GB1273184A - Stator blade rings - Google Patents
Stator blade ringsInfo
- Publication number
- GB1273184A GB1273184A GB37291/69A GB3729169A GB1273184A GB 1273184 A GB1273184 A GB 1273184A GB 37291/69 A GB37291/69 A GB 37291/69A GB 3729169 A GB3729169 A GB 3729169A GB 1273184 A GB1273184 A GB 1273184A
- Authority
- GB
- United Kingdom
- Prior art keywords
- stator blade
- july
- blade rings
- journal
- aerofoil
- Prior art date
- 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.)
- Expired
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
- 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
-
- 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
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1,273,184. Turbines; axial-flow compressor and pumps. SULZER BROS Ltd. July 24, 1969 [July 26, 1968], No.37291/69. Headings F1C and FIT] The subject matter of this Specification is the same as that of Specification 1, 271, 822 but the claims are concerned with the feature that the aerofoil and journal portions of the adjustable stator blades are formed from different materials, the journal material being suitable for dry running in a heat resistant plastics bearing.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH1127768A CH494343A (en) | 1968-07-26 | 1968-07-26 | Guide vane ring for turbo machines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1273184A true GB1273184A (en) | 1972-05-03 |
Family
ID=4371886
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB37291/69A Expired GB1273184A (en) | 1968-07-26 | 1969-07-24 | Stator blade rings |
GB61046/71A Expired GB1276640A (en) | 1968-07-26 | 1969-07-24 | Stator blade rings |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB61046/71A Expired GB1276640A (en) | 1968-07-26 | 1969-07-24 | Stator blade rings |
Country Status (7)
Country | Link |
---|---|
US (1) | US3552882A (en) |
BE (1) | BE731929A (en) |
CH (1) | CH494343A (en) |
DE (1) | DE1751813B1 (en) |
FR (1) | FR2013757A1 (en) |
GB (2) | GB1273184A (en) |
NL (1) | NL147224B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITTO20010446A1 (en) * | 2001-05-11 | 2002-11-11 | Fiatavio Spa | VANE FOR A STATOR OF A VARIABLE GEOMETRY TURBINE, IN PARTICULAR FOR AIRCRAFT ENGINES. |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2431660A (en) * | 1944-12-01 | 1947-11-25 | Bbc Brown Boveri & Cie | Turbine blade |
US3325087A (en) * | 1965-04-28 | 1967-06-13 | David R Davis | Stator casing construction for gas turbine engines |
-
1968
- 1968-07-26 CH CH1127768A patent/CH494343A/en not_active IP Right Cessation
- 1968-08-02 DE DE19681751813 patent/DE1751813B1/en not_active Withdrawn
- 1968-08-09 NL NL686811395A patent/NL147224B/en unknown
- 1968-11-27 US US779356A patent/US3552882A/en not_active Expired - Lifetime
-
1969
- 1969-04-23 BE BE731929D patent/BE731929A/xx unknown
- 1969-05-07 FR FR6914619A patent/FR2013757A1/fr not_active Withdrawn
- 1969-07-24 GB GB37291/69A patent/GB1273184A/en not_active Expired
- 1969-07-24 GB GB61046/71A patent/GB1276640A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2013757A1 (en) | 1970-04-10 |
US3552882A (en) | 1971-01-05 |
BE731929A (en) | 1969-10-23 |
NL147224B (en) | 1975-09-15 |
GB1276640A (en) | 1972-06-07 |
NL6811395A (en) | 1970-01-29 |
DE1751813B1 (en) | 1971-04-29 |
CH494343A (en) | 1970-07-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |