second combustion zone comprises an oxygen/fuel stoichiometric ratio of from 0.55 to 0.70.
Claim 11
Dependent Claim
25 words
The process defined in claim 7, wherein the temperature in said first combustion zone is in the range of from 1200 K to 1600 K.
Claim 12
Dependent Claim
25 words
The process defined in claim 5, wherein said sulphur-capture compound is selected from the group comprising oxides, hydroxides and carbonates of calcium, and combinations thereof.
Claim 13
Dependent Claim
22 words
The process defined in claim 1 or claim 5, wherein said fuel is selected from the group comprising petroleum products and by-products.