FR1435869A - Improvement in turbine construction - Google Patents

Improvement in turbine construction

Info

Publication number
FR1435869A
FR1435869A FR1722A FR1722A FR1435869A FR 1435869 A FR1435869 A FR 1435869A FR 1722 A FR1722 A FR 1722A FR 1722 A FR1722 A FR 1722A FR 1435869 A FR1435869 A FR 1435869A
Authority
FR
France
Prior art keywords
improvement
turbine construction
turbine
construction
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
FR1722A
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.)
RTX Corp
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
Application granted granted Critical
Publication of FR1435869A publication Critical patent/FR1435869A/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
    • 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)
FR1722A 1964-01-15 1965-01-13 Improvement in turbine construction Expired FR1435869A (en)

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
FR1435869A true FR1435869A (en) 1966-04-22

Family

ID=23322518

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1722A Expired FR1435869A (en) 1964-01-15 1965-01-13 Improvement in turbine construction

Country Status (8)

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

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 (en) * 1979-03-30 1980-10-24 Snecma REMOVABLE SEALING COVER FOR TURBOJET BLOWER HOUSING
DE3019920C2 (en) * 1980-05-24 1982-12-30 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Device for the outer casing of the rotor blades of axial turbines for gas turbine engines
FR2574476B1 (en) * 1984-12-06 1987-01-02 Snecma RETENTION HOUSING FOR TURBOJET BLOWER
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 (en) * 1948-12-06 1951-03-12 Const Et D Equipements Mecaniq Further training in the construction of cylinders for gas turbines
BE543281A (en) * 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
BE658332A (en) 1965-04-30
NL6500415A (en) 1965-07-16
SE305775B (en) 1968-11-04
GB1093312A (en) 1967-11-29
NL134135C (en)
DE1476916A1 (en) 1970-08-06
DE1476916B2 (en) 1970-11-26
CH460450A (en) 1968-07-31
US3243158A (en) 1966-03-29

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