BE658332A - - Google Patents

Info

Publication number
BE658332A
BE658332A BE658332DA BE658332A BE 658332 A BE658332 A BE 658332A BE 658332D A BE658332D A BE 658332DA BE 658332 A BE658332 A BE 658332A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE658332A publication Critical patent/BE658332A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04Shutting-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
    • F01D21/045Shutting-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)
BE658332D 1964-01-15 1965-01-15 BE658332A (US08088918-20120103-C00476.png)

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
BE658332A true BE658332A (US08088918-20120103-C00476.png) 1965-04-30

Family

ID=23322518

Family Applications (1)

Application Number Title Priority Date Filing Date
BE658332D BE658332A (US08088918-20120103-C00476.png) 1964-01-15 1965-01-15

Country Status (8)

Country Link
US (1) US3243158A (US08088918-20120103-C00476.png)
BE (1) BE658332A (US08088918-20120103-C00476.png)
CH (1) CH460450A (US08088918-20120103-C00476.png)
DE (1) DE1476916B2 (US08088918-20120103-C00476.png)
FR (1) FR1435869A (US08088918-20120103-C00476.png)
GB (1) GB1093312A (US08088918-20120103-C00476.png)
NL (2) NL6500415A (US08088918-20120103-C00476.png)
SE (1) SE305775B (US08088918-20120103-C00476.png)

Families Citing this family (9)

* 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
FR2574476B1 (fr) * 1984-12-06 1987-01-02 Snecma Carter de retention pour soufflante de turboreacteur
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 (US08088918-20120103-C00476.png) * 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

Also Published As

Publication number Publication date
US3243158A (en) 1966-03-29
FR1435869A (fr) 1966-04-22
CH460450A (fr) 1968-07-31
DE1476916A1 (de) 1970-08-06
NL6500415A (US08088918-20120103-C00476.png) 1965-07-16
SE305775B (US08088918-20120103-C00476.png) 1968-11-04
NL134135C (US08088918-20120103-C00476.png)
DE1476916B2 (de) 1970-11-26
GB1093312A (en) 1967-11-29

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