BE673345A - - Google Patents

Info

Publication number
BE673345A
BE673345A BE673345DA BE673345A BE 673345 A BE673345 A BE 673345A BE 673345D A BE673345D A BE 673345DA BE 673345 A BE673345 A BE 673345A
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 BE673345A publication Critical patent/BE673345A/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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/147Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • 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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BE673345D 1964-12-07 1965-12-06 BE673345A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US416387A US3269700A (en) 1964-12-07 1964-12-07 Heat shield for turbine strut

Publications (1)

Publication Number Publication Date
BE673345A true BE673345A (de) 1966-04-01

Family

ID=23649762

Family Applications (1)

Application Number Title Priority Date Filing Date
BE673345D BE673345A (de) 1964-12-07 1965-12-06

Country Status (5)

Country Link
US (1) US3269700A (de)
BE (1) BE673345A (de)
DE (1) DE1297938B (de)
FR (1) FR1457118A (de)
GB (1) GB1063240A (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009151701A2 (en) 2008-03-18 2009-12-17 United Technologies Corporation Gas turbine engine systems involving fairings with locating data
EP2218894A3 (de) * 2009-02-16 2013-07-24 Rolls-Royce plc Anordnung zur Befestigung einer Leitschaufel

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3403889A (en) * 1966-04-07 1968-10-01 Gen Electric Frame assembly having low thermal stresses
US3529902A (en) * 1968-05-22 1970-09-22 Gen Motors Corp Turbine vane
GB2168111B (en) * 1984-12-08 1988-05-18 Rolls Royce Rotor aerofoil blade containment
US4820117A (en) * 1987-07-09 1989-04-11 United Technologies Corporation Crossed I-beam structural strut
US5085559A (en) * 1990-04-16 1992-02-04 The United States Of America As Represented By The Secretary Of The Air Force Composite vane
GB9202982D0 (en) * 1992-02-13 1992-03-25 Preci Spark Ltd Reinforced vane
US5509783A (en) * 1993-02-09 1996-04-23 Preci-Spark, Ltd. Reinforced vane
US6796765B2 (en) 2001-12-27 2004-09-28 General Electric Company Methods and apparatus for assembling gas turbine engine struts
US8366047B2 (en) * 2005-05-31 2013-02-05 United Technologies Corporation Electrothermal inlet ice protection system
US7950899B2 (en) * 2005-05-31 2011-05-31 United Technologies Corporation Modular fan inlet case
EP1930544A1 (de) * 2006-10-30 2008-06-11 Siemens Aktiengesellschaft Turbinenschaufel
GB2467791B (en) * 2009-02-16 2011-06-01 Rolls Royce Plc Vane
FR2981700B1 (fr) * 2011-10-24 2016-08-26 Snecma Propulsion Solide Dispositif de fixation d'une piece creuse
CN102400721B (zh) * 2011-11-01 2014-04-02 沈阳黎明航空发动机(集团)有限责任公司 一种涡轮支承支点隔热屏的更换方法
CH705838A1 (de) * 2011-12-05 2013-06-14 Alstom Technology Ltd Abgasgehäuse für eine Gasturbine sowie Gasturbine mit einem Abgasgehäuse.
US9995160B2 (en) 2014-12-22 2018-06-12 General Electric Company Airfoil profile-shaped seals and turbine components employing same

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2500745A (en) * 1944-09-21 1950-03-14 Gen Electric Bucket structure for high-temperature turbomachines
US2771622A (en) * 1952-05-09 1956-11-27 Westinghouse Electric Corp Diaphragm apparatus
BE529252A (de) * 1953-06-01

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009151701A2 (en) 2008-03-18 2009-12-17 United Technologies Corporation Gas turbine engine systems involving fairings with locating data
WO2009151701A3 (en) * 2008-03-18 2010-11-18 United Technologies Corporation Gas turbine engine systems with fairing
EP2218894A3 (de) * 2009-02-16 2013-07-24 Rolls-Royce plc Anordnung zur Befestigung einer Leitschaufel

Also Published As

Publication number Publication date
DE1297938B (de) 1969-06-19
GB1063240A (en) 1967-03-30
US3269700A (en) 1966-08-30
FR1457118A (fr) 1966-10-28

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