DE2054926B2 - Halterung eines turbinenleitkranzes - Google Patents

Halterung eines turbinenleitkranzes

Info

Publication number
DE2054926B2
DE2054926B2 DE19702054926 DE2054926A DE2054926B2 DE 2054926 B2 DE2054926 B2 DE 2054926B2 DE 19702054926 DE19702054926 DE 19702054926 DE 2054926 A DE2054926 A DE 2054926A DE 2054926 B2 DE2054926 B2 DE 2054926B2
Authority
DE
Germany
Prior art keywords
ring
turbine
guide
outer ring
gas
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.)
Pending
Application number
DE19702054926
Other languages
German (de)
English (en)
Other versions
DE2054926C (de
DE2054926A1 (enExample
Inventor
Klaus Dipl Ing 8000 München Trappmann
Original Assignee
Motoren und Turbinen Union München GmbH, 8000 München
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 Motoren und Turbinen Union München GmbH, 8000 München filed Critical Motoren und Turbinen Union München GmbH, 8000 München
Priority to DE19702054926 priority Critical patent/DE2054926B2/de
Priority to FR7046312A priority patent/FR2112872A5/fr
Priority to GB5138571A priority patent/GB1368770A/en
Priority to US00196656A priority patent/US3765791A/en
Publication of DE2054926B2 publication Critical patent/DE2054926B2/de
Publication of DE2054926A1 publication Critical patent/DE2054926A1/de
Pending 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE19702054926 1970-11-07 1970-11-07 Halterung eines turbinenleitkranzes Pending DE2054926B2 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE19702054926 DE2054926B2 (de) 1970-11-07 1970-11-07 Halterung eines turbinenleitkranzes
FR7046312A FR2112872A5 (enExample) 1970-11-07 1970-12-22
GB5138571A GB1368770A (en) 1970-11-07 1971-11-04 Gas turbine engine
US00196656A US3765791A (en) 1970-11-07 1971-11-08 Turbine nozzle support

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19702054926 DE2054926B2 (de) 1970-11-07 1970-11-07 Halterung eines turbinenleitkranzes

Publications (2)

Publication Number Publication Date
DE2054926B2 true DE2054926B2 (de) 1972-02-03
DE2054926A1 DE2054926A1 (enExample) 1972-02-03

Family

ID=5787498

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19702054926 Pending DE2054926B2 (de) 1970-11-07 1970-11-07 Halterung eines turbinenleitkranzes

Country Status (4)

Country Link
US (1) US3765791A (enExample)
DE (1) DE2054926B2 (enExample)
FR (1) FR2112872A5 (enExample)
GB (1) GB1368770A (enExample)

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 (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4274805A (en) * 1978-10-02 1981-06-23 United Technologies Corporation Floating vane support
US4566851A (en) * 1984-05-11 1986-01-28 United Technologies Corporation First stage turbine vane support structure
US4883405A (en) * 1987-11-13 1989-11-28 The United States Of America As Represented By The Secretary Of The Air Force Turbine nozzle mounting arrangement
US4815933A (en) * 1987-11-13 1989-03-28 The United States Of America As Represented By The Secretary Of The Air Force Nozzle flange attachment and sealing arrangement
US6884026B2 (en) * 2002-09-30 2005-04-26 General Electric Company Turbine engine shroud assembly including axially floating shroud segment
US6910853B2 (en) * 2002-11-27 2005-06-28 General Electric Company Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion
US8172522B2 (en) * 2008-03-31 2012-05-08 General Electric Company Method and system for supporting stator components
US8092163B2 (en) * 2008-03-31 2012-01-10 General Electric Company Turbine stator mount
US9506356B2 (en) * 2013-03-15 2016-11-29 Rolls-Royce North American Technologies, Inc. Composite retention feature
US9840933B2 (en) * 2014-12-19 2017-12-12 Schlumberger Technology Corporation Apparatus for extending the flow range of turbines
GB201616197D0 (en) * 2016-09-23 2016-11-09 Rolls Royce Plc Gas turbine engine
CN112302738B (zh) * 2020-09-30 2023-03-07 北京航天动力研究所 一种用于高压力涡轮进气壳体结构的柔性、力分类方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3129922A (en) * 1961-11-27 1964-04-21 Frederick A Rosenthal Self centering ring seal
US3391904A (en) * 1966-11-02 1968-07-09 United Aircraft Corp Optimum response tip seal
GB1277212A (en) * 1968-09-26 1972-06-07 Rolls Royce A sealing device
US3520635A (en) * 1968-11-04 1970-07-14 Avco Corp Turbomachine shroud assembly

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 (enExample) * 1981-12-08 1992-01-30 United Technologies Corp., Hartford, Conn., Us

Also Published As

Publication number Publication date
GB1368770A (en) 1974-10-02
DE2054926A1 (enExample) 1972-02-03
FR2112872A5 (enExample) 1972-06-23
US3765791A (en) 1973-10-16

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