GB660383A - Blade mounting for axial-flow compressors and the like - Google Patents

Blade mounting for axial-flow compressors and the like

Info

Publication number
GB660383A
GB660383A GB4925/49A GB492549A GB660383A GB 660383 A GB660383 A GB 660383A GB 4925/49 A GB4925/49 A GB 4925/49A GB 492549 A GB492549 A GB 492549A GB 660383 A GB660383 A GB 660383A
Authority
GB
United Kingdom
Prior art keywords
blade
roots
slots
axial
rings
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
GB4925/49A
Inventor
Winnett Boyd
George Easton Anderson
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.)
AV Roe Canada Ltd
Original Assignee
AV Roe Canada 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 AV Roe Canada Ltd filed Critical AV Roe Canada Ltd
Publication of GB660383A publication Critical patent/GB660383A/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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

660,383. Compressor and like blades. BOYD, W., ANDERSON, G. E., and ROE, CANADA, Ltd., A. V. Feb. 15, 1950 [Feb. 23, 1949], No. 4925/49. Class 110(iii) In an axial-flow compressor or the like in which the blade roots are mounted in slots in the blade-supporting members, a coating of a thermosetting plastic is applied to the registering faces of either the slots or roots, or to both slots and roots. The roots of the blade are then inserted in the slots and the supporting members and blades are subjected to heat until the plastic is cured. The plastic 19 may be organosilicon polymer and the thickness between 0.0005 inch and 0.005 inch. The blade roots 11 are of dovetail section and fit into correspondingly-shaped slots 16 in the blade ring 12. The blade rings are supported in the casing 13 by spacer rings 14 which are secured by bolts 15, the blade rings and spacer rings being suitably stepped.
GB4925/49A 1949-02-23 1949-02-23 Blade mounting for axial-flow compressors and the like Expired GB660383A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB311354X 1949-02-23

Publications (1)

Publication Number Publication Date
GB660383A true GB660383A (en) 1951-11-07

Family

ID=10318531

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4925/49A Expired GB660383A (en) 1949-02-23 1949-02-23 Blade mounting for axial-flow compressors and the like

Country Status (4)

Country Link
CH (1) CH311354A (en)
DE (1) DE888299C (en)
FR (1) FR1013114A (en)
GB (1) GB660383A (en)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2857093A (en) * 1954-12-02 1958-10-21 Cincinnati Testing & Res Lab Stator casing and blade assembly
US2914300A (en) * 1955-12-22 1959-11-24 Gen Electric Nozzle vane support for turbines
US2917276A (en) * 1955-02-28 1959-12-15 Orenda Engines Ltd Segmented stator ring assembly
US2933286A (en) * 1954-09-15 1960-04-19 Gen Electric Damping turbine buckets
US2995294A (en) * 1954-12-02 1961-08-08 Studebaker Packard Corp Stator casing and blade assembly
US2996996A (en) * 1958-01-20 1961-08-22 Sulzer Ag Radial diffuser for a radial turbomachine
US3004700A (en) * 1959-08-18 1961-10-17 Gen Electric Turbine engine casing
US3045964A (en) * 1957-02-14 1962-07-24 Stalker Corp Bladed wheels for compressors, turbines and the like
US3339833A (en) * 1963-12-04 1967-09-05 Rolls Royce Axial fluid flow machine such as a compressor or turbine
EP0017306A1 (en) * 1979-03-14 1980-10-15 Rolls-Royce Plc Stator vane assembly for a gas turbine engine
US4500255A (en) * 1981-04-24 1985-02-19 United States Of America As Represented By The Secretary Of The Air Force Spacer structure
US4840536A (en) * 1987-04-07 1989-06-20 Mtu Motoren-Und Turbinen-Union Muenchen Gmbh Axial guide blade assembly for a compressor stator
US4889470A (en) * 1988-08-01 1989-12-26 Westinghouse Electric Corp. Compressor diaphragm assembly
US4934900A (en) * 1989-07-31 1990-06-19 Fuller Company Assembly forming a cylindrical cage of spaced apart vanes
FR2702242A1 (en) * 1993-03-03 1994-09-09 Snecma Stage of free blades at one end.
JP2012510582A (en) * 2008-12-05 2012-05-10 シーメンス アクティエンゲゼルシャフト Guide vane array structure for axial turbomachinery

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3000552A (en) * 1957-05-28 1961-09-19 Gen Motors Corp Compressor vane mounting
GB1485032A (en) * 1974-08-23 1977-09-08 Rolls Royce Gas turbine engine casing
GB2115883B (en) * 1982-02-26 1986-04-30 Gen Electric Turbomachine airfoil mounting assembly
DE3341871A1 (en) * 1983-11-19 1985-05-30 Brown, Boveri & Cie Ag, 6800 Mannheim Axial compressor
FR2636378B1 (en) * 1988-09-14 1990-11-30 Snecma DUAL FLOW TURBOREACTOR BLOWER RECTIFIER
US5022818A (en) * 1989-02-21 1991-06-11 Westinghouse Electric Corp. Compressor diaphragm assembly
FR2680384B1 (en) * 1991-08-13 1995-03-10 Plastiremo BLADE CROWN WITH SIMPLIFIED MOUNTING AND BLADE FOR ITS REALIZATION.

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE735668C (en) * 1940-04-26 1943-05-21 Maschf Augsburg Nuernberg Ag Gas turbine wheel made of ceramic material

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2933286A (en) * 1954-09-15 1960-04-19 Gen Electric Damping turbine buckets
US2857093A (en) * 1954-12-02 1958-10-21 Cincinnati Testing & Res Lab Stator casing and blade assembly
US2995294A (en) * 1954-12-02 1961-08-08 Studebaker Packard Corp Stator casing and blade assembly
US2917276A (en) * 1955-02-28 1959-12-15 Orenda Engines Ltd Segmented stator ring assembly
US2914300A (en) * 1955-12-22 1959-11-24 Gen Electric Nozzle vane support for turbines
US3045964A (en) * 1957-02-14 1962-07-24 Stalker Corp Bladed wheels for compressors, turbines and the like
US2996996A (en) * 1958-01-20 1961-08-22 Sulzer Ag Radial diffuser for a radial turbomachine
US3004700A (en) * 1959-08-18 1961-10-17 Gen Electric Turbine engine casing
US3339833A (en) * 1963-12-04 1967-09-05 Rolls Royce Axial fluid flow machine such as a compressor or turbine
EP0017306A1 (en) * 1979-03-14 1980-10-15 Rolls-Royce Plc Stator vane assembly for a gas turbine engine
US4500255A (en) * 1981-04-24 1985-02-19 United States Of America As Represented By The Secretary Of The Air Force Spacer structure
US4840536A (en) * 1987-04-07 1989-06-20 Mtu Motoren-Und Turbinen-Union Muenchen Gmbh Axial guide blade assembly for a compressor stator
US4889470A (en) * 1988-08-01 1989-12-26 Westinghouse Electric Corp. Compressor diaphragm assembly
US4934900A (en) * 1989-07-31 1990-06-19 Fuller Company Assembly forming a cylindrical cage of spaced apart vanes
FR2702242A1 (en) * 1993-03-03 1994-09-09 Snecma Stage of free blades at one end.
EP0616110A1 (en) * 1993-03-03 1994-09-21 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Row of blades unsupported at one end
US5429479A (en) * 1993-03-03 1995-07-04 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Stage of vanes free at one extremity
JP2012510582A (en) * 2008-12-05 2012-05-10 シーメンス アクティエンゲゼルシャフト Guide vane array structure for axial turbomachinery

Also Published As

Publication number Publication date
FR1013114A (en) 1952-07-23
CH311354A (en) 1955-11-30
DE888299C (en) 1953-08-31

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