Combustion chamber

Claim 2

A combustion chamber, comprising a flame tube means forming a combustion zone, an evaporator means projecting into said combustion zone, said evaporator means being provided with a first evaporator channel means to which air and fuel are separately fed, and including deflection surface means arranged at an end of said first evaporator channel means, said deflection surface means being operable to deflect the fuel/air mixture to all sides in a direction generally opposite the main flow direction prevailing in said first evaporator channel means, characterized by an annular channel partly surrounding said first evaporator channel means, said annular channel being in communication with said first evaporator channel means in an immediate vicinity of the deflection surface means, a mixing zone located upstream of the combustion zone, as viewed in a main flow direction, said annular channel terminating in discharge aperture means for providing an essentially outwardly directed discharge from said annular channel into the mixing zone, said discharge aperture means extending radially outwardly at approximately a right angle to a longitudinal axis of the annular channel, said mixing zone being formed by an annular space between an outer wall of the evaporator means and an intermediate wall of the flame tube means and being traversed by air, and radially extending web means arranged in said annular space within a first and a second plane, the discharge aperture means of the annular channel terminating substantially between said web means.

Claim 3

A combustion chamber according to claim 1, characterized in that the deflection surface means is substantially axially symmetrical to the evaporator axis while said first evaporator channel means is substantially coaxial to the evaporator means.

Claim 4

A combustion chamber according to claim 2, characterized in that the discharge of said annular channel by way of said aperture means is generally radially outwardly directed approximately at a right angle.

Claim 5

A combustion chamber according to claim 3, characterized in that the mixing zone terminates funnel-shaped in the combustion zone so that walls delimiting the mixing zones and an outer annular channel of the annular channel are located essentially on cone surfaces.

Claim 6

A combustion chamber, comprising a flame tube means forming a combustion zone, an evaporator pipe means projecting into said combustion zone and provided with a first evaporator channel means to which air and fuel are separately fed, and including deflection surface means arranged at the end of said channel means, said deflection surface means being operable to deflect the fuel/air mixture in a direction generally opposite the main flow direction prevailing in said first evaporator channel means, characterized in that an annular channel means partly surrounds said first evaporator channel means, said annular channel means being in communication with a mixing zone located upstream of the combustion zone, as viewed in a main flow direction, by way of discharge aperture means extending generally radially outwardly approximately at a right angle so as to provide an essentially outwardly directed discharge, said mixing zone being formed by an annular space between a wall of the evaporator means and a wall of the flame tube means and being traversed by air, and radially extending web means arranged in said annular space within a first and a second plane, the discharge aperture means of the annular channel means terminating substantially between said web means, said deflection surface means deflects the air/fuel mixture substantially on all sides and is substantially axially symmetrical to the evaporator axis with said first evaporator channel means being substantially coaxial to the evaporator means, the mixing zone terminates funnel-shaped in the combustion zone so that walls delimiting the mixing zones and an outer annular channel of the annular channel means are located essentially on cone surfaces, and in that a throttling slide member is arranged directly ahead of the web means arranged in the first plane of the mixing zone.

Claim 7

A combustion chamber, comprising a flame tube means forming a combustion zone, an evaporator pipe means projecting into said combustion zone and provided with a first evaporator channel means to which air and fuel are separately fed, and including deflection surface means arranged at the end of said channel means, said deflection surface means being operable to deflect the fuel/air mixture in a direction generally opposite the main flow direction prevailing in said first evaporator channel means, characterized in that an annular channel means partly surrounds said first evaporator channel means, said annular channel means being in communication with a mixing zone located upstream of the combustion zone, as viewed in a main flow direction, by way of discharge aperture means extending generally radially outwardly approximately at a right angle so as to provide an essentially outwardly directed discharge, said mixing zone being formed by an annular space between a wall of the evaporator means and a wall of the flame tube means and being traversed by air, and radially extending web means arranged in said annular space within a first and a second plane, the discharge aperture means of the annular channel means terminating substantially between said web means, said deflection surface means deflects the air/fuel mixture substantially on all sides and is substantially axially symmetrical to the evaporator axis with said first evaporator channel means being substantially coaxial to the evaporator means, the mixing zone terminates funnel-shaped in the combustion zone so that walls delimiting the mixing zones and an outer annular channel of the annular channel means are located essentially on cone surfaces, and in that a throttling slide member is arranged directly ahead of the web means arranged in the first plane of the mixing zone.

Claim 8

A combustion chamber according to claim 5, characterized in that the web means arranged in the annular space are rounded off at their sides such that the webs disposed in a respective plane form therebetween nozzle-shaped openings.

Claim 9

A combustion chamber according to claim 6, characterized in that the web means arranged in the second plane are offset with respect to the web means arranged in the first plane and in that a discharge aperture means of the annular channel means terminates downstream of each web means arranged in the first plane.

Claim 10

A combustion chamber comprising a flame tube means forming a combustion zone, an evaporator means projecting into said combustion zone, said evaporator means being provided with a first evaporator channel means to which air and fuel are separately fed, and including deflection surface means arranged at the end of said first evaporator channel means and operable to deflect the fuel/air mixture in a direction generally opposite to the main flow direction prevailing in said first evaporator channel means, characterized in that an annular channel means partly surrounds said first evaporator channel means, said annular channel means being in communication with a mixing zone located upstream of the combustion zone, as viewed in a main flow direction, by way of discharge aperture means for providing an essentially outwardly directed discharge, said mixing zone being formed by an annular space between a wall of the evaporator means and a wall of the flame tube means and being traversed by air, and radially extending web means arranged in said annular space within a first and a second plane, the discharge aperture means of the annular channel means terminating substantially between said web means, and in that a throttling slide member is arranged directly ahead of the web means arranged in the first plane of the mixing zone.

Claim 11

A combustion chamber comprising a flame tube means forming a combustion zone, an evaporator means projecting into said combustion zone, said evaporator means being provided with a first evaporator channel means to which air and fuel are separately fed, and including deflection surface means arranged at the end of said first evaporator channel means and operable to deflect the fuel/air mixture in a direction generally opposite to the main flow direction prevailing in said first evaporator channel means, characterized in that an annular channel means partly surrounds said first evaporator channel means, said annular channel means being in communication with a mixing zone located upstream of the combustion zone, as viewed in a main flow direction, by way of discharge aperture means for providing an essentially outwardly directed discharge, said mixing zone being formed by an annular space between a wall of the evaporator means and a wall of the flame tube means and being traversed by air, and radially extending web means arranged in said annular space within a first and a second plane, the discharge aperture means of the annular channel means terminating substantially between said web means, and in that a throttling slide member is arranged directly ahead of the web means arranged in the first plane of the mixing zone.

Claim 12

A combustion chamber comprising a flame tube means forming a combustion zone, an evaporator means projecting into said combustion zone and provided with a first evaporator channel means to which air and fuel are separately fed, and including deflection surface means arranged at the end of said first evaporator channel means, said deflection surface means being operable to deflect the fuel/air mixture in a direction generally opposite the main flow direction prevailing in said first evaporator channel means, characterized in that an annular channel means partly surrounds said first evaporator channel means, said annular channel means being in communication with a mixing zone located upstream of the combustion zone, as viewed in a main flow direction, by way of discharge aperture means for providing an essentially outwardly directed discharge, said mixing zone being formed by an annular space between a wall of the evaporator means and a wall of the flame tube means and being traversed by air, and web means arranged in said annular space within a first and a second plane, the web means arranged in the annular space are rounded off at their sides such that the webs disposed in a respective plane form therebetween nozzle-shaped openings, and in that the discharge aperture means of the annular channel means terminates substantially between said web means.

Claim 13

A combustion chamber comprising a flame tube means forming a combustion zone, an evaporator means projecting into said combustion zone and provided with a first evaporator channel means to which air and fuel are separately fed, and including deflection surface means arranged at the end of said first evaporator channel means, said deflection surface means being operable to deflect the fuel/air mixture in a direction generally opposite the main flow direction prevailing in said first evaporator channel means, characterized in that an annular channel means partly surrounds said first evaporator channel means, said annular channel means being in communication with a mixing zone located upstream of the combustion zone, as viewed in a main flow direction, by way of discharge aperture means for providing an essentially outwardly directed discharge, said mixing zone being formed by an annular space between a wall of the evaporator means and a wall of the flame tube means and being traversed by air, and web means arranged in said annular space within a first and a second plane, the web means arranged in the annular space are rounded off at their sides such that the webs disposed in a respective plane form therebetween nozzle-shaped openings, and in that the discharge aperture means of the annular channel means terminates substantially between said web means.

Claim 14

A combustion chamber according to claim 9, characterized in that the web means arranged in the second plane are offset with respect to the web means arranged in the first plane and in that a discharge aperture means of the annular channel means terminates downstream of each web means arranged in the first plane.

Claim 15

A combustion chamber according to claim 9, characterized in that one web means arranged in the second plane is located downstream of a respective web means arranged in the first plane, and in that a discharge aperture means bordering two cooperating web means of the first and second plane terminates between said two web means.

Claim 16

A combustion chamber according to claim 1, characterized in that the evaporator means includes an evaporator body and evaporator pot, and in that the annular channel is formed by an outer wall of the evaporator body and the evaporator pot substantially coaxially surrounding the evaporator body, said evaporator pot including an essentially flat bottom having drawn up edges, said edges serving as said deflection surface means.

Claim 17

A combustion chamber comprising a flame tube means forming a combustion zone, an evaporator pipe means projecting into said combustion zone and provided with a first evaporator channel means to which air and fuel are separately fed, and including deflection surface means arranged at an end of said first evaporator channel means, said deflection surface means being operable to deflect the fuel/air mixture in a direction generally opposite the main flow direction prevailing in said first evaporator channel means, characterized in that the evaporator means includes an evaporator body and an evaporator pot, an annular channel means partly surrounds said first evaporator channel means, said annular channel means being in communication with a mixing zone located upstream of the combustion zone, as viewed in a main flow direction, by way of discharge aperture means for providing an essentially outwardly directed discharge, the annular channel means is formed by an outer wall of the evaporator body and the evaporator pot substantially coaxially surrounds the evaporator body, said evaporator pot includes an essentially flat bottom having drawn up edges, said edges serving as the deflection surface means, said mixing zone being formed by an annular space between the outer walls of the evaporator body and a wall of the flame tube means and being traversed by air, web means arranged in said annular space within a first and a second plane, the discharge aperture means of the annular channel means terminating substantially between said web means, and in that an outer surface of the evaporator pot is secured at webs arranged in the annular channel means and at web means arranged in the second plane of the mixing zone.

Claim 18

A combustion chamber comprising a flame tube means forming a combustion zone, an evaporator pipe means projecting into said combustion zone and provided with a first evaporator channel means to which air and fuel are separately fed, and including deflection surface means arranged at an end of said first evaporator channel means, said deflection surface means being operable to deflect the fuel/air mixture in a direction generally opposite the main flow direction prevailing in said first evaporator channel means, characterized in that the evaporator means includes an evaporator body and an evaporator pot, an annular channel means partly surrounds said first evaporator channel means, said annular channel means being in communication with a mixing zone located upstream of the combustion zone, as viewed in a main flow direction, by way of discharge aperture means for providing an essentially outwardly directed discharge, the annular channel means is formed by an outer wall of the evaporator body and the evaporator pot substantially coaxially surrounds the evaporator body, said evaporator pot includes an essentially flat bottom having drawn up edges, said edges serving as the deflection surface means, said mixing zone being formed by an annular space between the outer walls of the evaporator body and a wall of the flame tube means and being traversed by air, web means arranged in said annular space within a first and a second plane, the discharge aperture means of the annular channel means terminating substantially between said web means, and in that an outer surface of the evaporator pot is secured at webs arranged in the annular channel means and at web means arranged in the second plane of the mixing zone.

Claim 19

A combustion chamber according to claim 13, characterized in that the first channel means of the evaporator means has the configuration of a Venturi nozzle.

Claim 20

A combustion chamber according to claim 14, characterized in that an insert of highly porous material is arranged in the first channel means.

Claim 21

A combustion chamber comprising an ignition nozzle means, a flame tube means forming a combustion zone, an evaporator means projecting into said combustion zone and provided with a first evaporator channel means to which air and fuel are separately fed, and including deflection surface means arranged at an end of said first evaporator channel means, said deflection surface means being operable to deflect the fuel/air mixture in a direction generally opposite the main flow direction prevailing in said first evaporator channel means, characterized in that annular channel means partly surround said first evaporator channel means, said annular channel means being in communication with a mixing zone located upstream of the combustion zone, as viewed in a main flow direction, by way of discharge aperture means for providing an essentially outwardly directed discharge, said mixing zone being formed by an annular space between a wall of the evaporator means and a wall of the flame tube means and being traversed by air, and web means arranged in said annular space within a first and a second plane, the discharge aperture means of the annular channel means terminating substantially between said web means, and in that the evaporator means includes a coaxial channel means to which air is supplied and in which the ignition nozzle means is arranged with a radial spacing relative to inner walls of the coaxial channel means, and in that said coaxial channel means is substantially coaxially surrounded by an inner annular channel forming part of said first evaporator channel means to which air and fuel are separately fed and which leads to the deflection surface means which is adjoined substantially coaxially by said annular channel means forming an outer annular channel which is in communication with the mixing zone.

Claim 22

A combustion chamber comprising an ignition nozzle means, a flame tube means forming a combustion zone, an evaporator means projecting into said combustion zone and provided with a first evaporator channel means to which air and fuel are separately fed, and including deflection surface means arranged at an end of said first evaporator channel means, said deflection surface means being operable to deflect the fuel/air mixture in a direction generally opposite the main flow direction prevailing in said first evaporator channel means, characterized in that annular channel means partly surround said first evaporator channel means, said annular channel means being in communication with a mixing zone located upstream of the combustion zone, as viewed in a main flow direction, by way of discharge aperture means for providing an essentially outwardly directed discharge, said mixing zone being formed by an annular space between a wall of the evaporator means and a wall of the flame tube means and being traversed by air, and web means arranged in said annular space within a first and a second plane, the discharge aperture means of the annular channel means terminating substantially between said web means, and in that the evaporator means includes a coaxial channel means to which air is supplied and in which the ignition nozzle means is arranged with a radial spacing relative to inner walls of the coaxial channel means, and in that said coaxial channel means is substantially coaxially surrounded by an inner annular channel forming part of said first evaporator channel means to which air and fuel are separately fed and which leads to the deflection surface means which is adjoined substantially coaxially by said annular channel means forming an outer annular channel which is in communication with the mixing zone.

Claim 23

A combustion chamber according to claim 16, characterized in that further web means constructed as swirl surfaces are arranged in the inner annular channel within the area of the air inlet, while fuel is being fed into said inner annular channel downstream of said further web means.

Claim 24

A combustion chamber according to claim 17, characterized in that the fuel is fed to the inner surface by way of capillary bores.

Claim 25

A combustion chamber according to claim 17, characterized in that the fuel is fed to the inner annular channel by way of an annular groove surrounding the same, into which is inserted a ring of highly porous material.

Claim 26

A combustion chamber according to claim 16, characterized in that the web means arranged in the annular space are rounded off at their sides such that the webs disposed in a respective plane form therebetween nozzle-shaped openings.

Claim 27

A combustion chamber according to claim 20, characterized in that the web means arranged in the second plane are offset with respect to the web means arranged in the first plane and in that a discharge aperture means of the annular channel means terminates downstream of each web means arranged in the first plane.

Claim 28

A combustion chamber according to claim 20, characterized in that one web means arranged in the second plane is located downstream of a respective web means arranged in the first plane, and in that a discharge aperture means bordering two cooperating web means of the first and second plane terminates between said two web means.

Claim 29

A combustion chamber according to claim 16, characterized in that the mixing zone terminates funnel-shaped in the combustion zone so that the walls delimiting the mixing zones and the outer annular channel of the annular channel means are located essentially on cone surfaces.

Claim 30

A combustion chamber according to claim 1, characterized in that the first evaporator channel means has a configuration of a Venturi nozzle.

Claim 31

A combustion chamber according to claim 1, characterized in that an insert of a highly porous material is arranged in the first evaporator channel means.

Claim 32

A combustion chamber according to claim 3, characterized by secondary air openings provided in the flame tube means inclined obliquely inwardly to the combustion zone opposite the main flow direction.

Claim 33

A combustion chamber according to claim 26, characterized in that the evaporator means, the web means and the wall of a flame tube means defining in part the mixing zone form a structural unit which is retained in the flame tube means by way of connecting means distributed over the circumference under the formation of an annular gap.

Claim 34

A combustion chamber according to claim 27, characterized in that the evaporator means includes an evaporator body and evaporator pot, and in that the annular channel is formed by an outer wall of the evaporator body and the evaporator pot substantially coaxially surrounding the evaporator body, said evaporator pot including an essentially flat bottom having drawn up edges, said edges serving as said deflection surface means.

Claim 35

A combustion chamber according to claim 1, characterized in that the evaporator means, the web means and the wall of a flame tube means defining in part the mixing zone form a structural unit which is retained in the flame tube means by way of connecting means distributed over the circumference under a formation of an annular gap.

Claim 36

A combustion chamber according to claim 1, characterized by secondary air openings provided in the flame tube means inclined obliquely inwardly to the combustion zone opposite the main flow direction.