RU95102360A - Individual flying vehicle - Google Patents

Individual flying vehicle

Info

Publication number
RU95102360A
RU95102360A RU95102360/11A RU95102360A RU95102360A RU 95102360 A RU95102360 A RU 95102360A RU 95102360/11 A RU95102360/11 A RU 95102360/11A RU 95102360 A RU95102360 A RU 95102360A RU 95102360 A RU95102360 A RU 95102360A
Authority
RU
Russia
Prior art keywords
obstacles
pneumatic
fuselage
vehicle
propellers
Prior art date
Application number
RU95102360/11A
Other languages
Russian (ru)
Other versions
RU2135393C1 (en
Inventor
А.П. Николайчук
В.И. Крылов
В.С. Кондратьев
Ю.К. Желандовский
Original Assignee
А.П. Николайчук
В.И. Крылов
В.С. Кондратьев
Ю.К. Желандовский
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 А.П. Николайчук, В.И. Крылов, В.С. Кондратьев, Ю.К. Желандовский filed Critical А.П. Николайчук
Priority to RU95102360A priority Critical patent/RU2135393C1/en
Publication of RU95102360A publication Critical patent/RU95102360A/en
Application granted granted Critical
Publication of RU2135393C1 publication Critical patent/RU2135393C1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/026—Aircraft not otherwise provided for characterised by special use for use as personal propulsion unit

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Lowering Means (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)

Abstract

FIELD: vertical take-off and landing flying vehicles. SUBSTANCE: disk-shaped fuselage 1 has vertical shafts 6 with propellers 5 and control jets 10. Cabin 12 is located from beneath. Pneumatic motor 7 is mounted rotatably over contour of fuselage 1. Thrust created by propellers 5 raises vehicle and control jets 10 provided for controllability in heading. Pneumatic motor 7 is used to project fuselage 1 in case of collision with obstacles and freely rotating it does not brake the vehicle at contact with obstacles. Two pneumatic motors 7 and 8 projecting from sides make it possible to move in narrow ravines. If pneumatic motors rotate in opposite direction, reaction turning cabin 12 is eliminated and additional force moving the vehicle forward is reduced. EFFECT: high maneuverability and increased cargo capacity at low dead weight.

Claims (1)

Изобретение относится к аппаратам вертикального взлета и посадки и позволяет достичь высокой маневренности, повышенной грузоподъемности при малом собственном весе. Дискообразный корпус 1 имеет вертикальные шахты 6 с воздушными винтами 5 и струйными рулями 10. Снизу расположена кабина 12. По контуру корпуса 1 установлен с возможностью вращения пневмотор 7. Тяга, создаваемая винтами 5, поднимает аппарат вверх, а струйные рули 10 обеспечивают управляемость по курсу (влево-вправо, вперед-назад). Пневмотор 7 предохраняет корпус 1 при столкновениях с препятствиями и, свободно вращаясь, не тормозит при контакте с препятствиями. Два пневмотора 7, 8, выступающие с бортов, позволяют продвигаться, например, в очень узких ущельях. Если пневмоторы 7, 8 принудительно вращаются в разные стороны, то устраняется реакция, разворачивающая кабину 12, и снижается дополнительное усилие, продвигающее аппарат вперед.
Figure 00000001
The invention relates to apparatus for vertical take-off and landing and allows to achieve high maneuverability, increased carrying capacity with low dead weight. The disk-shaped housing 1 has vertical shafts 6 with propellers 5 and jet rudders 10. The cab 12 is located at the bottom. The pneumatic motor 7 is rotatably mounted along the contour of housing 1. (left and right, back and forth). The pneumatic motor 7 protects the housing 1 in a collision with obstacles and, freely rotating, does not slow down in contact with obstacles. Two pneumatic motors 7, 8, protruding from the sides, allow you to move, for example, in very narrow gorges. If the pneumatic motors 7, 8 are forced to rotate in different directions, then the reaction that turns the cab 12 off is eliminated and the additional force that propels the apparatus forward is reduced.
Figure 00000001
RU95102360A 1995-02-17 1995-02-17 Individual flying vehicle RU2135393C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU95102360A RU2135393C1 (en) 1995-02-17 1995-02-17 Individual flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU95102360A RU2135393C1 (en) 1995-02-17 1995-02-17 Individual flying vehicle

Publications (2)

Publication Number Publication Date
RU95102360A true RU95102360A (en) 1996-11-27
RU2135393C1 RU2135393C1 (en) 1999-08-27

Family

ID=20164925

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95102360A RU2135393C1 (en) 1995-02-17 1995-02-17 Individual flying vehicle

Country Status (1)

Country Link
RU (1) RU2135393C1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2006093420A1 (en) * 2005-03-04 2006-09-08 Gnm Limited Propulsion device
NZ538630A (en) 2005-03-04 2007-02-23 Gnm Ltd Propulsion device for a personal flight device with fans rotating in the same direction
CN101108654B (en) * 2007-06-27 2012-04-25 东莞市龙行航空科技有限公司 Double-culvert one-seater vertically taking off and landing flyer
NZ569454A (en) 2008-06-27 2009-10-30 Martin Aircraft Company Ltd Propulsion device including control system
NZ569455A (en) 2008-06-27 2009-10-30 Martin Aircraft Company Ltd Propulsion device incorporating radiator cooling passage
NZ578511A (en) 2009-07-20 2010-12-24 Martin Aircraft Company Ltd Training system
RU2500573C1 (en) * 2012-11-23 2013-12-10 Лариса Константиновна Бородина Disc-shape aircraft driven by air
RU2579381C1 (en) * 2014-11-06 2016-04-10 Андрей Иванович Мерзляков Vertical take-off or landing aircraft
RU2617299C2 (en) * 2015-07-06 2017-04-24 Александр Александрович Скиперский Method of aircraft travel in space "as i want"
RU2734172C1 (en) * 2019-12-24 2020-10-13 Общество с ограниченной ответственностью "ОКБ АВИАРЕШЕНИЯ" (ООО "ОКБ АВИАРЕШЕНИЯ") Helicopter type aircraft engine liquid cooling system

Also Published As

Publication number Publication date
RU2135393C1 (en) 1999-08-27

Similar Documents

Publication Publication Date Title
US9139299B2 (en) Vertical takeoff and landing roadable vehicle
CA2771780C (en) Convertible vehicle for road, air, and water usage
US9254916B2 (en) Vertical take-off and landing aircraft with tiltrotor power for use on land and in air
US4757962A (en) Amphibious vehicle
US11279473B2 (en) STOL aircraft
RU95102360A (en) Individual flying vehicle
KR20120060590A (en) Quadro-Copter with traveling ground
US20210354816A1 (en) Vertical and short takeoff and landing (vstol) aircraft
WO1988000898A1 (en) Heli-hover amphibious aircraft
GB1332197A (en) Air-cushion vehicle
US20020195518A1 (en) Combination fixed and rotating wing aircraft and land vehicle
DE102016002231A9 (en) Aircraft with actively operated swiveling rotors and passive main rotor
DE4217374A1 (en) STOL aircraft with twin fuselage achieving air-cushion effect - has pivotable engine mountings affording choice of conventional flight or utilisation of ground effect for lift
JP6631367B2 (en) Amphibious vehicle
GB1397081A (en) Aircushion-supported vehicles
US10919629B2 (en) Vehicle, system, and method for vertical take-off and landing
US3162260A (en) Vehicle for travelling over land and/or water
RU2125523C1 (en) Multi-functional convertible transport facility
US3721405A (en) Azimuthal propulsion-control system
AU2020100605B4 (en) A vtol-capable airplane having angled propulsors
US2918233A (en) Aerodyne with external flow
RU2093422C1 (en) Vertical takeoff and landing flying vehicle
CN212194977U (en) Electric aerocar and electric aerocar control device
US12017766B2 (en) Flying car
WO2023062690A1 (en) Flight vehicle