IL62818A - Flow directing assembly for a gas turbine engine - Google Patents

Flow directing assembly for a gas turbine engine

Info

Publication number
IL62818A
IL62818A IL62818A IL6281881A IL62818A IL 62818 A IL62818 A IL 62818A IL 62818 A IL62818 A IL 62818A IL 6281881 A IL6281881 A IL 6281881A IL 62818 A IL62818 A IL 62818A
Authority
IL
Israel
Prior art keywords
gas turbine
turbine engine
flow directing
directing assembly
assembly
Prior art date
Application number
IL62818A
Other languages
English (en)
Other versions
IL62818A0 (en
Original Assignee
United Technologies 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
Priority claimed from US06/150,514 external-priority patent/US4426191A/en
Priority claimed from US06/150,490 external-priority patent/US4431373A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of IL62818A0 publication Critical patent/IL62818A0/xx
Publication of IL62818A publication Critical patent/IL62818A/xx

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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26—Double casings; Measures against temperature strain in casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IL62818A 1980-05-16 1981-05-08 Flow directing assembly for a gas turbine engine IL62818A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/150,514 US4426191A (en) 1980-05-16 1980-05-16 Flow directing assembly for a gas turbine engine
US06/150,490 US4431373A (en) 1980-05-16 1980-05-16 Flow directing assembly for a gas turbine engine

Publications (2)

Publication Number Publication Date
IL62818A0 IL62818A0 (en) 1981-07-31
IL62818A true IL62818A (en) 1985-08-30

Family

ID=26847728

Family Applications (1)

Application Number Title Priority Date Filing Date
IL62818A IL62818A (en) 1980-05-16 1981-05-08 Flow directing assembly for a gas turbine engine

Country Status (5)

Country Link
BR (1) BR8103028A (fr)
DE (1) DE3119056A1 (fr)
FR (1) FR2482661B1 (fr)
GB (1) GB2076071B (fr)
IL (1) IL62818A (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2534982A1 (fr) * 1982-10-22 1984-04-27 Snecma Dispositif de controle des jeux d'un compresseur haute pression
FR2535795B1 (fr) * 1982-11-08 1987-04-10 Snecma Dispositif de suspension d'aubes statoriques de compresseur axial pour le controle actif des jeux entre rotor et stator
US4553901A (en) * 1983-12-21 1985-11-19 United Technologies Corporation Stator structure for a gas turbine engine
US4650394A (en) * 1984-11-13 1987-03-17 United Technologies Corporation Coolable seal assembly for a gas turbine engine
US4642024A (en) * 1984-12-05 1987-02-10 United Technologies Corporation Coolable stator assembly for a rotary machine
US4650395A (en) * 1984-12-21 1987-03-17 United Technologies Corporation Coolable seal segment for a rotary machine
FR2577282B1 (fr) * 1985-02-13 1987-04-17 Snecma Carter de turbomachine associe a un dispositif pour ajuster le jeu entre rotor et stator
FR2607198B1 (fr) * 1986-11-26 1990-05-04 Snecma Carter de compresseur adapte pour le pilotage actif de ses dilatations et son procede de fabrication
US5197856A (en) * 1991-06-24 1993-03-30 General Electric Company Compressor stator
EP0550126A1 (fr) * 1992-01-02 1993-07-07 General Electric Company Bouclier thermique pour post-combusteur
FR2695164B1 (fr) * 1992-08-26 1994-11-04 Snecma Turbomachine munie d'un dispositif empêchant une circulation longitudinale de gaz autour des étages d'aubes de redressement.
US5320486A (en) * 1993-01-21 1994-06-14 General Electric Company Apparatus for positioning compressor liner segments
FR2711730B1 (fr) * 1993-10-27 1995-12-01 Snecma Turbomachine équipée de moyens de pilotage des jeux entre rotor et stator.
FR2829176B1 (fr) * 2001-08-30 2005-06-24 Snecma Moteurs Carter de stator de turbomachine
DE102004037356B4 (de) * 2004-07-30 2017-11-23 Ansaldo Energia Ip Uk Limited Wandstruktur zur Begrenzung eines Heißgaspfads

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE724321C (de) * 1936-03-01 1942-08-24 Karl Roeder Dr Ing In mindestens einer Achsebene unterteilter, mehrere Kraenze enthaltender Leitschaufeltraeger, insbesondere fuer UEberdruck-Dampfturbinen
DE907179C (de) * 1943-08-24 1954-03-22 Svenska Rotor Maskiner Ab Turbine mit einem oder mehreren Ringkoerpern
GB589294A (en) * 1943-08-24 1947-06-17 Ljungstroms Angturbin Ab Improvements in or relating to turbines
GB808655A (en) * 1954-11-22 1959-02-11 Rolls Royce Improvements in or relating to multi-stage axial-flow compressors
US2848156A (en) * 1956-12-18 1958-08-19 Gen Electric Fixed stator vane assemblies
GB1175674A (en) * 1965-12-22 1969-12-23 Rolls Royce Turbines and Compressors
US4019320A (en) * 1975-12-05 1977-04-26 United Technologies Corporation External gas turbine engine cooling for clearance control
GB2019954B (en) * 1978-04-04 1982-08-04 Rolls Royce Turbomachine housing

Also Published As

Publication number Publication date
DE3119056A1 (de) 1982-02-25
DE3119056C2 (fr) 1993-02-25
GB2076071A (en) 1981-11-25
IL62818A0 (en) 1981-07-31
FR2482661B1 (fr) 1986-12-05
BR8103028A (pt) 1982-02-09
GB2076071B (en) 1983-11-02
FR2482661A1 (fr) 1981-11-20

Similar Documents

Publication Publication Date Title
GB2103294B (en) Shroud assembly for a gas turbine engine
GB2078859B (en) Control means for a gas turbine engine
GB2125111B (en) Shroud assembly for a gas turbine engine
GB2097479B (en) Cooled vane for a gas turbine engine
DE3265642D1 (en) Fuel nozzle assembly for a gas turbine engine
JPS5791328A (en) Axial flow gas turbine engine
JPS56168040A (en) Circular combustor for gas turbine engine
JPS5720539A (en) Exhaust nozzle for gas turbine engine
GB2119028B (en) Aerofoil for a gas turbine engine
JPS5751901A (en) Gas turbine engine
GB2127906B (en) Rotor assembly e g for a gas turbine engine
GB2100808B (en) Blade root modification for a gas turbine engine
GB2117450B (en) Casing support for a gas turbine engine
JPS5784930A (en) Gas turbine engine
JPS56106006A (en) Moving blade for gas turbine engine
GB2088015B (en) Modular inlet gearbox for a gas turbine engine
JPS572449A (en) Gas turbine engine
GB2088963B (en) Gas turbine engine control
GB2076071B (en) Flow directing assembly for a gas turbine engine
GB2120325B (en) Prediffuser for a gas turbine engine
GB2161914B (en) Combustion equipment for a gas turbine engine
IL68682A0 (en) Diffuser case for a gas turbine engine
GB2105027B (en) Starting means for a gas turbine engine
GB2107405B (en) Nozzle guide vane for a gas turbine engine
GB2089894B (en) Gas turbine engine air dispensing arrangement

Legal Events

Date Code Title Description
KB Patent renewed
EXP Patent expired