FR823442A - Distributors and rectifiers for turbines and rotary compressors - Google Patents

Distributors and rectifiers for turbines and rotary compressors

Info

Publication number
FR823442A
FR823442A FR823442DA FR823442A FR 823442 A FR823442 A FR 823442A FR 823442D A FR823442D A FR 823442DA FR 823442 A FR823442 A FR 823442A
Authority
FR
France
Prior art keywords
rectifiers
distributors
turbines
rotary compressors
compressors
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
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.)
Rateau SA
Original Assignee
Rateau 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 Rateau SA filed Critical Rateau SA
Application granted granted Critical
Publication of FR823442A publication Critical patent/FR823442A/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
    • F01D9/044—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators permanently, e.g. by welding, brazing, casting or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR823442D 1936-10-02 1936-10-02 Distributors and rectifiers for turbines and rotary compressors Expired FR823442A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR823442T 1936-10-02

Publications (1)

Publication Number Publication Date
FR823442A true FR823442A (en) 1938-01-20

Family

ID=9281374

Family Applications (1)

Application Number Title Priority Date Filing Date
FR823442D Expired FR823442A (en) 1936-10-02 1936-10-02 Distributors and rectifiers for turbines and rotary compressors

Country Status (1)

Country Link
FR (1) FR823442A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE759514C (en) * 1940-04-10 1953-04-09 Aeg Blading produced by cutting a rolled profile for the guide wheels of turbines
DE906845C (en) * 1944-01-05 1954-03-18 Daimler Benz Ag Runner for axially flowed through turbomachines, especially for multi-stage axial compressors and axial turbines of aircraft engines or the like.
DE969599C (en) * 1943-05-27 1958-06-19 Holzwarth Gasturbinen G M B H Cooled nozzle body for centrifugal machines, especially exhaust gas turbines
US2856118A (en) * 1952-07-24 1958-10-14 Gen Motors Corp Blading assembly
DE1045591B (en) * 1951-02-27 1958-12-04 United Aircraft Corp Guide vane arrangement for multi-stage axial compressors
US2917276A (en) * 1955-02-28 1959-12-15 Orenda Engines Ltd Segmented stator ring assembly
US2924425A (en) * 1953-02-02 1960-02-09 Bristol Aero Engines Ltd Aerofoil-section bladed structures
US2959393A (en) * 1956-04-16 1960-11-08 Gen Electric Turbine bucket cover assembly
US3071346A (en) * 1960-06-21 1963-01-01 Wilgus S Broffitt Turbine nozzle
US3139265A (en) * 1960-01-28 1964-06-30 Nydqvist & Holm Ab Turbine and pump runner
FR2904033A1 (en) * 2006-07-19 2008-01-25 Snecma Sa Diffuser-synchronizing ring assembly for supplying air to annular combustion chamber in turbomachine e.g. jet engine or jet prop engine, has annular flanges and cylinders made of sheets to which blades are fixed by brazing

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE759514C (en) * 1940-04-10 1953-04-09 Aeg Blading produced by cutting a rolled profile for the guide wheels of turbines
DE969599C (en) * 1943-05-27 1958-06-19 Holzwarth Gasturbinen G M B H Cooled nozzle body for centrifugal machines, especially exhaust gas turbines
DE906845C (en) * 1944-01-05 1954-03-18 Daimler Benz Ag Runner for axially flowed through turbomachines, especially for multi-stage axial compressors and axial turbines of aircraft engines or the like.
DE1045591B (en) * 1951-02-27 1958-12-04 United Aircraft Corp Guide vane arrangement for multi-stage axial compressors
US2856118A (en) * 1952-07-24 1958-10-14 Gen Motors Corp Blading assembly
US2924425A (en) * 1953-02-02 1960-02-09 Bristol Aero Engines Ltd Aerofoil-section bladed structures
US2917276A (en) * 1955-02-28 1959-12-15 Orenda Engines Ltd Segmented stator ring assembly
US2959393A (en) * 1956-04-16 1960-11-08 Gen Electric Turbine bucket cover assembly
US3139265A (en) * 1960-01-28 1964-06-30 Nydqvist & Holm Ab Turbine and pump runner
US3071346A (en) * 1960-06-21 1963-01-01 Wilgus S Broffitt Turbine nozzle
FR2904033A1 (en) * 2006-07-19 2008-01-25 Snecma Sa Diffuser-synchronizing ring assembly for supplying air to annular combustion chamber in turbomachine e.g. jet engine or jet prop engine, has annular flanges and cylinders made of sheets to which blades are fixed by brazing
EP1882821A1 (en) * 2006-07-19 2008-01-30 Snecma Nozzle-synchronising ring assembly for a turbomachine
US7955051B2 (en) 2006-07-19 2011-06-07 Snecma Diffuser/guide vane assembly for a turbomachine

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