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A rotor (20) for a compressor, in particular in a gas turbine, has a number of rotor blades (25) which are arranged around the rotation axis of the rotor (20) in the form of a rim and are each held in a circumferential recess (21) on the rotor (20) by a blade root (26), with the blade root (26) havi

A rotor (20) for a compressor, in particular in a gas turbine, has a number of rotor blades (25) which are arranged around the rotation axis of the rotor (20) in the form of a rim and are each held in a circumferential recess (21) on the rotor (20) by a blade root (26), with the blade root (26) having a widening lower part (27) which engages behind two shoulders (24) that are formed on the side walls of the recess (21). In such a rotor, the life is lengthened in that the recess depth (T) of the recess (21) is substantially greater than a minimum recess depth (Tmin) which results in the rotor (20) having sufficient strength in the area of the blade attachment for starting, based on the predetermined material characteristics of the rotor (20) and the operating conditions of the compressor.

대표청구항 ▼

What is claimed is: 1. A compressor with a rotor, said rotor having predetermined material characteristics and said compressor having predetermined operating conditions, said predetermined material characteristics and operating conditions defining a compressor-specific minimum recess depth for a ci

What is claimed is: 1. A compressor with a rotor, said rotor having predetermined material characteristics and said compressor having predetermined operating conditions, said predetermined material characteristics and operating conditions defining a compressor-specific minimum recess depth for a circumferential, rotor-blade-receiving recess in said rotor, such that the rotor has sufficient initial strength in the area of the blade attachment, said rotor comprising: a circumferential recess including side walls and two shoulders formed in said side walls, each shoulder having a shoulder depth; a plurality of rotor blades arranged as a rim around a rotation axis of the rotor, each blade including a blade root which holds the rotor blades in the rotor circumferential recess; wherein each blade root includes a widening lower part which engages behind the two shoulders of the side walls; wherein the depth of the recess is at least 10% greater than said compressor-specific minimum recess depth; and wherein the shoulder depth is sized to correspond to the recess depth, and wherein the rotor blade roots are sized to correspond to the recess depth. 2. The compressor as claimed in claim 1, wherein the recess depth is about 40% greater than said compressor-specific minimum recess depth. 3. The compressor as claimed in claim 2, further comprising: cutouts formed in each blade root to reduce weight, said cutouts each comprising rounded depressions adjacent an edge of each cutout, formed on a lower face of each blade root lower part, each cutout comprising a circumferential hole that passes through the blade root above the lower part. 4. The compressor as claimed in claim 1, further comprising: cutouts formed in each blade root to reduce weight, said cutouts each comprising rounded depressions adjacent an edge of each cutout, formed on a lower face of each blade root lower part, each cutout comprising a circumferential hole that passes through the blade root above the lower part.