RU94013705A - AIRPLATFORM WITH VERTICAL TAKE-OFF AND LANDING - Google Patents

AIRPLATFORM WITH VERTICAL TAKE-OFF AND LANDING

Info

Publication number
RU94013705A
RU94013705A RU94013705/11A RU94013705A RU94013705A RU 94013705 A RU94013705 A RU 94013705A RU 94013705/11 A RU94013705/11 A RU 94013705/11A RU 94013705 A RU94013705 A RU 94013705A RU 94013705 A RU94013705 A RU 94013705A
Authority
RU
Russia
Prior art keywords
aircraft
landing
longitudinal
airplatform
cargo
Prior art date
Application number
RU94013705/11A
Other languages
Russian (ru)
Other versions
RU2090452C1 (en
Inventor
В.Г. Федчишин
Original Assignee
В.Г. Федчишин
Filing date
Publication date
Application filed by В.Г. Федчишин filed Critical В.Г. Федчишин
Priority to RU94013705A priority Critical patent/RU2090452C1/en
Priority claimed from RU94013705A external-priority patent/RU2090452C1/en
Publication of RU94013705A publication Critical patent/RU94013705A/en
Application granted granted Critical
Publication of RU2090452C1 publication Critical patent/RU2090452C1/en

Links

Claims (1)

Изобретение относится к авиастроению и может быть использовано при создании новых типов летательных аппаратов. Цель изобретения - обеспечение грузовым и пассажирским самолетам безаэродромный взлет и посадку, а также осуществление перевозок на незначительные расстояния большого количества пассажиров или крупногабаритных грузов. Цель достигается тем, что разнесенные друг от друга два фюзеляжа сигарообразной формы в местах соединения их с крыльевыми перемычками снабжены горизонтальными циклоидными движителями с утопленными в нишах фюзеляжей их редукторами и расположенными в продольных килевых надстройках дисками, соединяющими концевые цапфы лопастей. Передняя крыльевая перемычка снабжена двумя, а задняя - одними поворотно-выдвижными захватами, а двигатели на случай аварийной остановки одного из них соединены между собой продольными и поперечными валами с закрепленными на их концах разъемными муфтами. 3 з. п. ф-лы, 3 ил.The invention relates to aircraft and can be used to create new types of aircraft. The purpose of the invention is to provide cargo and passenger aircraft with a non-aerodrome take-off and landing, as well as transporting over a short distance a large number of passengers or large-size cargo. The goal is achieved by the fact that two cigar-shaped fuselages separated from each other at their junction points with wing lintels are equipped with horizontal cycloid thrusters with their gearboxes recessed into the fuselage niches and disks located in the longitudinal keel superstructures connecting the end pins of the blades. The front wing liner is equipped with two, and the rear - with one turn-retractable grippers, and the motors in case of an emergency stop of one of them are interconnected by longitudinal and transverse shafts with detachable couplings fixed at their ends. 3 h. n. f-ly, 3 ill.
RU94013705A 1994-04-18 1994-04-18 Aviation platform for vertical takeoff and landing RU2090452C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94013705A RU2090452C1 (en) 1994-04-18 1994-04-18 Aviation platform for vertical takeoff and landing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94013705A RU2090452C1 (en) 1994-04-18 1994-04-18 Aviation platform for vertical takeoff and landing

Publications (2)

Publication Number Publication Date
RU94013705A true RU94013705A (en) 1996-01-10
RU2090452C1 RU2090452C1 (en) 1997-09-20

Family

ID=20154889

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94013705A RU2090452C1 (en) 1994-04-18 1994-04-18 Aviation platform for vertical takeoff and landing

Country Status (1)

Country Link
RU (1) RU2090452C1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2443908C2 (en) * 2008-01-09 2012-02-27 Борис Николаевич Черняев "servid-m" rotary swirl propulsor
RU2473456C1 (en) * 2011-10-05 2013-01-27 Владимир Степанович Григорчук Vertical lift propulsor
RU2506204C1 (en) * 2012-09-20 2014-02-10 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Method of locating high-altitude platform and high-altitude platform
RU2521862C1 (en) * 2012-12-04 2014-07-10 Валерий Николаевич Шарыпов Vertical take-off and landing aircraft
RU2599854C2 (en) * 2014-08-27 2016-10-20 Владимир Александрович Пронин Aircraft with blade devices
RU2686608C1 (en) * 2018-07-05 2019-04-29 Александр Поликарпович Лялин Aerodynamic platform
RU2746025C2 (en) * 2018-11-19 2021-04-06 Александр Александрович Горшков Zero flight aircraft

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