CH496166A - Turbina a gas - Google Patents
Turbina a gasInfo
- Publication number
- CH496166A CH496166A CH558369A CH558369A CH496166A CH 496166 A CH496166 A CH 496166A CH 558369 A CH558369 A CH 558369A CH 558369 A CH558369 A CH 558369A CH 496166 A CH496166 A CH 496166A
- Authority
- CH
- Switzerland
- Prior art keywords
- gas turbine
- turbine
- gas
- Prior art date
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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1755168 | 1968-04-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH496166A true CH496166A (it) | 1970-09-15 |
Family
ID=10097172
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH558369A CH496166A (it) | 1968-04-11 | 1969-04-10 | Turbina a gas |
Country Status (4)
Country | Link |
---|---|
US (1) | US3635577A (it) |
CH (1) | CH496166A (it) |
DE (1) | DE1919310A1 (it) |
FR (1) | FR2006099A1 (it) |
Families Citing this family (20)
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 (it) * | 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 (it) * | 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 |
WO2002035072A2 (en) * | 2000-09-05 | 2002-05-02 | Sudarshan Paul Dev | Nested core gas turbine engine |
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 |
US8356469B1 (en) * | 2007-04-05 | 2013-01-22 | The United States Of America As Represented By The Secretary Of The Air Force | Gas turbine engine with dual compression rotor |
KR20140099443A (ko) * | 2011-09-23 | 2014-08-12 | 소크프라 시앙스 에 제니 에스.에.쎄. | 터빈부, 냉각 채널, 및 보강벽의 동심 배치를 갖는 로터 조립체 |
Family Cites Families (10)
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 |
-
1969
- 1969-04-07 US US814135A patent/US3635577A/en not_active Expired - Lifetime
- 1969-04-10 CH CH558369A patent/CH496166A/it not_active IP Right Cessation
- 1969-04-11 DE DE19691919310 patent/DE1919310A1/de active Pending
- 1969-04-11 FR FR6911306A patent/FR2006099A1/fr not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
US3635577A (en) | 1972-01-18 |
DE1919310A1 (de) | 1969-10-23 |
FR2006099A1 (it) | 1969-12-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PL | Patent ceased |