Method and burner for combustion of waste air

Claim 3

In a method according to claim 1, delivering the waste air in the form of two annular jets which surround each other and the primary flame in a coaxial arrangement, and twisting the annular jets and the primary flame around the longitudinal median axis of the burner tube as they enter the combustion chamber, the twist given to the inner annular jet being opposite to the direction in which the primary flame and the other annular jet are twisted.

Claim 4

In a method according to claim 1, decomposing the jet of waste air which surrounds the primary flame into a large number of individual jet-rays.

Claim 5

A burner system for the thermal post-combustion of waste air from industrial plants, which comprises a combustion chamber, a burner system proper which opens into the combustion chamber, and supply pipes for the waaste air for post-combustion, through which pipes the waste air is conducted into the zone of the burner mouth inside the combustion chamber, which comprises means to produce a primary flame which explodes into a fan at the point where the burner opens into the combustion chamber, means for introducing the waste air into the combustion chamber approximately concentrically with and around the primary flame, and means for decomposing the jet of waste air which surrounds the primary flame into a large number of individual jet rays, having a burner tube for supplying the burner, a fuel supply pipe passing through the burner means, in which the means for introducing the waste air into the combustion chamber comprises annular tube means into which the waste air is delivered surrounding the burner tube, the means for producing a primary flame includes a waste-air spiral in the path of the waste air flowing through the annular tube means, and the means for decomposing the jet of waste air comprises waste oulets leading from the annular tube means toward the combustion chamber and at least one twisting apparatus adjacent the downstream end of the annular tube means by the air of which the waste air stream is twisted around the longitudinal median axis of the burner tube, and a twisting device located adjacent the downstream end of the burner tube by the aid of which the primary flame is twisted around the longitudinal axis of the burner tube.

Claim 6

A burner system for the thermal post-combustion of waste air from industrial plants, which comprises a combustion chamber, a burner system proper which opens into the combustion chamber, and supply pipes for the waaste air for post-combustion, through which pipes the waste air is conducted into the zone of the burner mouth inside the combustion chamber, which comprises means to produce a primary flame which explodes into a fan at the point where the burner opens into the combustion chamber, means for introducing the waste air into the combustion chamber approximately concentrically with and around the primary flame, and means for decomposing the jet of waste air which surrounds the primary flame into a large number of individual jet rays, having a burner tube for supplying the burner, a fuel supply pipe passing through the burner means, in which the means for introducing the waste air into the combustion chamber comprises annular tube means into which the waste air is delivered surrounding the burner tube, the means for producing a primary flame includes a waste-air spiral in the path of the waste air flowing through the annular tube means, and the means for decomposing the jet of waste air comprises waste oulets leading from the annular tube means toward the combustion chamber and at least one twisting apparatus adjacent the downstream end of the annular tube means by the air of which the waste air stream is twisted around the longitudinal median axis of the burner tube, and a twisting device located adjacent the downstream end of the burner tube by the aid of which the primary flame is twisted around the longitudinal axis of the burner tube.

Claim 7

In a burner system according to claim 4, the annular tube means comprising concentric annular tubes for the waste air stream and the twisting appartus includes means which twist waste air flowing in said concentric tubes in opposite directions.

Claim 8

In a burner system according to claim 4 the annular tube means having a tube portion which widens in funnel-fashion towards the outside, the twisting apparatus being located in said tube portion.

Claim 9

A burner system according to claim 4, wherein the portions of the individual tubes which extend into the combustion chamber have an inclined direction pointing towards the outside.

Claim 10

A burner system according to claim 4, wherein the annular tube means and waste air outlets project in relation to the twisting device downstreamward by an amount which corresponds approximately to between twice or three-times the diameter of the burner tube.

Claim 11

A burner system according to claim 4, wherein openings are provided connecting the annular space between the fuel supply pipe and the burner tube with the interior of the annular tube means through which primary air is admitted into the burner tube and means are provided for adjusting the flow-cross-section of the holes.

Claim 12

A burner system according to claim 9, wherein the holes are distributed over the axial length of the burner tube.

Claim 13

A burner system according to claim 9, wherein the passage holes are located adjacent the end of the burner tube which is further from the combustion chamber.

Claim 14

In a burner system according to claim 4, in which the means connecting the interior of the reservoir with the combustion chamber comprises annular tube means downstream from the inlet head of the waste-air spiral and joined thereto, the ratio between the widths of the inlet head and the annular tube means being approximately 2:1.

Claim 15

In a burner system according to claim 12, a funnel-shaped guide piece conducting the waste air from the inlet head into the annular tube means, said funnel-shaped guide piece extending at an inclination in relation to the burner tube and to the reservoir.

Claim 16

A burner system according to claim 4, for operation by gas, wherein the fuel supply pipe comprises a ring-cylinder tube provided at its mouth with an axially adjustable deflector disc which lies downstream from the tube mouth and deflects the gas stream discharged from the ring-cylinder tube axially towards the outside.

Claim 17

A Burner system according to claim 14, wherein the annular space between the burner tube and the fuel supply pipe through which the primary air stream passes is provided at its front section with a perforated plate which is located upstream from the deflector disc.

Claim 18

A burner system according to claim 4, wherein a perforated plate is provided in the burner tube and at least one twisting appartus is provided in the burner tube downstream from the perforated plate.

Claim 19

A burner system according to claim 16, wherein the twisting device lies upstream from the mouth of the fuel supply tube.

Claim 20

A burner system according to claim 4, wherein the ratio between the diameter of the individual tubes and the burner tube is between 1:10 and 1:25.

Claim 21

A burner system according to claim 4, wherein the individual tubes comprise tube sections which are inclined towards the longitudinal median axis of the burner tube at an angle between 150° and 40°, the tube sections being inserted into corresponding apertures in the front wall of the ring-cylindrical reservoir, and fixed to it by welding.

Claim 22

A burner system according to claim 19, wherein the tube sections towards the combustion chamber, their other ends being at least approximately in line with the front wall of the reservoir.

Claim 23

A burner system according to claim 19, wherein the tube sections into the interior of the reservoir and align at their other side at least approximately with the front wall thereof.

Claim 24

A burner system according to claim 4, wherein the individual tubes form an integral part with the front wall of the reservoir.

Claim 25

A burner system acording to claim 4, wherein the individual tubes are arranged in at least three concentric circles which are uniformly equidistant one from the others, the tubes on one of the circles, seen in the circumferential direction, being staggered in relation to those of the other circle by the same amount and the tube sections in each of the circles having identical lengths, the length of the tube in the innermost circle being shortest and the tube lengths increasing towards the outside.

Claim 26

A burner system according to claim 4, in which the individual tubes have a straight-line longitudinal axis.

Claim 27

A burner system according to claim 4, in which the individual tubes have a longitudinal axis curved arch-like.

Claim 28

A burner system according to claim 4, wherein the intake section of the individual tubes is funnel-shaped.

Claim 29

A burner system according to claim 4; wherein the wall which separates the reservoir from the combustion chamber and and incorporates the individual tubes is inclined to the longitudinal median axis of the tube at an angle between 15° and 40°.

Claim 30

A burner system according to claim 4, wherein the wall which separates the reservoir from the combustion chamber and contains the individual tubes is approximately at right angles to the longitudinal center line of the tube.

Claim 31

A burner system according to claim 4 designed as a plane-burner wherein the components serving for the conveyance of waste air and fuel extend over a relatively long distance across the axial length and have a prismatic shape.

Claim 32

A burner system according to claim 4, wherein the twisting apparatus and device comprise blade-shaped objects which are arranged at an angle with the radius around the longitudinal median axis of the burner tube.

Claim 33

A burner system according to claim 4, wherein the twisting apparatus and device are axially adjustable.

Claim 34

A burner system according to claim 4, having around the burner head a burner-stone which widens in the axial direction towards the combustion chamber into a funnel-shaped object and is formed a heat resistant material.

Claim 35

A burner system according to claim 32 wherein the burner-stone is mounted on the wall of the combustion chamber.

Claim 36

A burner system according to claim 4, having a control funnel surrounding the mouths of the burner tube and of the reservoir, which control funnel widens towards the combustion chamber.

Claim 37

A burner system according to claim 4, wherein a flame monitor means forms an inner unit together with ignition-electrodes, an outer unit being formed by the fuel supply pipes and the burner tube, and wherein the two units can be taken out independently of each other and individually after loosening corresponding flange connections.

Claim 38

A burner system according to claim 4, wherein the combustion chamber comprises a plurality of axially consecutive rings of a ceramics material, the last ring of the assembled unit, seen from the side of the burner, comprising a sighting window through which the interior of the combustion chamber can be inspected, and a discharge port for burnt-up waste gases, while the penultimate stone comprises an annular portion which projects towards the inside and acts as a stopping-blend.

Claim 39

A burner system according to claim 36 wherein the rings engage with one another on the principle of a tongue and groove assembly, axially projecting portions of one ring fitting into corresponding recesses in the adjacent ring.

Claim 40

A burner system according to claim 36, having a cylindrical chamber of metal and having a front wall at the burner side which is detachable.

Claim 41

A burner system according to claim 36, wherein the cross-section of the combustion chamber is suddenly increased at the point where the burner enters the chamber, and guidewalls are provided in the zone of the burner mouth which, diverging towards the outside, assist the explosion of the flame.

Claim 42

A burner system according to claim 4, comprising a by-pass unit by the aid of which waste air, delivered from the industrial plant, is at least partly directly conducted into the combustion chamber, a heat exchanger for preheating and means for by-passig the heating chamber, means to control the quantity of waste air which is admitted into the combustion chamber comprising a slider formed of two slider-plates which rest against each other and are movable in relation to each other, and contain holes which are staggered in relation to each other when the slider is in its initial position.

Claim 43

A burner system according to claim 40 wherein one of the slider plates is in a fixed position while the other is longitudinally adjustable on the first plate be a nut accommodating a stationary rotating threaded spindle driven by a reversible motor which is temperature dependent.

Claim 44

A burner system according to claim 40, wherein a spring pressed the two slider plates against each other.

Claim 45

A burner system according to claim 40, wherein the holes in the two slider plates are designed so that the flow cross-section can be gradually increased at a constant rate.

Claim 46

A burner system according to claim 4 comprising a heat-exchanger unit for the pre-heating of the waste air, which contains a number of tubes conducting the waste gases discharged from the combustion chamber, in a heat-exchanger casing, the waste air stream being sprayed over the tubes prior to entering the combustion chamber, the casing having a narrow and elongated form seen in the direction of flow, and resistance-elements on the inner wall surfaces of the casing to counteract the formation of split streams along the inner surface of the casing wall.

Claim 47

Burner system according to claim 4, in an oil operated system, in which the fuel supply means includes two jets for which are fed individually with fuel by a pump provided with a return lead, each jet being supplied through coordinated magnet valves which connect, or disconnect, the jets in dependence on the air temperature.

Claim 48

A burner system according to claim 4, wherein -- in oil operated systems -- a return jet is provided for the fuel supply, and both the supply pipe and the return pipe are controlled by an individual magnetic valve which operates in dependence on the air temperature, and which are controlled from a pump preferably provided with a return system.

Claim 49

A burner system according to claim 4, wherein the end of the burner tube which is opposite to the end at the combustion chamber is fixed to the adjacent portions of the casing-wall.

Claim 50

A burner system according to claim 4, wherein the end of the burner tube which is oposite to the end at the combustion chamber is flexibly supported at the adjacent portions of the casing wall, the zone of the burner tube at the end facing the combustion chamber is connected by means of ties with the parts of the casing wall which face the other end of the tube, the tube being supported against the parts of the casing which face the combustion chamber and the end of the burner tube facing the combustion chamber comprises a plane butting surface on a flange-like portion which accommodates an annular packing between itself and a corresponding surface on the casing wall which faces the combustion chamber.

Claim 51

A burner system according to claim 48, wherein the butting surface of the burner tube comprises at least one web-like projection which extends in the direction of the longitudinal center line and is pressed into the packing when the butting surface and its counter-surface are pressed together.

Claim 52

A burner system as claimed in claim 4, which includes a burner tube for supplying the burner, a fuel supply pipe passing through the burner tube, and a reservoir surrounding the burner tube, in which the means to produce a primary flame includes a waste-air spiral for delivering into the reservoir and means connecting the interior of the reservoir with the combustion chamber, and the means for decomposing the jet of waste air comprises a plurality of individual small diameter tubes which project from the front end of the reservoir into the combustion chamber.