초록

A lower cost combustor is formed from a series of sheets of metal that are secured by mechanical fasteners. An increase in diameter of the combustor is achieved through the provision of securing rings to which the sheets of metal are secured.

대표청구항 ▼

1. A combustor for a turbine engine, the combustor having: an outer wall extending about a combustor axis,an inner wall coaxially arranged with the outer wall,and at least one ring shaped support;wherein the ring shaped support extends in a generally radial direction and has, a radially inner array

1. A combustor for a turbine engine, the combustor having: an outer wall extending about a combustor axis,an inner wall coaxially arranged with the outer wall,and at least one ring shaped support;wherein the ring shaped support extends in a generally radial direction and has, a radially inner array of apertures, the radially inner array extending circumferentially about the axis, and a radially outer array of apertures, the radially outer array extending circumferentially about the axis;the outer wall being secured to the ring shaped support using tabs extending through the radially outer array of apertures,the inner wall being secured to the ring shaped support using tabs extending through the radially inner array of apertures. 2. A combustor according to claim 1, wherein each axial length is formed from a sheet of material with mechanical fastening means along its longitudinal edges which engage such that the sheet forms a tube. 3. A combustor according to claim 2, wherein the mechanical fastening means along the longitudinal edges are tabs engaging apertures. 4. A combustor according to claim 1, wherein each axial length is formed from a plurality of sheets of material which have mechanical fastener means along their axially extending edges which engage mechanical fastening means on an axially extending edge of an adjacent sheet such that the plurality of sheets form a tube. 5. A combustor according to claim 4, wherein the mechanical fastener means are tabs and the mechanical fastening means are apertures. 6. A combustor for a turbine engine, the combustor having: an outer wall extending about a combustor axis, andat least one ring shaped support;wherein the ring shaped support extends in a generally radial direction and has, a radially inner array of apertures, the radially inner array extending circumferentially about the axis, and a radially outer array of apertures, the radially outer array extending circumferentially about the axis;the outer wall having two cylindrical portions, a first cylindrical portion being secured to a first side of the ring shapes support by a plurality of tabs extending through the radially inner array of apertures, and a second cylindrical portion being secured to a side of the ring shaped support opposite the first side by a plurality of tabs extending through the radially outer array of apertures. 7. A combustor for a turbine engine according to claim 6, wherein each cylindrical portion is formed from a sheet of material with mechanical fastening means along its longitudinal edges which engage to provide the cylindrical portion. 8. A combustor according to claim 7, wherein the mechanical fastening means along the longitudinal edges are tabs engaging apertures. 9. A combustor according to claim 6 which further comprises: an inner wall extending about the combustor axis, andan inner-wall ring shaped support which extends in a generally radial direction and has a radially inner array of apertures, the radially inner array extending circumferentially about the axis, and a radially outer array of apertures, the radially outer array extending circumferentially about the axis;the inner wall having two cylindrical portions, a first cylindrical portion being secured to a first side of the ring shapes support by a plurality of tabs extending through the radially inner array of apertures, and a second cylindrical portion being secured to a side of the ring shaped support opposite the first side by a plurality of tabs extending through the radially outer array of apertures. 10. A combustor according to claim 9, wherein a combustion volume in which fuel is combusted is defined between the outer wall and the inner wall.