EP 1910647 B1 20110907 - Method of mounting a securing element on a turbomachine rotor
Title (en)
Method of mounting a securing element on a turbomachine rotor
Title (de)
Verfahren zum Montieren eines Sicherungselements an einem Turbomaschinenrotor
Title (fr)
Procédé de montage d'un élément de sécurité sur un rotor de turbomachine
Publication
Application
Priority
- DE 2006001246 W 20060719
- DE 102005035901 A 20050730
Abstract (en)
[origin: DE102005035901A1] The unit has a plate-like base body (24) including a recess at its center, where the recess is formed between two end sections (26, 27) of the body. The recess defines a middle section of the body, which runs between the end sections. The middle section is flat and/or uncurved before the mounting of the securing unit at the rotor of the turbo-machine. The end sections have contact surfaces (29, 30) that run parallel to each other and face a rotor base body after the mounting of the securing unit. Independent claims are also included for the following: (1) a method of mounting a securing unit at a turbo-machine rotor for securing position of rotor blades in grooves of a rotor base body (2) a rotor of a turbo-machine e.g. gas turbine rotor, with securing units.
IPC 8 full level
F01D 5/30 (2006.01)
CPC (source: EP US)
F01D 5/3015 (2013.01 - EP US); F05D 2300/501 (2013.01 - EP US); Y10T 29/49316 (2015.01 - EP US); Y10T 29/49321 (2015.01 - EP US)
Designated contracting state (EPC)
DE ES FR GB IT
DOCDB simple family (publication)
DE 102005035901 A1 20070201; EP 1910647 A1 20080416; EP 1910647 B1 20110907; US 2009092497 A1 20090409; US 8128374 B2 20120306; WO 2007014543 A1 20070208
DOCDB simple family (application)
DE 102005035901 A 20050730; DE 2006001246 W 20060719; EP 06761823 A 20060719; US 98955206 A 20060719