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RU2015135410A - Helicopter vertical take-off - Google Patents

Helicopter vertical take-off Download PDF

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Publication number
RU2015135410A
RU2015135410A RU2015135410A RU2015135410A RU2015135410A RU 2015135410 A RU2015135410 A RU 2015135410A RU 2015135410 A RU2015135410 A RU 2015135410A RU 2015135410 A RU2015135410 A RU 2015135410A RU 2015135410 A RU2015135410 A RU 2015135410A
Authority
RU
Russia
Prior art keywords
aircraft
vertical take
propellers
wings
flight
Prior art date
Application number
RU2015135410A
Other languages
Russian (ru)
Other versions
RU2613074C2 (en
Inventor
Александр Поликарпович Лялин
Original Assignee
Александр Поликарпович Лялин
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 Поликарпович Лялин filed Critical Александр Поликарпович Лялин
Priority to RU2015135410A priority Critical patent/RU2613074C2/en
Publication of RU2015135410A publication Critical patent/RU2015135410A/en
Application granted granted Critical
Publication of RU2613074C2 publication Critical patent/RU2613074C2/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

Landscapes

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

Claims (3)

1. Винтомоторный самолет вертикального взлета, содержащий фюзеляж с крыльями, шасси, винтомоторные установки тянущего типа и средства, обеспечивающие вертикальный взлет, отличающийся тем, что средства, обеспечивающие вертикальный взлет, выполнены в виде воздушных винтов, расположенных с продольным наклоном под крыльями самолета и снабженных катушками, с намотанными на них тросами, свободные концы которых прикреплены к стабилизатору твердотопливной ракеты, и при этом воздушные винты вместе с катушками имеют возможность отделяться от крыльев самолета во время полета.1. A vertical take-off aircraft engine comprising a fuselage with wings, a landing gear, a propeller-type propeller system and vertical take-off means, characterized in that the vertical take-off means are made in the form of propellers arranged with a longitudinal inclination under the wings of the aircraft and equipped with coils with cables wound on them, the free ends of which are attached to the stabilizer of a solid rocket, and the propellers together with the coils can be separated from Flight of the aircraft during the flight. 2. Винтомоторный самолет вертикального взлета по п. 1, отличающийся тем, что твердотопливная ракета находится в тонкостенной трубе, расположенной в передней части фюзеляжа самолета или за его пределами и соосно с центром тяжести самолета.2. A vertical take-off aircraft engine according to claim 1, characterized in that the solid-propellant rocket is located in a thin-walled pipe located in front of the aircraft fuselage or outside and aligned with the center of gravity of the aircraft. 3. Винтомоторный самолет вертикального взлета по п. 1, отличающийся тем, что воздушные винты имеют лопасти с фиксированным углом атаки.3. An aircraft vertical take-off aircraft according to claim 1, characterized in that the propellers have blades with a fixed angle of attack.
RU2015135410A 2015-08-20 2015-08-20 Vertical takeoff propeller aircraft RU2613074C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2015135410A RU2613074C2 (en) 2015-08-20 2015-08-20 Vertical takeoff propeller aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2015135410A RU2613074C2 (en) 2015-08-20 2015-08-20 Vertical takeoff propeller aircraft

Publications (2)

Publication Number Publication Date
RU2015135410A true RU2015135410A (en) 2017-02-22
RU2613074C2 RU2613074C2 (en) 2017-03-15

Family

ID=58453840

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015135410A RU2613074C2 (en) 2015-08-20 2015-08-20 Vertical takeoff propeller aircraft

Country Status (1)

Country Link
RU (1) RU2613074C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2686608C1 (en) * 2018-07-05 2019-04-29 Александр Поликарпович Лялин Aerodynamic platform

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2212358C1 (en) * 2002-12-18 2003-09-20 Макаров Игорь Альбертович Flying vehicle
RU2252177C2 (en) * 2003-05-13 2005-05-20 Гордеев Вениамин Павлович Mode of flying and arrangement for its execution
RU2466061C2 (en) * 2010-01-11 2012-11-10 Николай Иванович Максимов Flight vehicle (versions), flight vehicles parts, method of exploiting flight vehicle and its parts
US20150102175A1 (en) * 2012-11-15 2015-04-16 Aviron Consulting Developmentand Manufacture For Advanced Aviation Fixed winged aircraft with foldable auto-rotation rotor

Also Published As

Publication number Publication date
RU2613074C2 (en) 2017-03-15

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