PL2126367T3 - Wielostopniowa sprężarka układu turbogazowego - Google Patents
Wielostopniowa sprężarka układu turbogazowegoInfo
- Publication number
- PL2126367T3 PL2126367T3 PL07706234T PL07706234T PL2126367T3 PL 2126367 T3 PL2126367 T3 PL 2126367T3 PL 07706234 T PL07706234 T PL 07706234T PL 07706234 T PL07706234 T PL 07706234T PL 2126367 T3 PL2126367 T3 PL 2126367T3
- Authority
- PL
- Poland
- Prior art keywords
- turbogas
- multistage compressor
- system multistage
- compressor
- turbogas system
- Prior art date
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
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/542—Bladed diffusers
- F04D29/544—Blade shapes
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP07706234.7A EP2126367B1 (en) | 2007-01-17 | 2007-01-17 | Turbogas system multistage compressor |
PCT/IT2007/000035 WO2008087670A1 (en) | 2007-01-17 | 2007-01-17 | Turbogas system multistage compressor |
Publications (1)
Publication Number | Publication Date |
---|---|
PL2126367T3 true PL2126367T3 (pl) | 2014-07-31 |
Family
ID=38120351
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL07706234T PL2126367T3 (pl) | 2007-01-17 | 2007-01-17 | Wielostopniowa sprężarka układu turbogazowego |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP2126367B1 (pl) |
PL (1) | PL2126367T3 (pl) |
WO (1) | WO2008087670A1 (pl) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114962342B (zh) * | 2022-05-27 | 2024-04-02 | 哈尔滨工程大学 | 一种压气机端区振动结构 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4678398A (en) * | 1985-05-08 | 1987-07-07 | The Garrett Corporation | High efficiency transonic mixed-flow compressor method and apparatus |
US5088892A (en) * | 1990-02-07 | 1992-02-18 | United Technologies Corporation | Bowed airfoil for the compression section of a rotary machine |
US5249921A (en) * | 1991-12-23 | 1993-10-05 | General Electric Company | Compressor outlet guide vane support |
US6375419B1 (en) * | 1995-06-02 | 2002-04-23 | United Technologies Corporation | Flow directing element for a turbine engine |
US6439838B1 (en) * | 1999-12-18 | 2002-08-27 | General Electric Company | Periodic stator airfoils |
SE0004001D0 (sv) * | 2000-11-02 | 2000-11-01 | Atlas Copco Tools Ab | Axial flow compressor |
-
2007
- 2007-01-17 EP EP07706234.7A patent/EP2126367B1/en not_active Revoked
- 2007-01-17 PL PL07706234T patent/PL2126367T3/pl unknown
- 2007-01-17 WO PCT/IT2007/000035 patent/WO2008087670A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2008087670A1 (en) | 2008-07-24 |
EP2126367A1 (en) | 2009-12-02 |
EP2126367B1 (en) | 2014-03-12 |
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