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FR1330656A - Cover belt vane, for turbines or compressors - Google Patents

Cover belt vane, for turbines or compressors

Info

Publication number
FR1330656A
FR1330656A FR906430A FR906430A FR1330656A FR 1330656 A FR1330656 A FR 1330656A FR 906430 A FR906430 A FR 906430A FR 906430 A FR906430 A FR 906430A FR 1330656 A FR1330656 A FR 1330656A
Authority
FR
France
Prior art keywords
compressors
turbines
cover belt
vane
belt vane
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
FR906430A
Other languages
French (fr)
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.)
BBC Brown Boveri AG Germany
BBC Brown Boveri France SA
Original Assignee
Brown Boveri und Cie AG Germany
BBC Brown Boveri France SA
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 Brown Boveri und Cie AG Germany, BBC Brown Boveri France SA filed Critical Brown Boveri und Cie AG Germany
Priority to FR906430A priority Critical patent/FR1330656A/en
Application granted granted Critical
Publication of FR1330656A publication Critical patent/FR1330656A/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
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR906430A 1962-08-08 1962-08-08 Cover belt vane, for turbines or compressors Expired FR1330656A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR906430A FR1330656A (en) 1962-08-08 1962-08-08 Cover belt vane, for turbines or compressors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR906430A FR1330656A (en) 1962-08-08 1962-08-08 Cover belt vane, for turbines or compressors

Publications (1)

Publication Number Publication Date
FR1330656A true FR1330656A (en) 1963-06-21

Family

ID=8784843

Family Applications (1)

Application Number Title Priority Date Filing Date
FR906430A Expired FR1330656A (en) 1962-08-08 1962-08-08 Cover belt vane, for turbines or compressors

Country Status (1)

Country Link
FR (1) FR1330656A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3850546A (en) * 1971-03-03 1974-11-26 Gen Motors Corp Turbomachine rotor
US4688988A (en) * 1984-12-17 1987-08-25 United Technologies Corporation Coolable stator assembly for a gas turbine engine
EP1408199A1 (en) * 2002-10-08 2004-04-14 United Technologies Corporation Leak resistant vane cluster
EP1510654A1 (en) * 2003-08-25 2005-03-02 Siemens Aktiengesellschaft Unitary turbine blade array and method to produce the unitary turbine blade array.
EP1870562A2 (en) * 2006-06-23 2007-12-26 Snecma Compressor synchronising ring sector or turbomachine nozzle guide vane sector
JP2010038161A (en) * 2008-08-01 2010-02-18 General Electric Co <Ge> Split doublet power nozzle and related method
FR2948737A1 (en) * 2009-07-31 2011-02-04 Snecma Outer shell sector forming assembly for bladed ring sector of turbine or compressor stator in turbojet engine of aircraft, has vibration-damping block supported against two friction surfaces respectively provided on two elementary sectors
EP2562355A3 (en) * 2011-08-23 2018-04-11 General Electric Company Coupled blade platforms and methods of sealing

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3850546A (en) * 1971-03-03 1974-11-26 Gen Motors Corp Turbomachine rotor
US4688988A (en) * 1984-12-17 1987-08-25 United Technologies Corporation Coolable stator assembly for a gas turbine engine
WO2004033871A3 (en) * 2002-10-08 2009-04-23 United Technologies Corp Leak resistant vane cluster
WO2004033871A2 (en) * 2002-10-08 2004-04-22 United Technologies Corporation Leak resistant vane cluster
US6910854B2 (en) 2002-10-08 2005-06-28 United Technologies Corporation Leak resistant vane cluster
EP1408199A1 (en) * 2002-10-08 2004-04-14 United Technologies Corporation Leak resistant vane cluster
EP1510654A1 (en) * 2003-08-25 2005-03-02 Siemens Aktiengesellschaft Unitary turbine blade array and method to produce the unitary turbine blade array.
EP1870562A2 (en) * 2006-06-23 2007-12-26 Snecma Compressor synchronising ring sector or turbomachine nozzle guide vane sector
FR2902843A1 (en) * 2006-06-23 2007-12-28 Snecma Sa COMPRESSOR RECTIFIER AREA OR TURBOMACHINE DISTRIBUTOR SECTOR
EP1870562A3 (en) * 2006-06-23 2008-04-02 Snecma Compressor synchronising ring sector or turbomachine nozzle guide vane sector
US7887286B2 (en) 2006-06-23 2011-02-15 Snecma Sector of a compressor guide vanes assembly or a sector of a turbomachine nozzle assembly
RU2445467C2 (en) * 2006-06-23 2012-03-20 Снекма Turbine unit stator sector, turbine unit compressor with said sector, turbine unit turbine and turbine unit
JP2010038161A (en) * 2008-08-01 2010-02-18 General Electric Co <Ge> Split doublet power nozzle and related method
FR2948737A1 (en) * 2009-07-31 2011-02-04 Snecma Outer shell sector forming assembly for bladed ring sector of turbine or compressor stator in turbojet engine of aircraft, has vibration-damping block supported against two friction surfaces respectively provided on two elementary sectors
EP2562355A3 (en) * 2011-08-23 2018-04-11 General Electric Company Coupled blade platforms and methods of sealing

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