RU2012140156A - ENGINE INSTALLATION WITH ELECTROMECHANICAL DRIVE OF SCREWS OF THE AIRCRAFT - Google Patents
ENGINE INSTALLATION WITH ELECTROMECHANICAL DRIVE OF SCREWS OF THE AIRCRAFT Download PDFInfo
- Publication number
- RU2012140156A RU2012140156A RU2012140156/11A RU2012140156A RU2012140156A RU 2012140156 A RU2012140156 A RU 2012140156A RU 2012140156/11 A RU2012140156/11 A RU 2012140156/11A RU 2012140156 A RU2012140156 A RU 2012140156A RU 2012140156 A RU2012140156 A RU 2012140156A
- Authority
- RU
- Russia
- Prior art keywords
- aircraft
- electromechanical drive
- screws
- electric motor
- engine installation
- Prior art date
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- Engine Equipment That Uses Special Cycles (AREA)
- Transmission Devices (AREA)
Abstract
Двигательная установка, состоящая из группы винтов с электромеханическим приводом их от электродвигателя большой мощности, создающего через редуктор крутящий момент винтов, питающаяся от электроэнергетической установки с одним приводным двигателем, отличающаяся от аналогов наличием электродвигателя вместо двигателя внутреннего сгорания, а также совместным применением тяговых и подъемных винтов для движения воздушного судна.A propulsion system consisting of a group of propellers with an electromechanical drive from a large electric motor that generates propeller torque through a gearbox, powered by an electric power plant with one drive motor, different from analogues by the presence of an electric motor instead of an internal combustion engine, as well as the combined use of traction and lifting screws for the movement of the aircraft.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2012140156/11A RU2542842C2 (en) | 2012-09-20 | 2012-09-20 | Aircraft electromechanical power plant |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2012140156/11A RU2542842C2 (en) | 2012-09-20 | 2012-09-20 | Aircraft electromechanical power plant |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2012140156A true RU2012140156A (en) | 2014-03-27 |
RU2542842C2 RU2542842C2 (en) | 2015-02-27 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2012140156/11A RU2542842C2 (en) | 2012-09-20 | 2012-09-20 | Aircraft electromechanical power plant |
Country Status (1)
Country | Link |
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RU (1) | RU2542842C2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RO131684A0 (en) * | 2016-09-27 | 2017-02-28 | Liviu Grigorian Giurca | Vertical take-off and landing aircrafts |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7198223B2 (en) * | 2001-02-14 | 2007-04-03 | Airscooter Corporation | Ultralight coaxial rotor aircraft |
FR2916418B1 (en) * | 2007-05-22 | 2009-08-28 | Eurocopter France | FAST HYBRID HELICOPTER WITH EXTENDABLE HIGH DISTANCE. |
RU2407675C1 (en) * | 2009-05-22 | 2010-12-27 | Открытое акционерное общество "Камов" | Tandem-rotor helicopter |
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2012
- 2012-09-20 RU RU2012140156/11A patent/RU2542842C2/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
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RU2542842C2 (en) | 2015-02-27 |
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Legal Events
Date | Code | Title | Description |
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MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20150207 |