GB1213408A - Improvements in lock for turbomachinery blades - Google Patents

Improvements in lock for turbomachinery blades

Info

Publication number
GB1213408A
GB1213408A GB26294/68A GB2629468A GB1213408A GB 1213408 A GB1213408 A GB 1213408A GB 26294/68 A GB26294/68 A GB 26294/68A GB 2629468 A GB2629468 A GB 2629468A GB 1213408 A GB1213408 A GB 1213408A
Authority
GB
United Kingdom
Prior art keywords
root
spacer
engaging
blade
retainer
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
GB26294/68A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB1213408A publication Critical patent/GB1213408A/en
Expired legal-status Critical Current

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB26294/68A 1967-09-21 1968-05-31 Improvements in lock for turbomachinery blades Expired GB1213408A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US669454A US3395891A (en) 1967-09-21 1967-09-21 Lock for turbomachinery blades

Publications (1)

Publication Number Publication Date
GB1213408A true GB1213408A (en) 1970-11-25

Family

ID=24686376

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26294/68A Expired GB1213408A (en) 1967-09-21 1968-05-31 Improvements in lock for turbomachinery blades

Country Status (5)

Country Link
US (1) US3395891A (enrdf_load_stackoverflow)
BE (1) BE716192A (enrdf_load_stackoverflow)
FR (1) FR1570396A (enrdf_load_stackoverflow)
GB (1) GB1213408A (enrdf_load_stackoverflow)
SE (1) SE326790B (enrdf_load_stackoverflow)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2300677A (en) * 1995-05-06 1996-11-13 Mtu Muenchen Gmbh Bearing plates for heads of axial rivets securing turbine blades to a rotor disc
US5749706A (en) * 1996-01-31 1998-05-12 Mtu Motoren- Und Turbinen-Union Muenchen Gmbh Turbine blade wheel assembly with rotor blades fixed to the rotor wheel by rivets
GB2408296A (en) * 2003-11-22 2005-05-25 Rolls Royce Plc Compressor blade root retainer with integral sealing means to reduce axial leakage
GB2410531A (en) * 2004-01-29 2005-08-03 Rolls Royce Plc Screw tightened fan blade locking lever
RU2324821C2 (ru) * 2005-01-27 2008-05-20 Снекма Устройство позиционирования лопатки и диск с лопатками, содержащий такое устройство, и турбореактивный двигатель
US20140301853A1 (en) * 2013-04-09 2014-10-09 MTU Aero Engines AG Securing blade assortment

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3572970A (en) * 1969-01-23 1971-03-30 Gen Electric Turbomachinery blade spacer
US3653781A (en) * 1970-12-18 1972-04-04 Gen Electric Turbomachinery blade retainer
DE2155344A1 (de) * 1971-11-08 1973-05-17 Motoren Turbinen Union Integrales turbinenrad mit offenen axialen durchbruechen am aeusseren kranz und kontrollierten kranzrissen
BE794573A (fr) * 1972-02-02 1973-05-16 Gen Electric Dispositif de fixation d'aubes
US3832092A (en) * 1973-10-19 1974-08-27 Gen Electric Device for locking turbomachinery blades
US3936234A (en) * 1975-02-10 1976-02-03 General Electric Company Device for locking turbomachinery blades
US4279572A (en) * 1979-07-09 1981-07-21 United Technologies Corporation Sideplates for rotor disk and rotor blades
FR2507679A1 (fr) * 1981-06-12 1982-12-17 Snecma Dispositif de verrouillage d'une aube de rotor de turbomachine
US4451205A (en) * 1982-02-22 1984-05-29 United Technologies Corporation Rotor blade assembly
FR2535794A1 (fr) * 1982-11-08 1984-05-11 Snecma Dispositif de retenue axiale et radiale d'aubes de soufflante
US4477226A (en) * 1983-05-09 1984-10-16 General Electric Company Balance for rotating member
US4505640A (en) * 1983-12-13 1985-03-19 United Technologies Corporation Seal means for a blade attachment slot of a rotor assembly
US4595340A (en) * 1984-07-30 1986-06-17 General Electric Company Gas turbine bladed disk assembly
US4778342A (en) * 1985-07-24 1988-10-18 Imo Delaval, Inc. Turbine blade retainer
US4797065A (en) * 1986-10-17 1989-01-10 Transamerica Delaval Inc. Turbine blade retainer
US5993160A (en) * 1997-12-11 1999-11-30 Pratt & Whitney Canada Inc. Cover plate for gas turbine rotor
US5984639A (en) * 1998-07-09 1999-11-16 Pratt & Whitney Canada Inc. Blade retention apparatus for gas turbine rotor
US6582195B2 (en) * 2001-06-27 2003-06-24 General Electric Company Compressor rotor blade spacer apparatus
US7264448B2 (en) * 2004-10-06 2007-09-04 Siemens Power Corporation, Inc. Remotely accessible locking system for turbine blades
US8708652B2 (en) * 2007-06-27 2014-04-29 United Technologies Corporation Cover plate for turbine rotor having enclosed pump for cooling air
FR2945329B1 (fr) * 2009-05-06 2011-06-03 Snecma Rotor de soufflante d'un turboracteur d'avion
US8439635B2 (en) * 2009-05-11 2013-05-14 Rolls-Royce Corporation Apparatus and method for locking a composite component
US8979502B2 (en) 2011-12-15 2015-03-17 Pratt & Whitney Canada Corp. Turbine rotor retaining system
US9840922B2 (en) * 2014-03-07 2017-12-12 United Technologies Corporation Fan blade spacer
GB201516657D0 (en) 2015-09-21 2015-11-04 Rolls Royce Plc Seal-plate anti-rotation in a stage of a gas turbine engine
CN106015093B (zh) * 2016-07-13 2018-06-29 上海电气燃气轮机有限公司 一种压气机动叶轮盘的锁紧结构

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2801074A (en) * 1952-10-01 1957-07-30 United Aircraft Corp Blade retaining means
US2971744A (en) * 1956-11-27 1961-02-14 Szydlowski Joseph Blade lock
US3076634A (en) * 1959-06-12 1963-02-05 Ass Elect Ind Locking means for compressor and turbine blades
US3057598A (en) * 1960-07-01 1962-10-09 Ass Elect Ind Locking means for turbine or compressor blading

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2300677A (en) * 1995-05-06 1996-11-13 Mtu Muenchen Gmbh Bearing plates for heads of axial rivets securing turbine blades to a rotor disc
US5727927A (en) * 1995-05-06 1998-03-17 Mtu Motoren- Und Turbinen-Union Muenchen Gmbh Device for securing rotor blades to a rotor, especially of a gas turbine propulsion plant
GB2300677B (en) * 1995-05-06 1999-11-24 Mtu Muenchen Gmbh A turbine rotor
US5749706A (en) * 1996-01-31 1998-05-12 Mtu Motoren- Und Turbinen-Union Muenchen Gmbh Turbine blade wheel assembly with rotor blades fixed to the rotor wheel by rivets
GB2408296A (en) * 2003-11-22 2005-05-25 Rolls Royce Plc Compressor blade root retainer with integral sealing means to reduce axial leakage
GB2410531A (en) * 2004-01-29 2005-08-03 Rolls Royce Plc Screw tightened fan blade locking lever
GB2410531B (en) * 2004-01-29 2006-03-01 Rolls Royce Plc Fan blade disk assembly
US7153103B2 (en) 2004-01-29 2006-12-26 Rolls-Royce Plc Fan blade and disk assembly
RU2324821C2 (ru) * 2005-01-27 2008-05-20 Снекма Устройство позиционирования лопатки и диск с лопатками, содержащий такое устройство, и турбореактивный двигатель
US20140301853A1 (en) * 2013-04-09 2014-10-09 MTU Aero Engines AG Securing blade assortment
US9695699B2 (en) * 2013-04-09 2017-07-04 MTU Aero Engines AG Securing blade assortment

Also Published As

Publication number Publication date
US3395891A (en) 1968-08-06
SE326790B (enrdf_load_stackoverflow) 1970-08-03
FR1570396A (enrdf_load_stackoverflow) 1969-06-06
BE716192A (enrdf_load_stackoverflow) 1968-11-04

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Legal Events

Date Code Title Description
CSNS Application of which complete specification have been accepted and published, but patent is not sealed