RU2008150966A - AIRCRAFT - Google Patents
AIRCRAFT Download PDFInfo
- Publication number
- RU2008150966A RU2008150966A RU2008150966/11A RU2008150966A RU2008150966A RU 2008150966 A RU2008150966 A RU 2008150966A RU 2008150966/11 A RU2008150966/11 A RU 2008150966/11A RU 2008150966 A RU2008150966 A RU 2008150966A RU 2008150966 A RU2008150966 A RU 2008150966A
- Authority
- RU
- Russia
- Prior art keywords
- rotation
- engine
- axis
- flywheels
- rotor
- Prior art date
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- Gear Transmission (AREA)
Abstract
Летательный аппарат содержит корпус, главный инерционный двигатель и дополнительный инерционный двигатель, каждый инерционный двигатель содержит роторы, оси вращения которых параллельны или расположены на одной прямой, и привод, содержащий двигатель и механическую передачу, соединяющую двигатель с роторами, на каждом роторе установлены маховики, ось вращения которых перпендикулярна оси вращения ротора, и механическая передача, содержащая конические шестерни, маховики соединены с шестернями с горизонтальной осью вращения, а центральная шестерня с вертикальной осью неподвижная и соединена с корпусом. The aircraft contains a hull, a main inertial engine and an additional inertial engine, each inertial engine contains rotors whose rotation axes are parallel or located on one straight line, and a drive containing a motor and a mechanical transmission connecting the engine to the rotors, flywheels are installed on each rotor, axis rotation of which is perpendicular to the axis of rotation of the rotor, and a mechanical transmission containing bevel gears, flywheels are connected to gears with a horizontal axis of rotation, and the central Single gear with vertical axis fixed and connected to the housing.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008150966/11A RU2008150966A (en) | 2008-12-22 | 2008-12-22 | AIRCRAFT |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008150966/11A RU2008150966A (en) | 2008-12-22 | 2008-12-22 | AIRCRAFT |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2008150966A true RU2008150966A (en) | 2010-06-27 |
Family
ID=42683223
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008150966/11A RU2008150966A (en) | 2008-12-22 | 2008-12-22 | AIRCRAFT |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2008150966A (en) |
-
2008
- 2008-12-22 RU RU2008150966/11A patent/RU2008150966A/en not_active Application Discontinuation
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FA93 | Acknowledgement of application withdrawn (no request for examination) |
Effective date: 20111223 |