RU2016117705A - Vertical takeoff and landing airplane - Google Patents

Vertical takeoff and landing airplane Download PDF

Info

Publication number
RU2016117705A
RU2016117705A RU2016117705A RU2016117705A RU2016117705A RU 2016117705 A RU2016117705 A RU 2016117705A RU 2016117705 A RU2016117705 A RU 2016117705A RU 2016117705 A RU2016117705 A RU 2016117705A RU 2016117705 A RU2016117705 A RU 2016117705A
Authority
RU
Russia
Prior art keywords
aircraft
elementary
landing
vertical take
propulsion device
Prior art date
Application number
RU2016117705A
Other languages
Russian (ru)
Inventor
Петр Геннадьевич Поздняков
Original Assignee
Петр Геннадьевич Поздняков
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 Петр Геннадьевич Поздняков filed Critical Петр Геннадьевич Поздняков
Priority to RU2016117705A priority Critical patent/RU2016117705A/en
Publication of RU2016117705A publication Critical patent/RU2016117705A/en

Links

Landscapes

  • Toys (AREA)
  • Transmission Devices (AREA)

Claims (4)

1. Самолет вертикального взлета и посадки, содержащий крыло, консоли, центроплан, шасси, отличающийся тем, что снабжен комплексным движителем, расположенным вблизи центра масс, который представляет собой матрицу элементарных движителей, воздушных винтов, приводимых в движение электродвигателями, смонтированными на раме с подвесом и приводом, позволяющим поворачивать комплексный движитель, по меньшей мере, в одной плоскости относительно корпуса СВВП, причем управление вектором тяги осуществляется как за счет поворота рамы, так и за счет индивидуального управления тягой винтов комплексного движителя.1. Aircraft of vertical take-off and landing, comprising a wing, consoles, center wing, landing gear, characterized in that it is equipped with a complex propulsion device located near the center of mass, which is a matrix of elementary propulsion devices, propellers driven by electric motors mounted on a frame with a suspension and a drive that allows you to rotate the complex mover in at least one plane relative to the VTOL casing, and the thrust vector is controlled both by rotating the frame and by ndividualnogo control integrated propulsor thrust screws. 2. Самолет вертикального взлета и посадки по п. 1, отличающийся тем, что элементарный движитель представляет собой сборку из двух и более соосно расположенных воздушных винтов, приводимых в движение электродвигателями.2. Aircraft of vertical take-off and landing according to claim 1, characterized in that the elementary mover is an assembly of two or more coaxially located propellers driven by electric motors. 3. Самолет вертикального взлета и посадки по п. 1, отличающийся тем, что воздушный винт элементарного движителя оснащен автоматом перекоса.3. Aircraft of vertical take-off and landing according to claim 1, characterized in that the propeller of the elementary propulsion device is equipped with a swash plate. 4. Самолет вертикального взлета и посадки по п. 1, отличающийся тем, что воздушный винт элементарного движителя оснащен механизмом изменения шага винта.4. Aircraft of vertical take-off and landing according to claim 1, characterized in that the propeller of the elementary propulsion device is equipped with a mechanism for changing the pitch of the screw.
RU2016117705A 2016-05-04 2016-05-04 Vertical takeoff and landing airplane RU2016117705A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2016117705A RU2016117705A (en) 2016-05-04 2016-05-04 Vertical takeoff and landing airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2016117705A RU2016117705A (en) 2016-05-04 2016-05-04 Vertical takeoff and landing airplane

Publications (1)

Publication Number Publication Date
RU2016117705A true RU2016117705A (en) 2017-11-14

Family

ID=60328250

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2016117705A RU2016117705A (en) 2016-05-04 2016-05-04 Vertical takeoff and landing airplane

Country Status (1)

Country Link
RU (1) RU2016117705A (en)

Similar Documents

Publication Publication Date Title
RU2020110832A (en) Tilt control system for electric aircraft with vertical take-off and landing (VTOL)
RU2016120302A (en) FULFILLED WITH VERTICAL TAKEOFF Aircraft
WO2017210595A3 (en) Vertical take-off and landing (vtol) winged air vehicle with complementary angled rotors
RU2724006C1 (en) Aircraft
WO2017107720A1 (en) Multirotor manned aerial vehicle
RU2016102944A (en) Vertical take-off aircraft
RU2014107956A (en) VERTICAL RETAINING VEHICLE WITH VERTICAL TAKEOFF
CN204223182U (en) Civilian depopulated helicopter rotor controls tilting frame actuating device
RU2013141179A (en) AIRCRAFT
WO2011152614A3 (en) Bottom-adjustable propeller-type flying object
KR101755278B1 (en) Vertical takeoff and landing unmanned aerial vehicle having fixed wing, equipped with hybrid propeller system
WO2018106137A3 (en) Distributed electric propulsion system and vertical take-off and landing aircraft
CN104290904A (en) Multi-rotor type aircraft
EP3368413B1 (en) Air vehicle and method and apparatus for control thereof
US10421540B1 (en) Tiltrotor aircraft having optimized hover capabilities
CN104477381A (en) Double-variable-pitch-propeller aircraft
CA3052416A1 (en) Device and method for improving the pitch control of a fixed-wing aircraft in stall/post-stall regime
RU2638221C2 (en) Vertical take-off and landing aircraft and method to control its flight
RU2017131255A (en) Aeromechanical method of controlling the configuration and flight mode of a convertible aircraft (convertiplane)
KR101621210B1 (en) Tilt-Cube-In-Wing Unmanned Aerial Vehicle
RU157967U1 (en) AIR ENGINE WITH VARIABLE DRIVING VECTOR
CN204507258U (en) A kind of many rotor unmanned aircrafts
RU2016117705A (en) Vertical takeoff and landing airplane
RU179060U1 (en) Unmanned aerial vehicle vertical takeoff and landing
CN204124363U (en) A kind of multi-rotor aerocraft

Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20180205