Combustion chamber, especially for gas turbines

Claim 2

A combustion chamber with an end-wall means having an axial inlet opening on an inlet side thereof, a first wall portion downstream of the end-wall means provided with secondary air inlet openings, means for supplying preheated combustion air into the combustion chamber, fuel injection means including a fuel injection nozzle disposed upstream of the inlet opening for injecting fuel into the preheated combustion air, first deflection means disposed essentially axially inside of the inlet opening for radially spreading out the fuel-air mixture flowing into the combustion chamber along the end-wall means, and second deflection means on the inside of the combustion chamber downstream of the first deflection means for forming an annular swirl so as to recombine the fuel-air mixture, characterized in that means are provided for mounting the first deflection means inside of the inlet opening so as to be axially adjustable with respect to the combustion chamber, and in that means are provided for supporting the injection nozzle so as to be axially adjustable with respect to the inlet opening of the combustion chamber.

Claim 3

A combustion chamber according to claim 1, characterized in that said means for mounting the first deflection means includes bar means for fixedly mounting the first deflection means at the supporting means, said bar means extend from the supporting means through the inlet opening to the first deflection means.

Claim 4

A combustion chamber according to claim 1, with an end-wall means having an axial inlet opening on the inlet side thereof, a first wall portion downstream of the end-wall means and provided with secondary air inlet openings, fuel injection means upstream of the inlet opening, means for supplying preheated combustion air, first deflection means disposed essentially axially inside of the inlet opening for radially spreading out the fuel-air mixture flowing into the combustion chamber along the end-wall means, and second deflection means on the inside of the combustion chamber downstream of the first deflection means for recombining the mixture in the sense of the formation of an annular swirl, characterized in that the end-wall means at the inlet side adjoins the inlet opening approximately hemispherically-shaped with a sphere diameter larger than a diametric dimension of the first wall portion, and in that a part of the combustion chamber adjoining the hemispherically-shaped end-wall means is reduced by way of a second wall portion approximately continuing the spherical shape to the adjacent first wall portion.

Claim 5

A combustion chamber according to claim 3, characterized in that the first deflection means is approximately mushroom-shaped and the first wall portion is substantially cylindrical.

Claim 6

A combustion chamber according to claim 4, characterized in that webs are distributed along a circumference of at least one of the first deflection means and an inner wall of the end-wall means.

Claim 7

A combustion chamber according to claim 1, characterized in that an edge of the inlet opening has a streamlined cross-sectional shape, and in that the fuel injection nozzle has a jet direction along generatrices of a cone approximately tangential to an inner edge of the inlet opening at a middle position of an axial adjustment of the first deflection means.

Claim 8

A combustion chamber according to claim 6, characterized in that the cross-sectional shape of the edge of the inlet opening is approximately drop-shaped.

Claim 9

A combustion chamber according to claim 1, characterized in that an end surface of the first deflection means facing an interior space of the combustion chamber has a concave configuration approximately matched to the a shape of the end-wall means.

Claim 10

A combustion chamber with an end-wall means having an axial inlet opening on an inlet side thereof, a first wall portion downstream of the end-wall means provided with secondary air inlet openings, means for supplying preheated combustion air into the combustion chamber, fuel injection means disposed upstream of the inlet opening for injecting fuel into the preheated combustion air, first deflection means disposed essentially axially inside of the inlet opening for radially spreading out the fuel-air mixture flowing into the combustion chamber along the end-wall means, and second deflection means on the inside of the combustion chamber downstream of the first deflection means for forming an annular swirl so as to recombine the fuel-air mixture, characterized in that means are provided for mounting the first deflection means inside of the inlet opening so as to be axially adjustable with respect to the combustion chamber, an edge of the inlet opening has a streamlined cross-sectional shape, the fuel injection means has a jet direction along generatrices of a cone approximately tangential to an inner edge of the inlet opening at a middle position of an axial adjustment of the first deflection means, and in that approximately radially extending webs are distributed along a circumference of at least one of the first deflection means and an inner wall of the end-wall means.

Claim 11

A combustion chamber with an end-wall means having an axial inlet opening on an inlet side thereof, a first wall portion downstream of the end-wall means provided with secondary air inlet openings, means for supplying preheated combustion air into the combustion chamber, fuel injection means disposed upstream of the inlet opening for injecting fuel into the preheated combustion air, first deflection means disposed essentially axially inside of the inlet opening for radially spreading out the fuel-air mixture flowing into the combustion chamber along the end-wall means, and second deflection means on the inside of the combustion chamber downstream of the first deflection means for forming an annular swirl so as to recombine the fuel-air mixture, characterized in that means are provided for mounting the first deflection means inside of the inlet opening so as to be axially adjustable with respect to the combustion chamber, an edge of the inlet opening has a streamlined cross-sectional shape, the fuel injection means has a jet direction along generatrices of a cone approximately tangential to an inner edge of the inlet opening at a middle position of an axial adjustment of the first deflection means, and in that approximately radially extending webs are distributed along a circumference of at least one of the first deflection means and an inner wall of the end-wall means.

Claim 12

A combustion chamber with an end-wall means having an axial inlet opening on an inlet side thereof, a first wall portion downstream of the end-wall means provided with secondary air inlet openings, means for supplying preheated combustion air into the combustion chamber, fuel injection means disposed upstream of the inlet opening for injecting fuel into the preheated combustion air, first deflection means disposed essentially axially inside of the inlet opening for radially spreading out the fuel-air mixture flowing into the combustion chamber along the end-wall means, and second deflection means on the inside of the combustion chamber downstream of the first deflection means for forming an annular swirl so as to recombine the fuel-air mixture, characterized in that means are provided for mounting the first deflection means inside of the inlet opening so as to be axially adjustable with respect to the combustion chamber, means are provided for supporting the fuel injection means so as to be axially adjustable with respect to the combustion chamber, said means for mounting the first deflection means includes a bar means for fixedly mounting the first deflection means at the supporting means, said bar means extend from the supporting means through the inlet opening to the first deflection means, an annular gap is formed between the end-wall means and the first deflection means, and in that at least one of the first deflection means and the end-wall means carry auxiliary webs projecting into said annular gap.

Claim 13

A combustion chamber with an end-wall means having an axial inlet opening on an inlet side thereof, a first wall portion downstream of the end-wall means provided with secondary air inlet openings, means for supplying preheated combustion air into the combustion chamber, fuel injection means disposed upstream of the inlet opening for injecting fuel into the preheated combustion air, first deflection means disposed essentially axially inside of the inlet opening for radially spreading out the fuel-air mixture flowing into the combustion chamber along the end-wall means, and second deflection means on the inside of the combustion chamber downstream of the first deflection means for forming an annular swirl so as to recombine the fuel-air mixture, characterized in that means are provided for mounting the first deflection means inside of the inlet opening so as to be axially adjustable with respect to the combustion chamber, means are provided for supporting the fuel injection means so as to be axially adjustable with respect to the combustion chamber, said means for mounting the first deflection means includes a bar means for fixedly mounting the first deflection means at the supporting means, said bar means extend from the supporting means through the inlet opening to the first deflection means, an annular gap is formed between the end-wall means and the first deflection means, and in that at least one of the first deflection means and the end-wall means carry auxiliary webs projecting into said annular gap.

Claim 14

A combustion chamber according to claim 10, characterized in that means are provided for controlling the axial position of the injection nozzle of the fuel injection means in dependence upon the operating conditions of the combustion chamber.

Claim 15

A combustion chamber according to claim 9, characterized in that the first deflection means is approximately mushroom-shaped and the first wall portion is substantially cylindrical.

Claim 16

A combustion chamber according to claim 10, characterized in that an end surface of the first deflection means facing an interior space of the combustion chamber has a concave configuration approximately matched to the a shape of the end-wall means.

Claim 17

A combustion chamber with an end-wall means having an axial inlet opening on an inlet side thereof, a first wall portion downstream of the end-wall means provided with secondary air inlet openings, means for supplying preheated combustion air into the combustion chamber, fuel injection means disposed upstream of the inlet opening for injecting fuel into the preheated combustion air, first deflection means disposed essentially axially inside of the inlet opening for radially spreading out the fuel-air mixture flowing into the combustion chamber along the end-wall means, and second deflection means on the inside of the combustion chamber downstream of the first deflection means for forming an annular swirl so as to recombine the fuel-air mixture, characterized in that means are provided for mounting the first deflection means inside of the inlet opening so as to be axially adjustable with respect to the combustion chamber, and in that approximately radially extending webs are distributed along a circumference of at least one of the first deflection means and an inner wall of the end-wall means.

Claim 18

A combustion chamber with an end-wall means having an axial inlet opening on an inlet side thereof, a first wall portion downstream of the end-wall means provided with secondary air inlet openings, means for supplying preheated combustion air into the combustion chamber, fuel injection means disposed upstream of the inlet opening for injecting fuel into the preheated combustion air, first deflection means disposed essentially axially inside of the inlet opening for radially spreading out the fuel-air mixture flowing into the combustion chamber along the end-wall means, and second deflection means on the inside of the combustion chamber downstream of the first deflection means for forming an annular swirl so as to recombine the fuel-air mixture, characterized in that means are provided for mounting the first deflection means inside of the inlet opening so as to be axially adjustable with respect to the combustion chamber, and in that approximately radially extending webs are distributed along a circumference of at least one of the first deflection means and an inner wall of the end-wall means.

Claim 19

A combustion chamber according to claim 3, characterized in that said means for mounting the first deflection means includes bar means for fixedly mounting the first deflection means at the supporting means, said bar means extend from the supporting means through the inlet opening to the first deflection means.

Claim 20

A combustion chamber with an end-wall means having an axial inlet opening on an inlet side thereof, a first wall portion downstream of the end-wall means provided with secondary air inlet openings, means for supplying preheated combustion air into the combustion chamber, fuel injection means disposed upstream of the inlet opening for injecting fuel into the preheated combustion air, first deflection means disposed essentially axially inside of the inlet opening for radially spreading out the fuel-air mixture flowing into the combustion chamber along the end-wall means, and second deflection means on the inside of the combustion chamber downstream of the first deflection means for forming an annular swirl so as to recombine the fuel-air mixture, characterized in that means are provided for mounting the first deflection means inside of the inlet opening so as to be axially adjustable with respect to the combustion chamber, means are provided for supporting the fuel injection means so as to be axially adjustable with respect to the combustion chamber, said means for mounting the first deflection means includes bar means for fixedly mounting the first deflection means at the supporting means, said bar means extend from the supporting means through the inlet opening to the first deflection means, an annular gap is formed between the end-wall means and the first deflection means, and in that at least one of the first deflection means and the end-wall means carry auxiliary webs projecting into said annular gap between the end-wall means and the first deflection means.

Claim 21

A combustion chamber with an end-wall means having an axial inlet opening on an inlet side thereof, a first wall portion downstream of the end-wall means provided with secondary air inlet openings, means for supplying preheated combustion air into the combustion chamber, fuel injection means disposed upstream of the inlet opening for injecting fuel into the preheated combustion air, first deflection means disposed essentially axially inside of the inlet opening for radially spreading out the fuel-air mixture flowing into the combustion chamber along the end-wall means, and second deflection means on the inside of the combustion chamber downstream of the first deflection means for forming an annular swirl so as to recombine the fuel-air mixture, characterized in that means are provided for mounting the first deflection means inside of the inlet opening so as to be axially adjustable with respect to the combustion chamber, means are provided for supporting the fuel injection means so as to be axially adjustable with respect to the combustion chamber, said means for mounting the first deflection means includes bar means for fixedly mounting the first deflection means at the supporting means, said bar means extend from the supporting means through the inlet opening to the first deflection means, an annular gap is formed between the end-wall means and the first deflection means, and in that at least one of the first deflection means and the end-wall means carry auxiliary webs projecting into said annular gap between the end-wall means and the first deflection means.

Claim 22

A combustion chamber according to claim 15, characterized in that means are provided for controlling an axial position of an injection nozzle of the fuel injection means in dependence upon the operating conditions of the combustion chamber.