RU2012120529A - SINGLE HELICOPTER - Google Patents

SINGLE HELICOPTER Download PDF

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Publication number
RU2012120529A
RU2012120529A RU2012120529/11A RU2012120529A RU2012120529A RU 2012120529 A RU2012120529 A RU 2012120529A RU 2012120529/11 A RU2012120529/11 A RU 2012120529/11A RU 2012120529 A RU2012120529 A RU 2012120529A RU 2012120529 A RU2012120529 A RU 2012120529A
Authority
RU
Russia
Prior art keywords
controls
helicopter
rotors
frame
nodes
Prior art date
Application number
RU2012120529/11A
Other languages
Russian (ru)
Other versions
RU2507120C2 (en
Inventor
Боян Фаисович Ахметшин
Original Assignee
Боян Фаисович Ахметшин
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Боян Фаисович Ахметшин filed Critical Боян Фаисович Ахметшин
Priority to RU2012120529/11A priority Critical patent/RU2507120C2/en
Publication of RU2012120529A publication Critical patent/RU2012120529A/en
Application granted granted Critical
Publication of RU2507120C2 publication Critical patent/RU2507120C2/en

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Abstract

Одноместный вертолет,содержащий трубчатый каркас, в нижней части которого располагается силовая установка с узлами и механизмами, необходимыми для передачи и распределения крутящего момента через валы на пару соосных воздушных несущих винтов, противоположного направления вращения, расположенных в верхней части вертолета, над которыми, соединенная с каркасом, располагается кабина пилота с органами управления и контроля, отличающийся тем, что его вертикальные габариты превышают диаметр несущих винтов более чем в полтора раза, а его центр тяжести, смещенный книзу, находится при полной загрузке аппарата не выше трети его вертикального размера.Single helicopter containing a tubular frame, in the lower part of which there is a power plant with the nodes and mechanisms necessary for transmitting and distributing torque through the shafts to a pair of coaxial rotor rotors, of the opposite direction of rotation, located in the upper part of the helicopter, over which, connected to frame, there is a cockpit with controls and controls, characterized in that its vertical dimensions exceed the diameter of the rotors by more than one and a half times, and its price p gravity biased downwardly, is loaded vehicle apparatus not higher than a third of its vertical size.

Claims (1)

Одноместный вертолет, содержащий трубчатый каркас, в нижней части которого располагается силовая установка с узлами и механизмами, необходимыми для передачи и распределения крутящего момента через валы на пару соосных воздушных несущих винтов, противоположного направления вращения, расположенных в верхней части вертолета, над которыми, соединенная с каркасом, располагается кабина пилота с органами управления и контроля, отличающийся тем, что его вертикальные габариты превышают диаметр несущих винтов более чем в полтора раза, а его центр тяжести, смещенный книзу, находится при полной загрузке аппарата не выше трети его вертикального размера. Single helicopter containing a tubular frame, in the lower part of which there is a power plant with the nodes and mechanisms necessary for transmitting and distributing torque through the shafts to a pair of coaxial rotor rotors, of the opposite direction of rotation, located in the upper part of the helicopter, over which, connected to the frame, is located cockpit with controls and controls, characterized in that its vertical dimensions exceed the diameter of the rotors by more than one and a half times, and its center of gravity, offset bottom, is fully loaded vehicle not exceeding one third of its vertical dimension.
RU2012120529/11A 2012-05-17 2012-05-17 Single-seat helicopter RU2507120C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2012120529/11A RU2507120C2 (en) 2012-05-17 2012-05-17 Single-seat helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2012120529/11A RU2507120C2 (en) 2012-05-17 2012-05-17 Single-seat helicopter

Publications (2)

Publication Number Publication Date
RU2012120529A true RU2012120529A (en) 2013-11-27
RU2507120C2 RU2507120C2 (en) 2014-02-20

Family

ID=49624892

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2012120529/11A RU2507120C2 (en) 2012-05-17 2012-05-17 Single-seat helicopter

Country Status (1)

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RU (1) RU2507120C2 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7032861B2 (en) * 2002-01-07 2006-04-25 Sanders Jr John K Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors
RU2314972C2 (en) * 2005-05-03 2008-01-20 Алексей Александрович Анищенко Helicopter
US7631834B1 (en) * 2006-02-24 2009-12-15 Stealth Robotics, Llc Aerial robot with dispensable conductive filament
GB2460441A (en) * 2008-05-30 2009-12-02 Gilo Ind Ltd Flying machine

Also Published As

Publication number Publication date
RU2507120C2 (en) 2014-02-20

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Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20150518

BF4A Cancelling a publication of earlier date [patents]

Free format text: PUBLICATION IN JOURNAL SHOULD BE CANCELLED

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

Effective date: 20180518