RU2000125037A - GAS TURBINE ENGINE COMPRESSOR STATOR - Google Patents
GAS TURBINE ENGINE COMPRESSOR STATORInfo
- Publication number
- RU2000125037A RU2000125037A RU2000125037/06A RU2000125037A RU2000125037A RU 2000125037 A RU2000125037 A RU 2000125037A RU 2000125037/06 A RU2000125037/06 A RU 2000125037/06A RU 2000125037 A RU2000125037 A RU 2000125037A RU 2000125037 A RU2000125037 A RU 2000125037A
- Authority
- RU
- Russia
- Prior art keywords
- gas turbine
- turbine engine
- compressor stator
- engine compressor
- casing
- Prior art date
Links
- 210000003746 Feathers Anatomy 0.000 claims 1
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2000125037/06A RU2186257C2 (en) | 2000-10-03 | 2000-10-03 | Compressor stator of gas turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2000125037/06A RU2186257C2 (en) | 2000-10-03 | 2000-10-03 | Compressor stator of gas turbine engine |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2186257C2 RU2186257C2 (en) | 2002-07-27 |
RU2000125037A true RU2000125037A (en) | 2002-09-10 |
Family
ID=20240636
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2000125037/06A RU2186257C2 (en) | 2000-10-03 | 2000-10-03 | Compressor stator of gas turbine engine |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2186257C2 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2941018B1 (en) * | 2009-01-09 | 2011-02-11 | Snecma | A VARIABLE CALIPER FOR A RECTIFIER STAGE, COMPRISING A NON-CIRCULAR INTERNAL PLATFORM |
RU2600479C1 (en) * | 2015-05-12 | 2016-10-20 | Открытое акционерное общество "Авиадвигатель" | High-pressure compressor of gas turbine engine |
-
2000
- 2000-10-03 RU RU2000125037/06A patent/RU2186257C2/en active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE60044228D1 (en) | Compressor rotor configuration | |
EP1382799A3 (en) | Gas turbine engine casing and rotor blade arrangement | |
EP1262634A3 (en) | Integral nozzle and shroud | |
RU2003131385A (en) | HOUSING, COMPRESSOR, TURBINE AND GAS-TURBINE ENGINE CONTAINING THIS HOUSING | |
CA2333809A1 (en) | Convex compressor casing | |
DE60007775D1 (en) | AXIAL FAN | |
GB2367028B (en) | Gas turbine engine rotor blades | |
EP0353498A3 (en) | Compressor diaphragm assembly | |
EP1225308A3 (en) | Split ring for gas turbine casing | |
EP1312756A3 (en) | Blade for turbine engine | |
KR920006615A (en) | Structure of compressor case | |
DE50111153D1 (en) | stator | |
WO2005059312A3 (en) | Turbomachine, especially a gas turbine | |
DE3876768D1 (en) | AXIAL FLOWED BLADE BLADES FOR COMPRESSORS OR TURBINES. | |
RU2000125037A (en) | GAS TURBINE ENGINE COMPRESSOR STATOR | |
RU2003133996A (en) | STEAM TURBINE | |
ATE403066T1 (en) | AIR MOTOR | |
KR100359611B1 (en) | Air foil bearing | |
RU96100268A (en) | GAS TURBINE ENGINE | |
RU2001122208A (en) | GAS TURBINE ENGINE COMPRESSOR STATOR | |
RU2003124326A (en) | GAS TURBINE ENGINE COMPRESSOR STATOR | |
RU2001103476A (en) | AXIAL COMPRESSOR | |
RU2001112386A (en) | GAS TURBINE ENGINE | |
RU96112049A (en) | AXIAL TURBO MACHINE | |
RU2001131062A (en) | Axial compressor stage of a gas turbine engine |