Rotor blade ring of an axial flow turbomachine

Fluid reaction surfaces (i.e. – impellers) – Rotor having flow confining or deflecting web – shroud or... – Axially extending shroud ring or casing

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416190, 416196R, F01D 522

Patent

active

046995692

ABSTRACT:
In the rotor blade ring of an axial flow turbomachine, the rotor blades are each provided at their radially outer ends with a shroud plate and are fastened at their radially inner ends, by means of a root, in a corresponding groove of the machine rotor. The shroud plates are connected together in the peripheral direction by means of wires rolled into turned recesses. Grooves (10), with a clear width (w.sub.1) which is dimensioned larger than the width (w.sub.2) of the shroud plate turned recess (8) provided for the wire (7) to be rolled in, are machined in the end surface (6) of the shroud plate (2). A spacer means (11), surrounding the wire at least in the region of the rolling positions and removable after rolling, is laid in the grooves during the rolling procedure. This material is preferably a hard paper which is burnt to ashes during machine operation.

REFERENCES:
patent: 764450 (1904-07-01), Geisenhoner
patent: 1061648 (1913-05-01), Westinghouse
patent: 1165005 (1915-12-01), Herr
patent: 1542402 (1925-06-01), Meissner
patent: 2771267 (1956-11-01), Weymouth, Jr.
patent: 2846184 (1958-08-01), Tournere
patent: 3377050 (1968-04-01), Guy
patent: 3501247 (1970-03-01), Tournere
patent: 4268223 (1981-05-01), Anner et al.

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