RU2018147797A - HELICOPTER - Google Patents

HELICOPTER Download PDF

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Publication number
RU2018147797A
RU2018147797A RU2018147797A RU2018147797A RU2018147797A RU 2018147797 A RU2018147797 A RU 2018147797A RU 2018147797 A RU2018147797 A RU 2018147797A RU 2018147797 A RU2018147797 A RU 2018147797A RU 2018147797 A RU2018147797 A RU 2018147797A
Authority
RU
Russia
Prior art keywords
fuselage
stretch marks
helicopter
engine
attached
Prior art date
Application number
RU2018147797A
Other languages
Russian (ru)
Other versions
RU2018147797A3 (en
RU2742513C2 (en
Inventor
Александр Александрович Горшков
Original Assignee
Александр Александрович Горшков
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 Александр Александрович Горшков filed Critical Александр Александрович Горшков
Priority to RU2018147797A priority Critical patent/RU2742513C2/en
Publication of RU2018147797A publication Critical patent/RU2018147797A/en
Publication of RU2018147797A3 publication Critical patent/RU2018147797A3/ru
Application granted granted Critical
Publication of RU2742513C2 publication Critical patent/RU2742513C2/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/06—Helicopters with single rotor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/52—Tilting of rotor bodily relative to fuselage

Landscapes

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

Claims (3)

1. Вертолет, содержащий соединенный с двигателем несущий винт с машущими лопастями, отличающийся тем, что втулка винта соединена с фюзеляжем посредством стержня, с шарнирами на концах, а также посредством шести растяжек управляемой длины, причем верхние концы указанных растяжек присоединены к не вращающемуся основанию втулки НВ в трех точках, расположенных по треугольнику, охватывающему шарнир крепления указанного стержня, а нижние концы растяжек, аналогичным образом, прикреплены к фюзеляжу.1. A helicopter comprising a rotor connected to the engine with flapping blades, characterized in that the rotor hub is connected to the fuselage by means of a rod, with hinges at the ends, and also through six stretch marks of controlled length, the upper ends of these stretch marks being attached to the non-rotating base of the bush HB at three points located in a triangle covering the hinge of attachment of the specified rod, and the lower ends of the stretch marks, in a similar way, are attached to the fuselage. 2. Вертолет по п. 1, отличающийся тем, что лопасти НВ шарнирно закреплены на силовом кольце, выполняющем функцию приводного вала, а двигатель и редуктор установлены внутри указанного силового кольца.2. The helicopter according to claim 1, characterized in that the HB blades are pivotally mounted on a power ring that acts as a drive shaft, and the engine and gearbox are installed inside the specified power ring. 3. Вертолет по п. 1, отличающийся тем, что он содержит два рулевых винта, с электроприводами и ограждающими кольцами, установленных в хвостовой и носовой частях фюзеляжа.3. The helicopter according to claim 1, characterized in that it contains two tail rotors, with electric drives and enclosing rings installed in the rear and nose of the fuselage.
RU2018147797A 2018-12-29 2018-12-29 Helicopter RU2742513C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2018147797A RU2742513C2 (en) 2018-12-29 2018-12-29 Helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2018147797A RU2742513C2 (en) 2018-12-29 2018-12-29 Helicopter

Publications (3)

Publication Number Publication Date
RU2018147797A true RU2018147797A (en) 2020-06-29
RU2018147797A3 RU2018147797A3 (en) 2021-01-19
RU2742513C2 RU2742513C2 (en) 2021-02-08

Family

ID=71509272

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2018147797A RU2742513C2 (en) 2018-12-29 2018-12-29 Helicopter

Country Status (1)

Country Link
RU (1) RU2742513C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11396370B2 (en) * 2020-03-19 2022-07-26 Textron Innovations Inc. Coaxial rotor systems for VTOL aircraft

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2156208C1 (en) * 1999-04-14 2000-09-20 Любимов Александр Александрович Helicopter column
EA201300193A1 (en) * 2007-11-07 2013-12-30 ХЕЛИСКАНДИА АпС AUTONOMOUS ROTOR SYSTEM FOR AIR AIRCRAFT
RU2533374C1 (en) * 2013-10-01 2014-11-20 Александр Александрович Любимов Helicopter
US10150561B2 (en) * 2016-02-01 2018-12-11 King Fahd University Of Petroleum And Minerals System and method of operation of twin-tiltrotor helicopter
EP3369653B1 (en) * 2017-03-02 2021-12-22 Lockheed Martin Corporation Hinge mechanism for a weight-shifting coaxial helicopter

Also Published As

Publication number Publication date
RU2018147797A3 (en) 2021-01-19
RU2742513C2 (en) 2021-02-08

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