RU2012147308A - GAS TURBINE ENGINE COMPRESSOR STATOR - Google Patents
GAS TURBINE ENGINE COMPRESSOR STATOR Download PDFInfo
- Publication number
- RU2012147308A RU2012147308A RU2012147308/06A RU2012147308A RU2012147308A RU 2012147308 A RU2012147308 A RU 2012147308A RU 2012147308/06 A RU2012147308/06 A RU 2012147308/06A RU 2012147308 A RU2012147308 A RU 2012147308A RU 2012147308 A RU2012147308 A RU 2012147308A
- Authority
- RU
- Russia
- Prior art keywords
- gas turbine
- turbine engine
- stator
- compressor stator
- compressor
- Prior art date
Links
Abstract
Статор компрессора газотурбинного двигателя, включающий внутренний и наружный корпусы, связанные между собой упругими элементами, отличающийся тем, что внутренний корпус статора компрессора состыкован с диффузором камеры сгорания в осевом направлении с зазором d на стыке, равным 0<d<0,6 мм, при этом во фланце диффузора камеры сгорания в месте стыка с внутренним корпусом статора компрессора выполнены пазы.The stator of a compressor of a gas turbine engine, comprising an inner and an outer casing interconnected by elastic elements, characterized in that the inner casing of the compressor stator is aligned with the diffuser of the combustion chamber in the axial direction with a gap d at the junction equal to 0 <d <0.6 mm, with this in the flange of the diffuser of the combustion chamber at the junction with the inner housing of the compressor stator are grooves.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012147308/06A RU2525384C2 (en) | 2012-11-07 | 2012-11-07 | Gas turbine engine compressor stator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2012147308/06A RU2525384C2 (en) | 2012-11-07 | 2012-11-07 | Gas turbine engine compressor stator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2012147308A true RU2012147308A (en) | 2014-05-20 |
| RU2525384C2 RU2525384C2 (en) | 2014-08-10 |
Family
ID=50695373
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2012147308/06A RU2525384C2 (en) | 2012-11-07 | 2012-11-07 | Gas turbine engine compressor stator |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2525384C2 (en) |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3777489A (en) * | 1972-06-01 | 1973-12-11 | Gen Electric | Combustor casing and concentric air bleed structure |
| RU2241840C2 (en) * | 2002-11-12 | 2004-12-10 | Открытое акционерное общество "Авиадвигатель" | Gas-turbine engine |
| FR2860039B1 (en) * | 2003-09-19 | 2005-11-25 | Snecma Moteurs | REALIZATION OF THE SEAL IN A TURBOJET FOR THE COLLECTION OF DOUBLE-SIDED JOINTS |
| FR2925109B1 (en) * | 2007-12-14 | 2015-05-15 | Snecma | TURBOMACHINE MODULE PROVIDED WITH A DEVICE FOR IMPROVING RADIAL GAMES |
| RU2447325C2 (en) * | 2010-06-21 | 2012-04-10 | Открытое акционерное общество "Авиадвигатель" | Gas turbine engine compressor stator |
-
2012
- 2012-11-07 RU RU2012147308/06A patent/RU2525384C2/en active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2525384C2 (en) | 2014-08-10 |
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| QZ41 | Official registration of changes to a registered agreement (patent) |
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