CH362269A - Leitapparat an einer Turbomaschine - Google Patents

Leitapparat an einer Turbomaschine

Info

Publication number
CH362269A
CH362269A CH362269DA CH362269A CH 362269 A CH362269 A CH 362269A CH 362269D A CH362269D A CH 362269DA CH 362269 A CH362269 A CH 362269A
Authority
CH
Switzerland
Prior art keywords
nozzle
turbo machine
turbo
machine
Prior art date
Application number
Other languages
English (en)
Inventor
Martin Fiori Bruno
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 CH362269A publication Critical patent/CH362269A/de

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

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)
CH362269D 1957-08-22 1958-08-22 Leitapparat an einer Turbomaschine CH362269A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US679623A US2984454A (en) 1957-08-22 1957-08-22 Stator units

Publications (1)

Publication Number Publication Date
CH362269A true CH362269A (de) 1962-05-31

Family

ID=24727658

Family Applications (1)

Application Number Title Priority Date Filing Date
CH362269D CH362269A (de) 1957-08-22 1958-08-22 Leitapparat an einer Turbomaschine

Country Status (7)

Country Link
US (1) US2984454A (de)
BE (1) BE570533A (de)
CH (1) CH362269A (de)
DE (1) DE1114364B (de)
FR (1) FR1211581A (de)
GB (1) GB893579A (de)
NL (2) NL99435C (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3243659A1 (de) * 1981-12-08 1983-07-21 United Technologies Corp., 06101 Hartford, Conn. Austrittsgehaeusebaugruppe fuer ein axialgasturbinentriebwerk

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3062499A (en) * 1960-05-18 1962-11-06 United Aircraft Corp Vane mounting and seal
US3075744A (en) * 1960-08-16 1963-01-29 United Aircraft Corp Turbine nozzle vane mounting means
GB1086432A (en) * 1965-09-21 1967-10-11 Bristol Siddeley Engines Ltd Gas turbine engines
US3423071A (en) * 1967-07-17 1969-01-21 United Aircraft Corp Turbine vane retention
US3511577A (en) * 1968-04-10 1970-05-12 Caterpillar Tractor Co Turbine nozzle construction
US3730640A (en) * 1971-06-28 1973-05-01 United Aircraft Corp Seal ring for gas turbine
US4425078A (en) * 1980-07-18 1984-01-10 United Technologies Corporation Axial flexible radially stiff retaining ring for sealing in a gas turbine engine
US4512712A (en) * 1983-08-01 1985-04-23 United Technologies Corporation Turbine stator assembly
GB2151709B (en) * 1983-12-19 1988-07-27 Gen Electric Improvements in gas turbine engines
US4720236A (en) * 1984-12-21 1988-01-19 United Technologies Corporation Coolable stator assembly for a gas turbine engine
FR2624913B1 (fr) * 1987-12-16 1990-04-20 Snecma Dispositif de fixation a vis d'une piece de revolution sur une bride annulaire de turbomachine
US5411370A (en) * 1994-08-01 1995-05-02 United Technologies Corporation Vibration damping shroud for a turbomachine vane
DE10133393B4 (de) 2001-07-13 2007-08-30 TransMIT Gesellschaft für Technologietransfer mbH Röhrchen mit Innendurchmessern im Nanometerbereich
US6884029B2 (en) * 2002-09-26 2005-04-26 Siemens Westinghouse Power Corporation Heat-tolerated vortex-disrupting fluid guide component
US7527469B2 (en) * 2004-12-10 2009-05-05 Siemens Energy, Inc. Transition-to-turbine seal apparatus and kit for transition/turbine junction of a gas turbine engine
US9963989B2 (en) * 2013-06-12 2018-05-08 United Technologies Corporation Gas turbine engine vane-to-transition duct seal

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB589542A (en) * 1941-09-22 1947-06-24 Karl Baumann Improvements in internal combustion turbines
BE471940A (de) * 1946-03-20
BE487120A (de) * 1946-03-25
FR964211A (de) * 1947-04-03 1950-08-08
FR965713A (de) * 1947-05-07 1950-09-20
US2654566A (en) * 1950-02-11 1953-10-06 A V Roe Canada Ltd Turbine nozzle guide vane construction
GB741138A (en) * 1952-10-03 1955-11-30 Vickers Electrical Co Ltd Improvements relating to gas turbines
US2942844A (en) * 1952-12-22 1960-06-28 Gen Motors Corp Turbine nozzle
BE529252A (de) * 1953-06-01

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3243659A1 (de) * 1981-12-08 1983-07-21 United Technologies Corp., 06101 Hartford, Conn. Austrittsgehaeusebaugruppe fuer ein axialgasturbinentriebwerk
DE3243659C2 (de) * 1981-12-08 1992-01-30 United Technologies Corp., Hartford, Conn., Us

Also Published As

Publication number Publication date
DE1114364B (de) 1961-09-28
FR1211581A (fr) 1960-03-17
NL99435C (de)
BE570533A (de)
NL230456A (de)
US2984454A (en) 1961-05-16
GB893579A (en) 1962-04-11

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