CH360073A - Blade protection in turbo machines - Google Patents

Blade protection in turbo machines

Info

Publication number
CH360073A
CH360073A CH360073DA CH360073A CH 360073 A CH360073 A CH 360073A CH 360073D A CH360073D A CH 360073DA CH 360073 A CH360073 A CH 360073A
Authority
CH
Switzerland
Prior art keywords
blade protection
turbo machines
turbo
machines
blade
Prior art date
Application number
Other languages
German (de)
Inventor
Rosslyn Harris Frank
Arthur Boyle John
Original Assignee
Vickers Electrical Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Vickers Electrical Co Ltd filed Critical Vickers Electrical Co Ltd
Publication of CH360073A publication Critical patent/CH360073A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/32—Locking, e.g. by final locking blades or keys
    • F01D5/323—Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
CH360073D 1957-03-22 1958-03-19 Blade protection in turbo machines CH360073A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB360073X 1957-03-22

Publications (1)

Publication Number Publication Date
CH360073A true CH360073A (en) 1962-02-15

Family

ID=10383939

Family Applications (1)

Application Number Title Priority Date Filing Date
CH360073D CH360073A (en) 1957-03-22 1958-03-19 Blade protection in turbo machines

Country Status (2)

Country Link
CH (1) CH360073A (en)
GB (1) GB840820A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4465432A (en) * 1981-12-09 1984-08-14 S.N.E.C.M.A. System for mounting and attaching turbine and compressor prismatic rooted blades and mounting process
EP2617946A2 (en) 2012-01-23 2013-07-24 MTU Aero Engines GmbH System for pre-setting an installation position of rotor blades, securing element, rotor blade, turbo engine and method
US9169734B2 (en) 2013-02-22 2015-10-27 MTU Aero Engines AG System for specifying an installation position of rotor blades, securing element, rotor blade, turbomachine, and method

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2696035A1 (en) * 2012-08-09 2014-02-12 MTU Aero Engines GmbH Retention device for rotor blades of a fluid flow engine and corresponding assembly process
FR3158535B1 (en) * 2024-01-24 2025-12-05 Safran Aircraft Engines Multi-axial shim plate for turbomachine rotor, rotor and turbomachine assembly

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4465432A (en) * 1981-12-09 1984-08-14 S.N.E.C.M.A. System for mounting and attaching turbine and compressor prismatic rooted blades and mounting process
EP2617946A2 (en) 2012-01-23 2013-07-24 MTU Aero Engines GmbH System for pre-setting an installation position of rotor blades, securing element, rotor blade, turbo engine and method
DE102012200891A1 (en) 2012-01-23 2013-07-25 Mtu Aero Engines Gmbh System for specifying a mounting position of blades, securing element, blade, turbomachine and method
EP2617946A3 (en) * 2012-01-23 2017-07-26 MTU Aero Engines AG System for pre-setting an installation position of rotor blades, securing element, rotor blade, turbo engine and method
US9169734B2 (en) 2013-02-22 2015-10-27 MTU Aero Engines AG System for specifying an installation position of rotor blades, securing element, rotor blade, turbomachine, and method

Also Published As

Publication number Publication date
GB840820A (en) 1960-07-13

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