RU2008110287A - VERTICAL TAKEOFF AND LANDING AIRCRAFT ENGINE - Google Patents
VERTICAL TAKEOFF AND LANDING AIRCRAFT ENGINE Download PDFInfo
- Publication number
- RU2008110287A RU2008110287A RU2008110287/06A RU2008110287A RU2008110287A RU 2008110287 A RU2008110287 A RU 2008110287A RU 2008110287/06 A RU2008110287/06 A RU 2008110287/06A RU 2008110287 A RU2008110287 A RU 2008110287A RU 2008110287 A RU2008110287 A RU 2008110287A
- Authority
- RU
- Russia
- Prior art keywords
- engine
- outer casing
- engine according
- turbocompressors
- impellers
- Prior art date
Links
- NAGRVUXEKKZNHT-UHFFFAOYSA-N Imazosulfuron Chemical compound COC1=CC(OC)=NC(NC(=O)NS(=O)(=O)C=2N3C=CC=CC3=NC=2Cl)=N1 NAGRVUXEKKZNHT-UHFFFAOYSA-N 0.000 title 1
- 238000002485 combustion reaction Methods 0.000 claims abstract 4
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1. Двигатель самолета вертикального взлета и посадки, содержащий турбокомпрессор с корпусом, компрессором, камерой сгорания, выход из которой соединен газовым трактом с турбиной, и реактивное сопло, отличающийся тем, двигатель выполнен биротативным с двумя турбокомпрессорами, содержащими, в свою очередь, валы с рабочими колесами компрессоров и рабочими колесами турбин. ! 2. Двигатель по п.1, отличающийся тем, что концентрично валам турбокомпрессоров выполнен внешний корпус. ! 3. Двигатель по 2, отличающийся тем, что реактивное сопло соединено с внешним корпусом. ! 4. Двигатель по п.1, или 2, или 3, отличающийся тем, что камера сгорания прикреплена к внешнему корпусу.1. The engine of an airplane of vertical take-off and landing, comprising a turbocompressor with a housing, a compressor, a combustion chamber, the outlet of which is connected by a gas path to the turbine, and a jet nozzle, characterized in that the engine is made biotic with two turbocompressors, which in turn contain shafts with impellers of compressors and impellers of turbines. ! 2. The engine according to claim 1, characterized in that the outer casing is made concentrically to the shafts of the turbocompressors. ! 3. The engine according to claim 2, characterized in that the jet nozzle is connected to the outer casing. ! 4. The engine according to claim 1, or 2, or 3, characterized in that the combustion chamber is attached to the outer casing.
Claims (4)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008110287/06A RU2008110287A (en) | 2008-03-17 | 2008-03-17 | VERTICAL TAKEOFF AND LANDING AIRCRAFT ENGINE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008110287/06A RU2008110287A (en) | 2008-03-17 | 2008-03-17 | VERTICAL TAKEOFF AND LANDING AIRCRAFT ENGINE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2008110287A true RU2008110287A (en) | 2009-09-27 |
Family
ID=41168924
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008110287/06A RU2008110287A (en) | 2008-03-17 | 2008-03-17 | VERTICAL TAKEOFF AND LANDING AIRCRAFT ENGINE |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2008110287A (en) |
-
2008
- 2008-03-17 RU RU2008110287/06A patent/RU2008110287A/en not_active Application Discontinuation
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FA92 | Acknowledgement of application withdrawn (lack of supplementary materials submitted) |
Effective date: 20090922 |