GB1259739A - Improvements in or relating to axial flow compressors - Google Patents
Improvements in or relating to axial flow compressorsInfo
- Publication number
- GB1259739A GB1259739A GB7555/70A GB755570A GB1259739A GB 1259739 A GB1259739 A GB 1259739A GB 7555/70 A GB7555/70 A GB 7555/70A GB 755570 A GB755570 A GB 755570A GB 1259739 A GB1259739 A GB 1259739A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring
- supporting
- stator
- control ring
- blade
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CS120669 | 1969-02-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1259739A true GB1259739A (en) | 1972-01-12 |
Family
ID=5345873
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7555/70A Expired GB1259739A (en) | 1969-02-20 | 1970-02-17 | Improvements in or relating to axial flow compressors |
Country Status (5)
Country | Link |
---|---|
US (1) | US3647312A (de) |
CH (1) | CH510202A (de) |
DE (1) | DE2005536B2 (de) |
GB (1) | GB1259739A (de) |
SE (1) | SE359148B (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8905887B2 (en) | 2012-02-13 | 2014-12-09 | Rolls-Royce Plc | Unison ring gear assembly |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3736070A (en) * | 1971-06-22 | 1973-05-29 | Curtiss Wright Corp | Variable stator blade assembly for axial flow, fluid expansion engine |
FR2698405B1 (fr) * | 1992-11-25 | 1994-12-23 | Snecma | Turbomachine à plusieurs étages d'aubes de stator à orientation variable. |
US8186963B2 (en) * | 2010-08-31 | 2012-05-29 | General Electric Company | Airfoil shape for compressor inlet guide vane |
BE1026816B1 (fr) * | 2018-11-29 | 2020-07-01 | Safran Aero Boosters Sa | Système de calage variable d’aubes d’un étage statorique d’un compresseur d’une turbomachine d’aéronef |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2305311A (en) * | 1937-07-07 | 1942-12-15 | Jendrassik George | Gas turbine plant equipped with regulating apparatus |
GB621175A (en) * | 1946-11-16 | 1949-04-05 | Power Jets Res & Dev Ltd | Improvements in or relating to stator blading of compressors and like machines |
US3013771A (en) * | 1960-10-18 | 1961-12-19 | Chrysler Corp | Adjustable nozzles for gas turbine engine |
-
1970
- 1970-02-06 DE DE19702005536 patent/DE2005536B2/de not_active Withdrawn
- 1970-02-17 US US11948A patent/US3647312A/en not_active Expired - Lifetime
- 1970-02-17 GB GB7555/70A patent/GB1259739A/en not_active Expired
- 1970-02-18 CH CH230870A patent/CH510202A/de not_active IP Right Cessation
- 1970-02-20 SE SE02222/70A patent/SE359148B/xx unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8905887B2 (en) | 2012-02-13 | 2014-12-09 | Rolls-Royce Plc | Unison ring gear assembly |
Also Published As
Publication number | Publication date |
---|---|
SE359148B (de) | 1973-08-20 |
CH510202A (de) | 1971-07-15 |
US3647312A (en) | 1972-03-07 |
DE2005536B2 (de) | 1972-05-04 |
DE2005536A1 (de) | 1970-09-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |