RU2017113842A - Rotorcraft - Google Patents

Rotorcraft Download PDF

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Publication number
RU2017113842A
RU2017113842A RU2017113842A RU2017113842A RU2017113842A RU 2017113842 A RU2017113842 A RU 2017113842A RU 2017113842 A RU2017113842 A RU 2017113842A RU 2017113842 A RU2017113842 A RU 2017113842A RU 2017113842 A RU2017113842 A RU 2017113842A
Authority
RU
Russia
Prior art keywords
rotor
coaxial rotor
stabilizer
wing
coaxial
Prior art date
Application number
RU2017113842A
Other languages
Russian (ru)
Other versions
RU2017113842A3 (en
RU2673754C2 (en
Inventor
Евгений Петрович Юриков
Владимир Иванович Андреев
Original Assignee
Евгений Петрович Юриков
Владимир Иванович Андреев
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 Евгений Петрович Юриков, Владимир Иванович Андреев filed Critical Евгений Петрович Юриков
Priority to RU2017113842A priority Critical patent/RU2673754C2/en
Publication of RU2017113842A3 publication Critical patent/RU2017113842A3/ru
Publication of RU2017113842A publication Critical patent/RU2017113842A/en
Application granted granted Critical
Publication of RU2673754C2 publication Critical patent/RU2673754C2/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Claims (1)

Скоростной винтокрыл с увеличенной дальностью полета, содержащий соосный несущий винт, фюзеляж, силовую установку, редуктор, крылья, стабилизатор, шасси, систему управления, отличающийся тем, что крыло замкнутое, расположено вблизи центра тяжести, под соосным несущим винтом, стабилизатор с управляемыми газодинамическими и механическими рулями, соосный несущий винт авторотирующий автожирный; силовая установка с дополнительным воздушным компрессором, с тянущими маршевыми ВРД, с мотор-генератором; с устройством синхронизации перевода несущего винта с режима работы по вертолетному в режим работы по самолетному и обратно.High-speed rotary wing with increased flight range, containing a coaxial rotor, fuselage, power unit, gearbox, wings, stabilizer, landing gear, control system, characterized in that the wing is closed, located near the center of gravity, under the coaxial rotor, a stabilizer with controlled gas-dynamic and mechanical rudders, coaxial rotor autorotating autogyro; a power plant with an additional air compressor, with pulling mid-flight propulsion engines, with a motor generator; with a synchronization device for transferring the rotor from the helicopter mode of operation to the airplane mode of operation and vice versa.
RU2017113842A 2017-04-20 2017-04-20 Rotary-wing aircraft RU2673754C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2017113842A RU2673754C2 (en) 2017-04-20 2017-04-20 Rotary-wing aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2017113842A RU2673754C2 (en) 2017-04-20 2017-04-20 Rotary-wing aircraft

Publications (3)

Publication Number Publication Date
RU2017113842A3 RU2017113842A3 (en) 2018-10-23
RU2017113842A true RU2017113842A (en) 2018-10-23
RU2673754C2 RU2673754C2 (en) 2018-11-29

Family

ID=63923150

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2017113842A RU2673754C2 (en) 2017-04-20 2017-04-20 Rotary-wing aircraft

Country Status (1)

Country Link
RU (1) RU2673754C2 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU96358U1 (en) * 2010-01-22 2010-07-27 Владимир Анатольевич Мымрин SHORT TAKEOFF AND LANDING ROTARY AIRCRAFT
FR2976912B1 (en) * 2011-06-24 2014-02-21 Eurocopter France AIRCRAFT WITH ROTARY BOAT AND FIXED BOAT.
RU130951U1 (en) * 2013-03-05 2013-08-10 Григорий Иванович Кузнецов RUNWING AIRCRAFT WITH AUTOMOTIVE ROLLING SCREW AND WING
DE202013011072U1 (en) * 2013-12-06 2014-01-27 Maximilian Salbaum tilt rotor aircraft

Also Published As

Publication number Publication date
RU2017113842A3 (en) 2018-10-23
RU2673754C2 (en) 2018-11-29

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Legal Events

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

Effective date: 20200421