WO2015094020A3 - Convertiplane with reactive rotor drive, which is controlled by rotors by means of swash plates, via control levers, and which does not require additional control means - Google Patents

Convertiplane with reactive rotor drive, which is controlled by rotors by means of swash plates, via control levers, and which does not require additional control means Download PDF

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Publication number
WO2015094020A3
WO2015094020A3 PCT/RU2014/000955 RU2014000955W WO2015094020A3 WO 2015094020 A3 WO2015094020 A3 WO 2015094020A3 RU 2014000955 W RU2014000955 W RU 2014000955W WO 2015094020 A3 WO2015094020 A3 WO 2015094020A3
Authority
WO
WIPO (PCT)
Prior art keywords
rotors
convertiplane
controlled
require additional
rotor drive
Prior art date
Application number
PCT/RU2014/000955
Other languages
French (fr)
Russian (ru)
Other versions
WO2015094020A2 (en
Inventor
Андрей Геннадьевич БОРМОТОВ
Иван Александрович ОШКУКОВ
Original Assignee
Андрей Геннадьевич БОРМОТОВ
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 Андрей Геннадьевич БОРМОТОВ filed Critical Андрей Геннадьевич БОРМОТОВ
Publication of WO2015094020A2 publication Critical patent/WO2015094020A2/en
Publication of WO2015094020A3 publication Critical patent/WO2015094020A3/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)

Abstract

The invention relates to transport engineering, and more particularly to convertiplanes having lifting rotors, similar to side-by-side rotor helicopters, for vertical take-off and landing and for airplane flight once the aircraft is converted. The entire aircraft is controlled by the rotors of the convertiplane by means of a helicopter-type swash plate, without the need for additional devices such as elevators, ailerons, rudders and other aerodynamic devices and mechanisms.
PCT/RU2014/000955 2013-12-20 2014-12-17 Convertiplane with reactive rotor drive, which is controlled by rotors by means of swash plates, via control levers, and which does not require additional control means WO2015094020A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2013156785/11A RU2570241C2 (en) 2013-12-20 2013-12-20 Convertiplane with rotors jet drive controlled by rotors via wobble plate and control levers with no extra control means
RU2013156785 2013-12-20

Publications (2)

Publication Number Publication Date
WO2015094020A2 WO2015094020A2 (en) 2015-06-25
WO2015094020A3 true WO2015094020A3 (en) 2015-08-13

Family

ID=53403854

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2014/000955 WO2015094020A2 (en) 2013-12-20 2014-12-17 Convertiplane with reactive rotor drive, which is controlled by rotors by means of swash plates, via control levers, and which does not require additional control means

Country Status (2)

Country Link
RU (1) RU2570241C2 (en)
WO (1) WO2015094020A2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107336833B (en) * 2017-07-05 2023-10-31 天津凤凰智能科技有限公司 Composite unmanned aerial vehicle and control method
RU2771513C2 (en) * 2017-08-24 2022-05-05 Игорь Викторович Лентов Combined method for control of aircraft
RU183800U1 (en) * 2018-04-19 2018-10-02 Юрий Иванович Безруков ROPE WING BEZRUKOV
RU2705743C1 (en) * 2018-11-08 2019-11-11 Дмитрий Васильевич Плешков Convertiplane
CN110217389A (en) * 2019-06-19 2019-09-10 中国人民解放军空军工程大学 A kind of coaxial double-rotary wing unmanned plane that vector verts

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1593A1 (en) * 1925-01-31 1926-08-31 Ф.В. Дробышев Airplane-Helicopter
US5839691A (en) * 1996-05-22 1998-11-24 Lariviere; Jean Soulez Vertical takeoff and landing aircraft
RU2182100C2 (en) * 2000-01-05 2002-05-10 Пивоваров Вячеслав Иванович Rotor
US7275711B1 (en) * 2004-02-23 2007-10-02 Kenneth Warren Flanigan Gas-powered tip-jet-driven compound VTOL aircraft

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2132289C1 (en) * 1996-10-24 1999-06-27 Клименко Алексей Геннадьевич Vertical take-off and landing flying vehicle
RU2211155C2 (en) * 2000-11-16 2003-08-27 Общество с ограниченной ответственностью Научно-Производственное Предприятие "ТЕХНОКРАТ" Aeromobile
RU2310583C2 (en) * 2005-11-15 2007-11-20 Д.С. Дуров Amphibious convertible helicopter

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1593A1 (en) * 1925-01-31 1926-08-31 Ф.В. Дробышев Airplane-Helicopter
US5839691A (en) * 1996-05-22 1998-11-24 Lariviere; Jean Soulez Vertical takeoff and landing aircraft
RU2182100C2 (en) * 2000-01-05 2002-05-10 Пивоваров Вячеслав Иванович Rotor
US7275711B1 (en) * 2004-02-23 2007-10-02 Kenneth Warren Flanigan Gas-powered tip-jet-driven compound VTOL aircraft

Also Published As

Publication number Publication date
RU2570241C2 (en) 2015-12-10
WO2015094020A2 (en) 2015-06-25
RU2013156785A (en) 2015-06-27

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