RU2005140463A - TWO-CIRCUIT TURBOREACTIVE ENGINE - Google Patents
TWO-CIRCUIT TURBOREACTIVE ENGINE Download PDFInfo
- Publication number
- RU2005140463A RU2005140463A RU2005140463/06A RU2005140463A RU2005140463A RU 2005140463 A RU2005140463 A RU 2005140463A RU 2005140463/06 A RU2005140463/06 A RU 2005140463/06A RU 2005140463 A RU2005140463 A RU 2005140463A RU 2005140463 A RU2005140463 A RU 2005140463A
- Authority
- RU
- Russia
- Prior art keywords
- inner movable
- nozzle
- movable bodies
- movable housing
- fairing
- Prior art date
Links
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2005140463/06A RU2315887C2 (en) | 2005-12-23 | 2005-12-23 | High by-pass ratio turbojet engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2005140463/06A RU2315887C2 (en) | 2005-12-23 | 2005-12-23 | High by-pass ratio turbojet engine |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2005140463A true RU2005140463A (en) | 2007-06-27 |
RU2315887C2 RU2315887C2 (en) | 2008-01-27 |
Family
ID=38315251
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2005140463/06A RU2315887C2 (en) | 2005-12-23 | 2005-12-23 | High by-pass ratio turbojet engine |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2315887C2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2445490C2 (en) * | 2007-11-06 | 2012-03-20 | Эрбюс Операсьон (Сас) | Method for improving characteristics of double-flow jet turbine engine |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008045072A1 (en) | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Dual function cascade integrated variable area fan nozzle and thrust reverser |
FR2929998B1 (en) * | 2008-04-14 | 2011-08-12 | Aircelle Sa | DOUBLE FLOW TURBOREACTOR NACELLE |
US8695920B2 (en) * | 2008-06-02 | 2014-04-15 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US20140174056A1 (en) | 2008-06-02 | 2014-06-26 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
FR2936222B1 (en) * | 2008-09-24 | 2011-04-01 | Aircelle Sa | NACELLE WITH VARIABLE TUBE SECTION |
FR2949141B1 (en) * | 2009-08-14 | 2011-07-15 | Aircelle Sa | PUSH REVERSING DEVICE |
FR2957979B1 (en) * | 2010-03-25 | 2012-03-30 | Aircelle Sa | PUSH REVERSING DEVICE |
FR2960600B1 (en) * | 2010-06-01 | 2013-10-25 | Aircelle Sa | ACTUATING SYSTEM OF A PUSH REVERSING DEVICE |
FR2960917B1 (en) * | 2010-06-03 | 2012-05-18 | Aircelle Sa | THRUST INVERTER WITH LOCKABLE VARIABLE TUBE SECTION |
FR2978991A1 (en) * | 2011-08-08 | 2013-02-15 | Snecma | THRUST INVERSION DEVICE FOR COMPACT PIPE |
BR102012028749B1 (en) * | 2011-12-21 | 2022-01-18 | United Technologies Corporation | GAS TURBINE ENGINE |
SG11201402663XA (en) * | 2012-01-09 | 2014-09-26 | United Technologies Corp | Gas turbine engine with geared architecture |
FR3007800B1 (en) * | 2013-07-01 | 2017-10-20 | Aircelle Sa | THRUST INVERTER OF A TURBOJET NACELLE COMPRISING PARTIALLY INTEGRATED GRIDS IN HOODS |
-
2005
- 2005-12-23 RU RU2005140463/06A patent/RU2315887C2/en not_active IP Right Cessation
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2445490C2 (en) * | 2007-11-06 | 2012-03-20 | Эрбюс Операсьон (Сас) | Method for improving characteristics of double-flow jet turbine engine |
Also Published As
Publication number | Publication date |
---|---|
RU2315887C2 (en) | 2008-01-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20091224 |