RU2006110656A - GAS TURBINE ENGINE - Google Patents
GAS TURBINE ENGINE Download PDFInfo
- Publication number
- RU2006110656A RU2006110656A RU2006110656/06A RU2006110656A RU2006110656A RU 2006110656 A RU2006110656 A RU 2006110656A RU 2006110656/06 A RU2006110656/06 A RU 2006110656/06A RU 2006110656 A RU2006110656 A RU 2006110656A RU 2006110656 A RU2006110656 A RU 2006110656A
- Authority
- RU
- Russia
- Prior art keywords
- air
- cooling air
- output
- nozzle
- pressure compressor
- Prior art date
Links
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2006110656/06A RU2316662C1 (en) | 2006-04-03 | 2006-04-03 | Gas-turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2006110656/06A RU2316662C1 (en) | 2006-04-03 | 2006-04-03 | Gas-turbine engine |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2006110656A true RU2006110656A (en) | 2007-10-10 |
RU2316662C1 RU2316662C1 (en) | 2008-02-10 |
Family
ID=38952604
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2006110656/06A RU2316662C1 (en) | 2006-04-03 | 2006-04-03 | Gas-turbine engine |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2316662C1 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2634373A1 (en) * | 2012-02-28 | 2013-09-04 | Siemens Aktiengesellschaft | Arrangement for a turbomachine |
RU2500895C1 (en) * | 2012-04-24 | 2013-12-10 | Николай Борисович Болотин | Gas turbine engine turbine |
RU2499894C1 (en) * | 2012-05-11 | 2013-11-27 | Николай Борисович Болотин | Bypass gas turbine engine |
RU2506435C2 (en) * | 2012-05-11 | 2014-02-10 | Николай Борисович Болотин | Gas turbine engine and method for radial clearance adjustment in gas turbine |
RU2501956C1 (en) * | 2012-07-31 | 2013-12-20 | Николай Борисович Болотин | Bypass gas turbine engine, method of radial gap adjustment in turbine of bypass gas turbine engine |
RU2519127C1 (en) * | 2013-04-24 | 2014-06-10 | Николай Борисович Болотин | Turbine of gas turbine engine and method for adjustment of radial clearance in turbine |
RU2553919C2 (en) * | 2013-05-27 | 2015-06-20 | Николай Борисович Болотин | Gas-turbine engine |
RU2525049C1 (en) * | 2013-06-04 | 2014-08-10 | Открытое акционерное общество "Авиадвигатель" | High temperature gas turbine engine |
RU2567890C1 (en) * | 2014-06-02 | 2015-11-10 | Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) | Gas turbine engine |
-
2006
- 2006-04-03 RU RU2006110656/06A patent/RU2316662C1/en active
Also Published As
Publication number | Publication date |
---|---|
RU2316662C1 (en) | 2008-02-10 |
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Legal Events
Date | Code | Title | Description |
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QB4A | Licence on use of patent |
Effective date: 20101007 |
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QZ41 | Official registration of changes to a registered agreement (patent) |
Free format text: LICENCE FORMERLY AGREED ON 20101007 Effective date: 20110826 |
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PD4A | Correction of name of patent owner |