CA557093A - Dispositif de blocage de lame de rotor - Google Patents

Dispositif de blocage de lame de rotor

Info

Publication number
CA557093A
CA557093A CA557093A CA557093DA CA557093A CA 557093 A CA557093 A CA 557093A CA 557093 A CA557093 A CA 557093A CA 557093D A CA557093D A CA 557093DA CA 557093 A CA557093 A CA 557093A
Authority
CA
Canada
Prior art keywords
locking device
rotor blade
blade locking
rotor
locking
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA557093A
Other languages
English (en)
Inventor
Joseph T. Purvis
Robert M. Sachs
Original Assignee
AV Roe Canada Ltd
Publication date
Application granted granted Critical
Publication of CA557093A publication Critical patent/CA557093A/fr
Expired legal-status Critical Current

Links

CA557093A Dispositif de blocage de lame de rotor Expired CA557093A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA557093T

Publications (1)

Publication Number Publication Date
CA557093A true CA557093A (fr) 1958-05-06

Family

ID=35723499

Family Applications (1)

Application Number Title Priority Date Filing Date
CA557093A Expired CA557093A (fr) Dispositif de blocage de lame de rotor

Country Status (1)

Country Link
CA (1) CA557093A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5584659A (en) * 1994-08-29 1996-12-17 Mtu Motoren- Und Turbinen-Union Muenchen Gmbh Device for fixing turbine blades and for eliminating rotor balance errors in axially flow-through compressors or turbines of gas turbine drives

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5584659A (en) * 1994-08-29 1996-12-17 Mtu Motoren- Und Turbinen-Union Muenchen Gmbh Device for fixing turbine blades and for eliminating rotor balance errors in axially flow-through compressors or turbines of gas turbine drives

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