RU2012140156A - ENGINE INSTALLATION WITH ELECTROMECHANICAL DRIVE OF SCREWS OF THE AIRCRAFT - Google Patents

ENGINE INSTALLATION WITH ELECTROMECHANICAL DRIVE OF SCREWS OF THE AIRCRAFT Download PDF

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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
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RU
Russia
Prior art keywords
aircraft
electromechanical drive
screws
electric motor
engine installation
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Application number
RU2012140156/11A
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Russian (ru)
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RU2542842C2 (en
Inventor
Евгений Иванович Смирнов
Андрей Евгеньевич Смирнов
Original Assignee
Евгений Иванович Смирнов
Андрей Евгеньевич Смирнов
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Application filed by Евгений Иванович Смирнов, Андрей Евгеньевич Смирнов filed Critical Евгений Иванович Смирнов
Priority to RU2012140156/11A priority Critical patent/RU2542842C2/en
Publication of RU2012140156A publication Critical patent/RU2012140156A/en
Application granted granted Critical
Publication of RU2542842C2 publication Critical patent/RU2542842C2/en

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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)

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.
RU2012140156/11A 2012-09-20 2012-09-20 Aircraft electromechanical power plant RU2542842C2 (en)

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)

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RU2012140156A true RU2012140156A (en) 2014-03-27
RU2542842C2 RU2542842C2 (en) 2015-02-27

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RU2012140156/11A RU2542842C2 (en) 2012-09-20 2012-09-20 Aircraft electromechanical power plant

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Families Citing this family (1)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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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RU2542842C2 (en) 2015-02-27

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20150207