CH494895A - Guide vane ring for turbo machines - Google Patents
Guide vane ring for turbo machinesInfo
- Publication number
- CH494895A CH494895A CH1127668A CH1127668A CH494895A CH 494895 A CH494895 A CH 494895A CH 1127668 A CH1127668 A CH 1127668A CH 1127668 A CH1127668 A CH 1127668A CH 494895 A CH494895 A CH 494895A
- Authority
- CH
- Switzerland
- Prior art keywords
- guide vane
- vane ring
- turbo machines
- turbo
- machines
- 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
-
- 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
-
- 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
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Mounting Of Bearings Or Others (AREA)
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH1127668A CH494895A (en) | 1968-07-26 | 1968-07-26 | Guide vane ring for turbo machines |
DE19681751812 DE1751812B2 (en) | 1968-07-26 | 1968-08-02 | GUIDE VANE WREATH OF AN AXIALLY FLOWED SCHROEMUNGS MACHINE |
NL686811394A NL145635B (en) | 1968-07-26 | 1968-08-09 | AXIALLY FLOWED TURBO MACHINE. |
US779545A US3582231A (en) | 1968-07-26 | 1968-11-27 | Bearing mount for vane rings of turboengines |
BE731928D BE731928A (en) | 1968-07-26 | 1969-04-23 | |
FR6914796A FR2013758A1 (en) | 1968-07-26 | 1969-05-08 | |
GB37290/69A GB1271822A (en) | 1968-07-26 | 1969-07-24 | Stator blade rings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH1127668A CH494895A (en) | 1968-07-26 | 1968-07-26 | Guide vane ring for turbo machines |
Publications (1)
Publication Number | Publication Date |
---|---|
CH494895A true CH494895A (en) | 1970-08-15 |
Family
ID=4371878
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH1127668A CH494895A (en) | 1968-07-26 | 1968-07-26 | Guide vane ring for turbo machines |
Country Status (7)
Country | Link |
---|---|
US (1) | US3582231A (en) |
BE (1) | BE731928A (en) |
CH (1) | CH494895A (en) |
DE (1) | DE1751812B2 (en) |
FR (1) | FR2013758A1 (en) |
GB (1) | GB1271822A (en) |
NL (1) | NL145635B (en) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3850544A (en) * | 1973-11-02 | 1974-11-26 | Gen Electric | Mounting arrangement for a bearing of axial flow turbomachinery having variable pitch stationary blades |
US4025227A (en) * | 1975-06-30 | 1977-05-24 | United Technologies Corporation | Variable area turbine |
US3966352A (en) * | 1975-06-30 | 1976-06-29 | United Technologies Corporation | Variable area turbine |
CA1052231A (en) * | 1976-04-22 | 1979-04-10 | Dominion Engineering Works Limited | Water turbine bearing seal |
DE19747555A1 (en) * | 1997-10-28 | 1999-04-29 | Voith Sulzer Papiertech Patent | Heated and / or coolable cylinder |
US6453556B1 (en) * | 2000-10-11 | 2002-09-24 | Hmy Ltd. | Method of producing exhaust gas vane blade for superchargers of motor vehicles and vane blade |
EP1895106A1 (en) * | 2006-08-28 | 2008-03-05 | ABB Turbo Systems AG | Sealing of variable guide vanes |
CN112388260A (en) * | 2020-11-20 | 2021-02-23 | 无锡航亚科技股份有限公司 | Machining method for journal of double-journal rectifying blade of aircraft engine |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE514728A (en) * | 1951-10-10 | |||
GB755527A (en) * | 1953-10-15 | 1956-08-22 | Power Jets Res & Dev Ltd | Mounting of swivelling guide vane elements in axial flow elastic fluid turbines |
US3013771A (en) * | 1960-10-18 | 1961-12-19 | Chrysler Corp | Adjustable nozzles for gas turbine engine |
US3367628A (en) * | 1966-10-31 | 1968-02-06 | United Aircraft Corp | Movable vane unit |
-
1968
- 1968-07-26 CH CH1127668A patent/CH494895A/en not_active IP Right Cessation
- 1968-08-02 DE DE19681751812 patent/DE1751812B2/en not_active Withdrawn
- 1968-08-09 NL NL686811394A patent/NL145635B/en unknown
- 1968-11-27 US US779545A patent/US3582231A/en not_active Expired - Lifetime
-
1969
- 1969-04-23 BE BE731928D patent/BE731928A/xx unknown
- 1969-05-08 FR FR6914796A patent/FR2013758A1/fr not_active Withdrawn
- 1969-07-24 GB GB37290/69A patent/GB1271822A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE1751812A1 (en) | 1970-10-01 |
DE1751812B2 (en) | 1971-05-13 |
FR2013758A1 (en) | 1970-04-10 |
NL6811394A (en) | 1970-01-29 |
BE731928A (en) | 1969-10-23 |
NL145635B (en) | 1975-04-15 |
US3582231A (en) | 1971-06-01 |
GB1271822A (en) | 1972-04-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PL | Patent ceased |