FR2006099A1 - - Google Patents

Info

Publication number
FR2006099A1
FR2006099A1 FR6911306A FR6911306A FR2006099A1 FR 2006099 A1 FR2006099 A1 FR 2006099A1 FR 6911306 A FR6911306 A FR 6911306A FR 6911306 A FR6911306 A FR 6911306A FR 2006099 A1 FR2006099 A1 FR 2006099A1
Authority
FR
France
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.)
Withdrawn
Application number
FR6911306A
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.)
Aerostatic Ltd
Original Assignee
Aerostatic Ltd
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 Aerostatic Ltd filed Critical Aerostatic Ltd
Publication of FR2006099A1 publication Critical patent/FR2006099A1/fr
Withdrawn legal-status Critical Current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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/284—Selection of ceramic materials
    • 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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • F01D1/04—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines traversed by the working-fluid substantially axially
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric
FR6911306A 1968-04-11 1969-04-11 Withdrawn FR2006099A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1755168 1968-04-11

Publications (1)

Publication Number Publication Date
FR2006099A1 true FR2006099A1 (fr) 1969-12-19

Family

ID=10097172

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6911306A Withdrawn FR2006099A1 (fr) 1968-04-11 1969-04-11

Country Status (4)

Country Link
US (1) US3635577A (fr)
CH (1) CH496166A (fr)
DE (1) DE1919310A1 (fr)
FR (1) FR2006099A1 (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3970408A (en) * 1967-10-26 1976-07-20 Bio-Medicus, Inc. Apparatus for use with delicate fluids
US4038815A (en) * 1973-03-30 1977-08-02 Northern Research And Engineering Corporation Gas turbine
US3901622A (en) * 1973-05-31 1975-08-26 Gen Motors Corp Yieldable shroud support
US3999376A (en) * 1973-07-05 1976-12-28 Ford Motor Company One-piece ceramic support housing for a gas turbine with a rotary regenerator
US3867065A (en) * 1973-07-16 1975-02-18 Westinghouse Electric Corp Ceramic insulator for a gas turbine blade structure
US4064690A (en) * 1974-05-17 1977-12-27 United Turbine Ab & Co. Gas turbine power plant
USB552006I5 (fr) * 1975-02-24 1976-02-03
DE2554353A1 (de) * 1975-12-03 1977-06-16 Motoren Turbinen Union Gasturbinentriebwerk
FR2475113A1 (fr) * 1980-02-04 1981-08-07 Rockwell International Corp Rotor ceramique pour turbine
DE3909050C1 (fr) * 1989-03-18 1990-08-16 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
US5263315A (en) * 1990-11-09 1993-11-23 Sundstrand Corp. Starting of a small turbojet
US5207054A (en) * 1991-04-24 1993-05-04 Sundstrand Corporation Small diameter gas turbine engine
JP2630701B2 (ja) * 1991-10-21 1997-07-16 陸郎 野津 対称翼型タービンのタービンロータブレード
US5241815A (en) * 1992-04-22 1993-09-07 Lee Dae S Heat-recovering-thrust-turbine having rotational flow path
US5473899A (en) * 1993-06-10 1995-12-12 Viteri; Fermin Turbomachinery for Modified Ericsson engines and other power/refrigeration applications
EP1317608A4 (fr) * 2000-09-05 2004-12-15 Sudarshan Paul Dev Turbine a gaz a coeur emboite
US6397577B1 (en) * 2001-04-02 2002-06-04 The United States Of America As Represented By The Secretary Of The Air Force Shaftless gas turbine engine spool
US6647732B2 (en) * 2001-09-17 2003-11-18 Industrial Technology Research Institute Gas turbine engine with compressor and turbine inside a hollow shaft
US8192141B1 (en) * 2007-04-05 2012-06-05 The United States Of America As Represented By The Secretary Of The Air Force Dual compression rotor
US9670840B2 (en) 2011-09-23 2017-06-06 Socpra—Science Et Genie, S.E.C. Rotor assembly having a concentric arrangement of a turbine portion, a cooling channel and a reinforcement wall

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2414410A (en) * 1941-06-23 1947-01-14 Rolls Royce Axial-flow compressor, turbine, and the like
US2430398A (en) * 1942-09-03 1947-11-04 Armstrong Siddeley Motors Ltd Jet-propulsion internal-combustion turbine plant
US2454738A (en) * 1944-01-31 1948-11-23 Power Jets Res And Development Internal-combustion turbine power plant
FR907059A (fr) * 1946-09-20 1946-02-28 Turbine à gaz à haute température
US2686657A (en) * 1947-08-02 1954-08-17 United Aircraft Corp Diaphragm seal for turbines
US2721445A (en) * 1949-12-22 1955-10-25 James V Giliberty Aircraft propulsion plant of the propeller-jet turbine type
US2643852A (en) * 1950-01-09 1953-06-30 Us Air Force High-speed turbine
US2963268A (en) * 1957-03-25 1960-12-06 Gen Electric Pressurized seal
US3025037A (en) * 1957-10-24 1962-03-13 Bert F Beckstrom Gas turbine
US3035759A (en) * 1957-11-13 1962-05-22 Gen Electric Rotor and stator construction

Also Published As

Publication number Publication date
CH496166A (it) 1970-09-15
US3635577A (en) 1972-01-18
DE1919310A1 (de) 1969-10-23

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Legal Events

Date Code Title Description
ST Notification of lapse