CH326300A - Axial durchströmte Turbine, insbesondere Gasturbine - Google Patents
Axial durchströmte Turbine, insbesondere GasturbineInfo
- Publication number
- CH326300A CH326300A CH326300DA CH326300A CH 326300 A CH326300 A CH 326300A CH 326300D A CH326300D A CH 326300DA CH 326300 A CH326300 A CH 326300A
- Authority
- CH
- Switzerland
- Prior art keywords
- turbine
- axial flow
- particular gas
- gas turbine
- flow turbine
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
-
- A—HUMAN NECESSITIES
- A41—WEARING APPAREL
- A41D—OUTERWEAR; PROTECTIVE GARMENTS; ACCESSORIES
- A41D31/00—Materials specially adapted for outerwear
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2950084X | 1953-10-15 | ||
GB28462/53A GB755527A (en) | 1953-10-15 | 1954-10-04 | Mounting of swivelling guide vane elements in axial flow elastic fluid turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
CH326300A true CH326300A (de) | 1957-12-15 |
Family
ID=32396004
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH326300D CH326300A (de) | 1953-10-15 | 1954-10-12 | Axial durchströmte Turbine, insbesondere Gasturbine |
Country Status (5)
Country | Link |
---|---|
US (1) | US2950084A (de) |
CH (1) | CH326300A (de) |
DE (1) | DE1003512B (de) |
FR (1) | FR1114461A (de) |
GB (1) | GB755527A (de) |
Families Citing this family (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2936108A (en) * | 1957-04-29 | 1960-05-10 | Gen Electric | Compressor |
US3059900A (en) * | 1960-11-15 | 1962-10-23 | Chrysler Corp | Gas turbine engine interstage inner shroud suspension |
DE1218800B (de) * | 1961-04-25 | 1966-06-08 | M A N Turbo Ges Mit Beschraenk | Gasturbine, insbesondere Kleingasturbine |
US3059902A (en) * | 1961-07-03 | 1962-10-23 | Chrysler Corp | Adjustable nozzle and intermediate inner shroud support |
US3224194A (en) * | 1963-06-26 | 1965-12-21 | Curtiss Wright Corp | Gas turbine engine |
US3471126A (en) * | 1966-10-31 | 1969-10-07 | United Aircraft Corp | Movable vane unit |
US3367628A (en) * | 1966-10-31 | 1968-02-06 | United Aircraft Corp | Movable vane unit |
CH494340A (de) * | 1968-07-26 | 1970-07-31 | Sulzer Ag | Leitschaufelkranz für Turbomaschinen III |
CH494895A (de) * | 1968-07-26 | 1970-08-15 | Sulzer Ag | Leitschaufelkranz für Turbomaschinen |
FR2030895A5 (de) * | 1969-05-23 | 1970-11-13 | Motoren Turbinen Union | |
FR2055780A1 (de) * | 1969-08-14 | 1971-04-30 | Bennes Marrel | |
US4025227A (en) * | 1975-06-30 | 1977-05-24 | United Technologies Corporation | Variable area turbine |
US4007998A (en) * | 1975-08-22 | 1977-02-15 | Carrier Corporation | Blade assembly |
US3990810A (en) * | 1975-12-23 | 1976-11-09 | Westinghouse Electric Corporation | Vane assembly for close coupling the compressor turbine and a single stage power turbine of a two-shaped gas turbine |
US4035101A (en) * | 1976-03-24 | 1977-07-12 | Westinghouse Electric Corporation | Gas turbine nozzle vane adjusting mechanism |
US4214852A (en) * | 1978-04-20 | 1980-07-29 | General Electric Company | Variable turbine vane assembly |
DE2835349C2 (de) * | 1978-08-11 | 1979-12-20 | Mtu Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Verstelleitgitter für hochbelastete Verdichter, insbesondere von Gasturbinentriebwerken |
US4863352A (en) * | 1984-11-02 | 1989-09-05 | General Electric Company | Blade carrying means |
DE3613857A1 (de) * | 1986-04-24 | 1987-10-29 | Kuehnle Kopp Kausch Ag | Axialdrallregler fuer einen abgasturbolader fuer verbrennungsmotoren |
DE3623001C1 (de) * | 1986-07-09 | 1987-07-09 | Mtu Muenchen Gmbh | Verstellvorrichtung fuer schwenkbare Leitschaufeln von Turbotriebwerken |
US4834613A (en) * | 1988-02-26 | 1989-05-30 | United Technologies Corporation | Radially constrained variable vane shroud |
US5108259A (en) * | 1988-12-19 | 1992-04-28 | General Electric Company | Flexible connector for use in aircraft |
US5672047A (en) * | 1995-04-12 | 1997-09-30 | Dresser-Rand Company | Adjustable stator vanes for turbomachinery |
US5931636A (en) * | 1997-08-28 | 1999-08-03 | General Electric Company | Variable area turbine nozzle |
ITTO20010444A1 (it) * | 2001-05-11 | 2002-11-11 | Fiatavio Spa | Turbina assiale per applicazioni aeronautiche. |
FR2890707B1 (fr) | 2005-09-14 | 2007-12-14 | Snecma | Douille pour pivot d'aube a angle de calage variable pour turbomachine |
EP1820941A1 (de) * | 2006-02-09 | 2007-08-22 | Siemens Aktiengesellschaft | Leitapparat und Dämpfelement für einen Leitapparat |
EP1895106A1 (de) * | 2006-08-28 | 2008-03-05 | ABB Turbo Systems AG | Abdichtung verstellbarer Leitschaufeln |
FR2920469A1 (fr) * | 2007-08-30 | 2009-03-06 | Snecma Sa | Aube a calage variable de turbomachine |
DE102008021683A1 (de) * | 2008-04-30 | 2009-11-05 | Rolls-Royce Deutschland Ltd & Co Kg | Rotierende Einheit für einen Axialkompressor |
US8920116B2 (en) * | 2011-10-07 | 2014-12-30 | Siemens Energy, Inc. | Wear prevention system for securing compressor airfoils within a turbine engine |
EP2884054A1 (de) * | 2013-12-10 | 2015-06-17 | MTU Aero Engines GmbH | Verstellbare Leitschaufel mit Kegelstumpf in einer Lageranordnung |
EP3176386B1 (de) * | 2015-12-04 | 2021-01-27 | MTU Aero Engines GmbH | Innenringsystem, zugehöriger innenring, zwichengehäuse und strömungsmaschine |
DE102016204291A1 (de) * | 2016-03-16 | 2017-09-21 | MTU Aero Engines AG | Leitschaufelteller mit einem angefasten und einem zylindrischen Randbereich |
GB201616108D0 (en) * | 2016-09-22 | 2016-11-09 | Rolls Royce Plc | Gas turbine engine |
GB2588956A (en) * | 2019-11-15 | 2021-05-19 | Rolls Royce Plc | A variable vane assembly |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2300766A (en) * | 1940-05-10 | 1942-11-03 | Bbc Brown Boveri & Cie | Multistage centrifugal compressor |
US2337861A (en) * | 1941-02-04 | 1943-12-28 | James Russell Kennedy | Propeller |
BE471940A (de) * | 1946-03-20 | |||
BE496713A (de) * | 1949-07-01 | |||
BE514728A (de) * | 1951-10-10 |
-
1954
- 1954-10-04 GB GB28462/53A patent/GB755527A/en not_active Expired
- 1954-10-07 DE DEP12825A patent/DE1003512B/de active Pending
- 1954-10-11 US US461601A patent/US2950084A/en not_active Expired - Lifetime
- 1954-10-12 CH CH326300D patent/CH326300A/de unknown
- 1954-10-13 FR FR1114461D patent/FR1114461A/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR1114461A (fr) | 1956-04-12 |
GB755527A (en) | 1956-08-22 |
US2950084A (en) | 1960-08-23 |
DE1003512B (de) | 1957-02-28 |
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