RU97112726A - VERTICAL TAKEOFF AND LANDING AIRCRAFT - Google Patents

VERTICAL TAKEOFF AND LANDING AIRCRAFT

Info

Publication number
RU97112726A
RU97112726A RU97112726/28A RU97112726A RU97112726A RU 97112726 A RU97112726 A RU 97112726A RU 97112726/28 A RU97112726/28 A RU 97112726/28A RU 97112726 A RU97112726 A RU 97112726A RU 97112726 A RU97112726 A RU 97112726A
Authority
RU
Russia
Prior art keywords
engines
landing
aircraft
fuselage
wings
Prior art date
Application number
RU97112726/28A
Other languages
Russian (ru)
Other versions
RU2132289C1 (en
Inventor
А.Г. Клименко
Original Assignee
А.Г. Клименко
Filing date
Publication date
Application filed by А.Г. Клименко filed Critical А.Г. Клименко
Publication of RU97112726A publication Critical patent/RU97112726A/en
Application granted granted Critical
Publication of RU2132289C1 publication Critical patent/RU2132289C1/en

Links

Claims (1)

Летательный аппарат с вертикальным взлетом и посадкой, включающий в свою конструкцию: фюзеляж с кабиной пилотов и пассажиров, цельноповоротное вертикальное и горизонтальное оперения, два крыла с двигателями и шасси на консолях, жестко связанные центропланом, который выполнен с возможностью поворота вокруг поперечной оси самолета, отличающийся тем, что крылья выполнены в виде пилонов, на которых размещены мотогондолы с двигателями (оснащенными винтами, применяемыми на самолетах с обычной схемой взлета и посадки) и основные шасси, при этом крылья, двигатели и шасси жестко связаны с центропланом, имеющим возможность поворота вокруг поперечной оси самолета на угол 90-120o; центроплан выполнен из двух лонжеронов: переднего и заднего, между которыми выполнено окно, причем передний лонжерон имеет форму цилиндра, проходит внутри фюзеляжа и является осью вращения центроплана с установленными на нем двигателями и шасси, а задний лонжерон заключен в обтекатель, с возможностью уборки в специальную нишу, выполненную в нижней части фюзеляжа, шасси установлено таким образом, что имеет возможность автоматически становиться по полету в самолетном режиме полета.Aircraft with vertical take-off and landing, including in its design: a fuselage with a cockpit for passengers and passengers, a fully rotatable vertical and horizontal tail, two wings with engines and a landing gear on consoles, rigidly connected by a center wing, which is made to rotate around the transverse axis of the aircraft, characterized the fact that the wings are made in the form of pylons on which engine nacelles with engines (equipped with propellers used on planes with the usual take-off and landing pattern) and main landing gears are placed, while m wings, engines and landing gear are rigidly connected to the center wing, which can rotate around the transverse axis of the aircraft at an angle of 90-120 o ; the center wing is made of two spars: the front and rear, between which the window is made, and the front side member has the shape of a cylinder, passes inside the fuselage and is the axis of rotation of the center section with engines and chassis mounted on it, and the rear side member is enclosed in a fairing, with the possibility of cleaning in a special a niche made in the lower part of the fuselage, the chassis is installed in such a way that it can automatically become in flight in airplane mode of flight.
RU97112726A 1996-10-24 1997-07-25 Vertical take-off and landing flying vehicle RU2132289C1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
UA96104035 1996-10-24
UA96104035 1996-10-24

Publications (2)

Publication Number Publication Date
RU97112726A true RU97112726A (en) 1999-06-10
RU2132289C1 RU2132289C1 (en) 1999-06-27

Family

ID=21689156

Family Applications (1)

Application Number Title Priority Date Filing Date
RU97112726A RU2132289C1 (en) 1996-10-24 1997-07-25 Vertical take-off and landing flying vehicle

Country Status (1)

Country Link
RU (1) RU2132289C1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2484279C1 (en) * 2011-12-19 2013-06-10 Николай Евгеньевич Староверов Method for improving braking efficiency of aircraft during ground rolling and increasing safety at takeoff and landing, and device for its implementation
RU2495796C1 (en) * 2012-04-18 2013-10-20 Валерий Туркубеевич Пчентлешев Aircraft
CN102632994B (en) * 2012-05-05 2014-07-09 扬州大学 Tilt rotor aircraft
RU2570241C2 (en) * 2013-12-20 2015-12-10 Андрей Геннадьевич Бормотов Convertiplane with rotors jet drive controlled by rotors via wobble plate and control levers with no extra control means
WO2015138217A1 (en) 2014-03-13 2015-09-17 Endurant Systems, Llc Uav configurations and battery augmentation for uav internal combustion engines, and associated systems and methods
CN105035319A (en) * 2015-07-27 2015-11-11 江阴市翔诺电子科技有限公司 Novel vertical take-off and landing air vehicle and control method thereof
US9821909B2 (en) * 2016-04-05 2017-11-21 Swift Engineering, Inc. Rotating wing assemblies for tailsitter aircraft
CN105667781A (en) * 2016-04-06 2016-06-15 南京航空航天大学 Aircraft capable of changing layout between rotor wing and fixed wing
US10421540B1 (en) * 2017-03-02 2019-09-24 Bell Textron Inc. Tiltrotor aircraft having optimized hover capabilities
US20200079492A1 (en) 2018-09-11 2020-03-12 Swift Engineering, Inc. Systems and methods for aerodynamic deployment of wing structures
WO2020190223A1 (en) * 2019-03-21 2020-09-24 Acikel Guerkan Vtol tilting fuselage winged frame multirotor aircraft

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