Pulse combustion apparatus and method

Claim 2

A pulse combustion apparatus wherein explosive combustion cycles provide gas pressure oscillations comprising a primary burner means operably connected to a main burner means to flow combustion gases from said primary to said main burner means, fuel supply means for self-feeding a combustible gaseous mixture of each of said primary and main burner means, combustion chamber means for pulse combustion of said combustible gaseous mixture to provide combustion gases, and exhaust means for self-exhausting said combustion gases from said apparatus, each of said burner means being separately operable after start-up to provide self-sustaining pulse combustion of said combustible gaseous mixture, said burner means also being simultaneously operable with said combustion chamber means and exhaust means cooperating to provide resonant combustion of combustible gaseous mixtures in each of said burner means at substantially the same frequency of pressure oscillations for self-feeding said combustible gaseous mixture and self-exhausting said combustion gases in accordance with said pressure oscillations.

Claim 3

An apparatus according to claim 1, wherein said primary burner means cooperates with said fuel supply means to provide a flow of said combustible gaseous mixture to said main burner means during start-up of the main burner means.

Claim 4

An apparatus according to claim 2, wherein combustion gases from said primary burner means provide ignition of said combustible gaseous mixture in said main burner means during start-up.

Claim 5

An apparatus according to claim 3, wherein said combustion chamber means includes a common chamber for combustion of combustible gaseous mixture supplied to each of said burner means.

Claim 6

An apparatus according to claim 4, wherein each of said burner means includes a mixer head for receiving combustible gaseous mixture from said fuel supply means, and said primary burner mixer head includes an outlet opening into said main burner mixer head.

Claim 7

An apparatus according to claim 5, wherein said main burner mixer head includes an outlet opening into said common chamber.

Claim 8

An apparatus according to claim 6, wherein said burner mixer heads and common chamber are aligned along a central axis.

Claim 9

An apparatus to claim 3, wherein said primary and main burner means respectively include a primary and a main mixer head, each of said mixer heads being adapted to receive combustible gaseous mixture from said fuel supply means, said combustion chamber means includes a primary and a main combustion chamber respectively associated with said primary and main mixer heads for combustion of combustible gaseous mixture fed into the mixer heads, and said exhaust means includes a primary and a main tailpipe respectively associated with said primary and main combustion chambers for receiving combustion gases from the combustion chambers, said primary tailpipe being connected to said main mixer head, and said main tailpipe discharging said combustion gases from said apparatus.

Claim 10

An apparatus according to claim 3, wherein said primary burner means is sized to have a primary fuel input rate, said main burner means is sized to have a main fuel input rate, said main fuel input rate being higher than said primary fuel input rate, and said main burner means also includes valve means to regulate the flow of combustible gaseous mixture to said main burner means and the turndown ratio of said apparatus, said primary burner means reducing the frequency and pressure amplitude variations in said main burner means as compared with a similarly sized burner not including a primary burner means whereby said turndown ratio of said apparatus is larger than it would be in such similarly sized burner not including primary burner means.

Claim 11

A pulse combustion apparatus comprising a primary burner, a main burner, fuel supply means for self-feeding of a combustible gaseous mixture to each of said burners, combustion chamber means for pulse combustion of said combustible gaseous mixture to provide combustion gases, and exhaust means for self-exhausting combustion gases from said apparatus, said primary burner being operable connected to said main burner to flow combustion gases from the primary burner into the main burner, each of said burners being separately operable after start-up to provide self-sustaining pulse combustion of said combustible gaseous mixture, said burner means also being simultaneously operable with said combustion chamber means and exhaust means cooperating to provide resonant explosive combustion cycles and gas pressure oscillations in each of said burners at substantially the same frequency for self-feeding said combustible gaseous mixture and self-exhausting said combustion gases in accordance with said pressure oscillations.

Claim 12

A pulse combustion apparatus comprising a primary burner, a main burner, fuel supply means for self-feeding of a combustible gaseous mixture to each of said burners, combustion chamber means for pulse combustion of said combustible gaseous mixture to provide combustion gases, and exhaust means for self-exhausting combustion gases from said apparatus, said primary burner being operable connected to said main burner to flow combustion gases from the primary burner into the main burner, each of said burners being separately operable after start-up to provide self-sustaining pulse combustion of said combustible gaseous mixture, said burner means also being simultaneously operable with said combustion chamber means and exhaust means cooperating to provide resonant explosive combustion cycles and gas pressure oscillations in each of said burners at substantially the same frequency for self-feeding said combustible gaseous mixture and self-exhausting said combustion gases in accordance with said pressure oscillations.

Claim 13

An apparatus according to claim 10, wherein aid primary burner is arranged to start before said main burner to provide pressure oscillations for causing said fuel supply means to provide a flow of combustible gaseous mixture to said main burner during start-up of the main burner, and said primary burner is arranged to ignite said combustible gaseous mixture in said main burner by contact with combustion gases from said primary burner.

Claim 14

An apparatus according to claim 11, wherein said combustion chamber means includes a common chamber for combustion of combustible gaseous mixture supplied to each of said burners.

Claim 15

An apparatus according to claim 12, wherein each of said burners includes a mixer head for receiving combustible gaseous mixture from said fuel supply means, said primary mixer head includes an outlet opening into said main mixer head, and said main mixer head includes an outlet opening into said common chamber.

Claim 16

An ignition and a stabilizer system for a main pulse combustion burner comprising a primary pulse combustion burner operably connected to flow combustion gases from said primary burner into said main burner, fuel supply means for self-feeding a combustible gaseous mixture to said main burner in response to gas pressure oscillations, and combustion chamber means and exhaust means to provide resonant explosive combustion of said combustible gaseous mixture and gas pressure oscillations in each of said burners, said primary burner being arranged to start before said main burner to provide gas pressure oscillations for causing said fuel supply means to provide a flow of combustible gaseous mixture to said main burner during start-up and to ignite said combustible gaseous mixture in said main burner by contact with combustion gases from the primary burner, said primary burner having a smaller heating capacity than said main burner and thereby improving the reliability of ignition of the main burner.

Claim 17

An ignition and a stabilizer system for a main pulse combustion burner comprising a primary pulse combustion burner operably connected to flow combustion gases from said primary burner into said main burner, fuel supply means for self-feeding a combustible gaseous mixture to said main burner in response to gas pressure oscillations, and combustion chamber means and exhaust means to provide resonant explosive combustion of said combustible gaseous mixture and gas pressure oscillations in each of said burners, said primary burner being arranged to start before said main burner to provide gas pressure oscillations for causing said fuel supply means to provide a flow of combustible gaseous mixture to said main burner during start-up and to ignite said combustible gaseous mixture in said main burner by contact with combustion gases from the primary burner, said primary burner having a smaller heating capacity than said main burner and thereby improving the reliability of ignition of the main burner.

Claim 18

A system according to claim 14, wherein said primary burner is sized to have a primary fuel input rate and said main burner is sized to have a main fuel input rate, each of said burners being separately operable after start-up to provide self-sustaining pulse combustion of said combustible gaseous mixture at their respective fuel input rates, and said burners are simultaneously operable at a total fuel input rate greater than the sum of said primary and main fuel input rates.

Claim 19

A system according to claim 14, wherein said combustion chamber means includes a common chamber.

Claim 20

A system according to claim 16, wherein each of said primary and main burners includes a mixer head, and said primary burner mixer head includes an outlet opening into said main burner mixer head.

Claim 21

A system according to claim 17, wherein said main burner mixer head is a region of said common chamber.

Claim 22

A system according to claim 15, wherein said resonant explosive combustion and gas pressure oscillations occur in each of said burners at substantially the same frequency as determined by the frequency of operation of said primary burner.

Claim 23

A system according to claim 19, wherein said primary burner reduces frequency and pressure amplitude variations in said main burner during steady state operation as compared with a similarly sized burner not including a primary burner.

Claim 26

A method according to claim 21, including the steps of starting said main burner means by self-feeding combustible gaseous mixture into the main burner means in response to the pressure oscillations of said primary burner means and igniting the combustible gaseous mixture in said main burner means by contact with the combustion gases from said primary burner means.

Claim 27

A method according to claim 22, wherein said primary and main burner means include a common combustion chamber and separate mixer heads, step (b) includes self-feeding combustible gaseous mixture into each of said mixer heads, and step (d) includes flowing combustion gases from said primary mixer head into said main mixer head.

Claim 28

A method according to claim 22, wherein each of said primary and main burner means respectively includes a mixer head for receiving and beginning the combustion of combustible gaseous mixture to provide combustion gases, combustion chamber means for receiving combustion gases from the mixer head and completing the combustion thereof, and exhaust means for removing said combustion gases from said combustion chamber, and step (d) includes flowing combustion gases from said primary exhaust means into said main mixer head and venting combustion gases from said main exhaust means to the atmosphere.

Claim 29

A method according to claim 21, wherein said burner means respectively have primary and main fuel input rates, and step (b) includes self-feeding combustible gaseous mixture into said main burner means at a higher rate than the self-feeding of combustible gaseous mixture into said primary burner means.

Claim 30

A method according to claim 25, wherein said main burner means include valve means to regulate the flow of combustible gaseous mixture to said main burner means and the turndown ratio of the burner means, said turndown ratio of said burner means being larger than it would be in a similarly sized burner not including primary burner means.

Claim 31

A method according to claim 21, wherein step (c) includes operating said primary burner means at a preselected frequency which is followed by the main burner means whereby the primary burner means stabilizes the operation of the main burner means.

Claim 32

A method according to claim 22, wherein said primary burner means has a smaller heating capacity than said main burner means whereby the reliability of starting the main burner is improved.

Claim 33

A method according to claim 22, wherein the primary burner means is sized to have a primary fuel input rate and said main burner means is sized to have a main fuel input rate, and step (d) includes self-feeding said combustible gaseous mixture to said primary and main burner means at a total fuel input rate greater than the sum of said primary and main fuel input rates.

Claim 34

A pulse combustion apparatus wherein explosive combustion cycles provide gas pressure oscillations comprising a primary burner means operably connected to a main burner means to flow combustion gases from said primary to said main burner means, fuel supply means for self-feeding a combustible gaseous mixture to said burner means, combustion chamber means for pulse combustion of said combustible gaseous mixture to provide combustion gases, and exhaust means for self-exhausting said combustion gases from said apparatus, said combustion chamber means and exhaust means cooperating to provide resonant combustion of combustible gaseous mixtures in each of said burner means at substantially the same frequency of pressure oscillations for self-feeding said combustible gaseous mixture and self-exhausting said combustion gases in accordance with said pressure oscillations, said primary burner means cooperating with said fuel supply means to provide a flow of said combustible gaseous mixture to said main burner means during start-up of the main burner means and to ignite said combustible gaseous mixture in said main burner means during start-up, said combustion chamber means including a common chamber for combustion of combustible gaseous mixture supplied to each of said burner means.

Claim 35

A pulse combustion apparatus wherein explosive combustion cycles provide gas pressure oscillations comprising a primary burner means operably connected to a main burner means to flow combustion gases from said primary to said main burner means, fuel supply means for self-feeding a combustible gaseous mixture to said burner means, combustion chamber means for pulse combustion of said combustible gaseous mixture to provide combustion gases, and exhaust means for self-exhausting said combustion gases from said apparatus, said combustion chamber means and exhaust means cooperating to provide resonant combustion of combustible gaseous mixtures in each of said burner means at substantially the same frequency of pressure oscillations for self-feeding said combustible gaseous mixture and self-exhausting said combustion gases in accordance with said pressure oscillations, said primary burner means cooperating with said fuel supply means to provide a flow of said combustible gaseous mixture to said main burner means during start-up of the main burner means and to ignite said combustible gaseous mixture in said main burner means during start-up, said combustion chamber means including a common chamber for combustion of combustible gaseous mixture supplied to each of said burner means.

Claim 36

A pulse combustion apparatus comprising a primary burner, a main burner, fuel supply means for self-feeding of a combustible gaseous mixture to each of said burners, combustion chamber means for pulse combustion of said combustible gaseous mixture to provide combustion gases, and exhaust means for self-exhausting combustion gases from said apparatus, said primary burner being operably connected to said main burner to flow combustion gases from the primary burner into the main burner, said combustion chamber means and exhaust means cooperating to provide resonant explosive combustion cycles and gas pressure oscillations in each of said burners at substantially the same frequency for self-feeding said combustible gaseous mixture and self-exhausting said combustion gases in accordance with said pressure oscillations, said primary burner being arranged to start before said main burner to provide pressure oscillations for causing said fuel supply means to provide a flow of combustible gaseous mixture to said main burner during start-up of the main burner, said primary burner also being arranged to ignite said combustible gaseous mixture in said main burner by contact with combustion gases from said primary burner, and said combustion means including a common chamber for combustion of combustible gaseous mixture supplied to each of said burners.

Claim 37

A pulse combustion apparatus comprising a primary burner, a main burner, fuel supply means for self-feeding of a combustible gaseous mixture to each of said burners, combustion chamber means for pulse combustion of said combustible gaseous mixture to provide combustion gases, and exhaust means for self-exhausting combustion gases from said apparatus, said primary burner being operably connected to said main burner to flow combustion gases from the primary burner into the main burner, said combustion chamber means and exhaust means cooperating to provide resonant explosive combustion cycles and gas pressure oscillations in each of said burners at substantially the same frequency for self-feeding said combustible gaseous mixture and self-exhausting said combustion gases in accordance with said pressure oscillations, said primary burner being arranged to start before said main burner to provide pressure oscillations for causing said fuel supply means to provide a flow of combustible gaseous mixture to said main burner during start-up of the main burner, said primary burner also being arranged to ignite said combustible gaseous mixture in said main burner by contact with combustion gases from said primary burner, and said combustion means including a common chamber for combustion of combustible gaseous mixture supplied to each of said burners.

Claim 38

An ignition and a stabilizer system for a main pulse combustion burner comprising a primary pulse combustion burner operably connected to flow combustion gases from said primary burner into said main burner, fuel supply means for self-feeding a combustible gaseous mixture to said main burner in response to gas pressure oscillations, and combustion chamber means and exhaust means to provide resonant explosive combustion of said combustible gaseous mixture and gas pressure oscillations in each of said burners, said primary burner being arranged to start before said main burner to provide gas pressure oscillations for causing said fuel supply means to provide a flow of combustible gaseous mixture to said main burner during start-up and to ignite said combustible gaseous mixture in said main burner by contact with combustion gases from the primary burner, said combustion chamber means including a common chamber. for combustion of combustible gaseous mixture supplied to each of said burners.

Claim 39

An ignition and a stabilizer system for a main pulse combustion burner comprising a primary pulse combustion burner operably connected to flow combustion gases from said primary burner into said main burner, fuel supply means for self-feeding a combustible gaseous mixture to said main burner in response to gas pressure oscillations, and combustion chamber means and exhaust means to provide resonant explosive combustion of said combustible gaseous mixture and gas pressure oscillations in each of said burners, said primary burner being arranged to start before said main burner to provide gas pressure oscillations for causing said fuel supply means to provide a flow of combustible gaseous mixture to said main burner during start-up and to ignite said combustible gaseous mixture in said main burner by contact with combustion gases from the primary burner, said combustion chamber means including a common chamber. for combustion of combustible gaseous mixture supplied to each of said burners.