CH460450A - Turbine à gaz - Google Patents

Turbine à gaz

Info

Publication number
CH460450A
CH460450A CH53065A CH53065A CH460450A CH 460450 A CH460450 A CH 460450A CH 53065 A CH53065 A CH 53065A CH 53065 A CH53065 A CH 53065A CH 460450 A CH460450 A CH 460450A
Authority
CH
Switzerland
Prior art keywords
gas turbine
turbine
gas
Prior art date
Application number
CH53065A
Other languages
English (en)
Inventor
Maxon Desmond James
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of CH460450A publication Critical patent/CH460450A/fr

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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH53065A 1964-01-15 1965-01-14 Turbine à gaz CH460450A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US337905A US3243158A (en) 1964-01-15 1964-01-15 Turbine construction

Publications (1)

Publication Number Publication Date
CH460450A true CH460450A (fr) 1968-07-31

Family

ID=23322518

Family Applications (1)

Application Number Title Priority Date Filing Date
CH53065A CH460450A (fr) 1964-01-15 1965-01-14 Turbine à gaz

Country Status (8)

Country Link
US (1) US3243158A (fr)
BE (1) BE658332A (fr)
CH (1) CH460450A (fr)
DE (1) DE1476916B2 (fr)
FR (1) FR1435869A (fr)
GB (1) GB1093312A (fr)
NL (2) NL6500415A (fr)
SE (1) SE305775B (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2574476A1 (fr) * 1984-12-06 1986-06-13 Snecma Carter de retention pour soufflante de turboreacteur

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3295751A (en) * 1965-04-21 1967-01-03 United Aircraft Corp Compressor stator shroud arrangement
US3387820A (en) * 1965-05-24 1968-06-11 Continental Aviat & Engineerin Turbine engine construction
US3391904A (en) * 1966-11-02 1968-07-09 United Aircraft Corp Optimum response tip seal
US3428129A (en) * 1966-12-27 1969-02-18 Mobil Oil Corp Vertical fracture control
US3836279A (en) * 1973-02-23 1974-09-17 United Aircraft Corp Seal means for blade and shroud
FR2452601A1 (fr) * 1979-03-30 1980-10-24 Snecma Support amovible de revetement d'etancheite pour carter de soufflante de turboreacteur
DE3019920C2 (de) * 1980-05-24 1982-12-30 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur äußeren Ummantelung der Laufschaufeln von Axialturbinen für Gasturbinentriebwerke
US5395211A (en) * 1994-01-14 1995-03-07 United Technologies Corporation Stator structure for a rotary machine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR975879A (fr) * 1948-12-06 1951-03-12 Const Et D Equipements Mecaniq Perfectionnement dans la construction des cylindres pour turbines à gaz
BE543281A (fr) * 1954-12-16
GB868197A (en) * 1956-09-28 1961-05-17 Rolls Royce Improvements in or relating to protective arrangements for use with rotating parts
US2987296A (en) * 1957-12-02 1961-06-06 Bendix Corp Safety device for starter turbine
US3146992A (en) * 1962-12-10 1964-09-01 Gen Electric Turbine shroud support structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2574476A1 (fr) * 1984-12-06 1986-06-13 Snecma Carter de retention pour soufflante de turboreacteur
EP0184962A1 (fr) * 1984-12-06 1986-06-18 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Carter de rétention pour soufflante de turboréacteur

Also Published As

Publication number Publication date
GB1093312A (en) 1967-11-29
FR1435869A (fr) 1966-04-22
SE305775B (fr) 1968-11-04
DE1476916A1 (de) 1970-08-06
NL134135C (fr)
DE1476916B2 (de) 1970-11-26
BE658332A (fr) 1965-04-30
US3243158A (en) 1966-03-29
NL6500415A (fr) 1965-07-16

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