GB1515348A - Multistage axial-flow compressors - Google Patents
Multistage axial-flow compressorsInfo
- Publication number
- GB1515348A GB1515348A GB2280675A GB2280675A GB1515348A GB 1515348 A GB1515348 A GB 1515348A GB 2280675 A GB2280675 A GB 2280675A GB 2280675 A GB2280675 A GB 2280675A GB 1515348 A GB1515348 A GB 1515348A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade carrier
- upstream
- stator blade
- stator
- inlet
- 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
- F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1515348 Axial-flow compressors BROWN BOVERI-SULZER TURBOMACHINERY Ltd 23 May 1975 [17 June 1974] 22806/75 Heading F1C A multi-stage axial-flow compressor comprises two or more successive compression sections A, B, C each comprising a stator blade carrier 8, 20, 35 and having an inlet to which an inlet connection 4, 30, 44 leads and to which (except in the case of the upstream section A), the delivery of the preceding section leads; each stator blade carrier 20, 35 other than the upstream one 8 being connected to the casing 3 by a generally radially extending partition 3a, 3b which on its upstream side bounds the respective inlet connection 30, 44, and each such stator blade carrier 20, 35 extending from its partition 3a, 3b to form with the immediately upstream stator blade carrier 8, 20 an annular intake passage 24, 39. Adjustable inlet stator blades 11, 25, 40 and it may be, 28, 43 are provided. Each blade 25, 40 may change smoothly in profile along its length or may be divided into two zones 25a, 25b or 40a, 40b of differing profile as appropriate for the two flows handled by the blade.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH824774A CH579218A5 (en) | 1974-06-17 | 1974-06-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1515348A true GB1515348A (en) | 1978-06-21 |
Family
ID=4337406
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2280675A Expired GB1515348A (en) | 1974-06-17 | 1975-05-23 | Multistage axial-flow compressors |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPS5113407A (en) |
CH (1) | CH579218A5 (en) |
DE (1) | DE2430117B1 (en) |
FR (1) | FR2274805A1 (en) |
GB (1) | GB1515348A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITUB20152489A1 (en) * | 2015-07-24 | 2017-01-24 | Nuovo Pignone Tecnologie Srl | COMPRESSION TRAIN WITH AN AXIAL COMPRESSOR AND LNG SYSTEM WITH AN AXIAL COMPRESSOR |
ITUB20152501A1 (en) * | 2015-07-24 | 2017-01-24 | Nuovo Pignone Tecnologie Srl | COMPRESSION TRAIN WITH A CENTRIFUGAL COMPRESSOR AND LNG SYSTEM WITH A CENTRIFUGAL COMPRESSOR |
WO2017017025A1 (en) * | 2015-07-24 | 2017-02-02 | Nuovo Pignone Tecnologie Srl | Lng plant including an axial compressor and a centrifugal compressor |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060198726A1 (en) * | 2005-03-07 | 2006-09-07 | General Electric Company | Apparatus for eliminating compressor stator vibration induced by tip leakage vortex bursting |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5015607U (en) * | 1973-06-07 | 1975-02-19 |
-
1974
- 1974-06-17 CH CH824774A patent/CH579218A5/xx not_active IP Right Cessation
- 1974-06-22 DE DE2430117A patent/DE2430117B1/en active Pending
-
1975
- 1975-05-22 FR FR7515947A patent/FR2274805A1/en active Granted
- 1975-05-23 GB GB2280675A patent/GB1515348A/en not_active Expired
- 1975-06-16 JP JP7300075A patent/JPS5113407A/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITUB20152489A1 (en) * | 2015-07-24 | 2017-01-24 | Nuovo Pignone Tecnologie Srl | COMPRESSION TRAIN WITH AN AXIAL COMPRESSOR AND LNG SYSTEM WITH AN AXIAL COMPRESSOR |
ITUB20152501A1 (en) * | 2015-07-24 | 2017-01-24 | Nuovo Pignone Tecnologie Srl | COMPRESSION TRAIN WITH A CENTRIFUGAL COMPRESSOR AND LNG SYSTEM WITH A CENTRIFUGAL COMPRESSOR |
WO2017017025A1 (en) * | 2015-07-24 | 2017-02-02 | Nuovo Pignone Tecnologie Srl | Lng plant including an axial compressor and a centrifugal compressor |
CN107850077A (en) * | 2015-07-24 | 2018-03-27 | 诺沃皮尼奥内技术股份有限公司 | LNG plant including axial compressor and centrifugal compressor |
Also Published As
Publication number | Publication date |
---|---|
JPS5113407A (en) | 1976-02-02 |
DE2430117B1 (en) | 1975-03-20 |
FR2274805A1 (en) | 1976-01-09 |
CH579218A5 (en) | 1976-08-31 |
FR2274805B1 (en) | 1978-09-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed |