RU2007143755A - GAS TURBINE ENGINE - Google Patents
GAS TURBINE ENGINE Download PDFInfo
- Publication number
- RU2007143755A RU2007143755A RU2007143755/06A RU2007143755A RU2007143755A RU 2007143755 A RU2007143755 A RU 2007143755A RU 2007143755/06 A RU2007143755/06 A RU 2007143755/06A RU 2007143755 A RU2007143755 A RU 2007143755A RU 2007143755 A RU2007143755 A RU 2007143755A
- Authority
- RU
- Russia
- Prior art keywords
- compressor
- gas turbine
- turbine engine
- turbine
- gears
- Prior art date
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 238000002485 combustion reaction Methods 0.000 claims abstract 2
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Газотурбинный двигатель, содержащий входное устройство, компрессор, камеру сгорания, турбину и сопло, отличающийся тем, что содержит независимо вращающиеся в противоположные стороны диски компрессора и турбины, имеющие на ступицах венцы зубчатых колес с внутренним зацеплением, параллельно расположенные валы с шестернями, расположенными между компрессором и турбиной.A gas turbine engine comprising an input device, a compressor, a combustion chamber, a turbine and a nozzle, characterized in that it contains independently rotated in opposite directions compressor disks and turbines having gear wheels with internal gears on the hubs, shafts arranged in parallel with gears located between the compressor and a turbine.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2007143755/06A RU2374467C2 (en) | 2007-11-26 | 2007-11-26 | Gas turbine engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2007143755/06A RU2374467C2 (en) | 2007-11-26 | 2007-11-26 | Gas turbine engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2007143755A true RU2007143755A (en) | 2009-06-10 |
| RU2374467C2 RU2374467C2 (en) | 2009-11-27 |
Family
ID=41024031
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2007143755/06A RU2374467C2 (en) | 2007-11-26 | 2007-11-26 | Gas turbine engine |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2374467C2 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2539315C1 (en) * | 2014-03-18 | 2015-01-20 | Николай Борисович Болотин | Liquid-propellant rocket engine turbopump unit |
| RU2602656C1 (en) * | 2015-11-10 | 2016-11-20 | Николай Борисович Болотин | Return carrier rocket stage, method of its operation and gas turbine engine |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1113542A (en) * | 1967-01-06 | 1968-05-15 | Rolls Royce | Gas turbine engine |
| US3861139A (en) * | 1973-02-12 | 1975-01-21 | Gen Electric | Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition |
| GB2194292A (en) * | 1986-08-29 | 1988-03-02 | Gen Electric | High bypass ratio counterrotating turbofan engine |
| RU2075658C1 (en) * | 1991-01-02 | 1997-03-20 | Акционерное общество открытого типа "Авиадвигатель" | Gas-turbine engine rotor support |
| DE4122008A1 (en) * | 1991-07-03 | 1993-01-14 | Mtu Muenchen Gmbh | GAUGE ENGINE WITH COUNTER-PRESSURE LOW-PRESSURE COMPRESSOR (BOOSTER) |
-
2007
- 2007-11-26 RU RU2007143755/06A patent/RU2374467C2/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| RU2374467C2 (en) | 2009-11-27 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20121127 |