RU2014106059A - SCREEN PLAN - Google Patents

SCREEN PLAN Download PDF

Info

Publication number
RU2014106059A
RU2014106059A RU2014106059/11A RU2014106059A RU2014106059A RU 2014106059 A RU2014106059 A RU 2014106059A RU 2014106059/11 A RU2014106059/11 A RU 2014106059/11A RU 2014106059 A RU2014106059 A RU 2014106059A RU 2014106059 A RU2014106059 A RU 2014106059A
Authority
RU
Russia
Prior art keywords
wings
propellers
reduce
engines
fuselage
Prior art date
Application number
RU2014106059/11A
Other languages
Russian (ru)
Other versions
RU2646776C2 (en
Inventor
Владимир Петрович Толстоухов
Original Assignee
Владимир Петрович Толстоухов
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 Владимир Петрович Толстоухов filed Critical Владимир Петрович Толстоухов
Priority to RU2014106059A priority Critical patent/RU2646776C2/en
Publication of RU2014106059A publication Critical patent/RU2014106059A/en
Application granted granted Critical
Publication of RU2646776C2 publication Critical patent/RU2646776C2/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60V—AIR-CUSHION VEHICLES
    • B60V1/00—Air-cushion
    • B60V1/08—Air-cushion wherein the cushion is created during forward movement of the vehicle by ram effect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/08—Aircraft not otherwise provided for having multiple wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)

Abstract

Экраноплан, включающий фюзеляж, шасси, вертикальное оперение, крылья, двигатели, отличающийся тем, что для сокращения длины разбега, снижения скорости выхода на полет в экранном режиме и увеличения высоты полета на этом режиме крылья установлены на фюзеляже по схеме ″биплан-тандем″, на верхних крыльях установлены движители - воздушные винты, размещенные в аэродинамических кольцах, причем на головных крыльях и следующих за ними движители установлены наклонно, хвостовой маршевый движитель установлен горизонтально, в плоскостях нижних (экранирующих) крыльев размещены воздушные винты, связанные валами с соответствующими двигателями, а на верхней и нижней поверхностях крыльев выполнены каналы для прохождения воздушных потоков.Wing, including the fuselage, landing gear, vertical tail, wings, engines, characterized in that to reduce the take-off run, reduce the flight speed in screen mode and increase flight altitude in this mode, the wings are mounted on the fuselage according to the ″ biplane-tandem ″ scheme propellers are installed on the upper wings - propellers located in the aerodynamic rings, moreover, the head wings and the following propellers are mounted obliquely, the tail propulsion is mounted horizontally in the lower planes Wounding) wings are placed propellers connected by shafts to the respective engines, and channels for the passage of air flows are made on the upper and lower surfaces of the wings.

Claims (1)

Экраноплан, включающий фюзеляж, шасси, вертикальное оперение, крылья, двигатели, отличающийся тем, что для сокращения длины разбега, снижения скорости выхода на полет в экранном режиме и увеличения высоты полета на этом режиме крылья установлены на фюзеляже по схеме ″биплан-тандем″, на верхних крыльях установлены движители - воздушные винты, размещенные в аэродинамических кольцах, причем на головных крыльях и следующих за ними движители установлены наклонно, хвостовой маршевый движитель установлен горизонтально, в плоскостях нижних (экранирующих) крыльев размещены воздушные винты, связанные валами с соответствующими двигателями, а на верхней и нижней поверхностях крыльев выполнены каналы для прохождения воздушных потоков. Wing, including the fuselage, landing gear, vertical tail, wings, engines, characterized in that to reduce the take-off run, reduce the flight speed in screen mode and increase flight altitude in this mode, the wings are mounted on the fuselage according to the ″ biplane-tandem ″ scheme propellers are installed on the upper wings - propellers located in the aerodynamic rings, moreover, the head wings and the following propellers are mounted obliquely, the tail propulsion is mounted horizontally in the lower planes Wounding) wings are placed propellers connected by shafts to the respective engines, and channels for the passage of air flows are made on the upper and lower surfaces of the wings.
RU2014106059A 2014-02-18 2014-02-18 Ekranoplan RU2646776C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2014106059A RU2646776C2 (en) 2014-02-18 2014-02-18 Ekranoplan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2014106059A RU2646776C2 (en) 2014-02-18 2014-02-18 Ekranoplan

Publications (2)

Publication Number Publication Date
RU2014106059A true RU2014106059A (en) 2015-08-27
RU2646776C2 RU2646776C2 (en) 2018-03-07

Family

ID=54015331

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014106059A RU2646776C2 (en) 2014-02-18 2014-02-18 Ekranoplan

Country Status (1)

Country Link
RU (1) RU2646776C2 (en)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA995717A (en) * 1972-04-14 1976-08-24 Frank S. Malvestuto (Jr.) High speed water vessel
US3856238A (en) * 1972-04-14 1974-12-24 F Malvestuto Aircraft transporter
RU2211773C1 (en) * 2003-02-18 2003-09-10 Ишков Юрий Григорьевич Wing-in-ground-effect craft-amphibia on air cushion
DE102009004239A1 (en) * 2009-01-05 2010-07-08 Ivan Novikov-Kopp Method for the complex increase of aerodynamic and transport properties, ground effect vehicle for carrying out the method (variants) and flight method
WO2012026838A1 (en) * 2010-08-26 2012-03-01 Shulim Semenovich Shvidler Airplane

Also Published As

Publication number Publication date
RU2646776C2 (en) 2018-03-07

Similar Documents

Publication Publication Date Title
WO2015143093A3 (en) Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades
EA201300348A1 (en) TRANSFORMABLE AIRCRAFT VERTICAL TAKEOFF AND LANDING WITH A TURNING WING
EA201491528A1 (en) AERIAL VERTICAL TAKE-OFF AIRCRAFT AND LANDING WITH TWO WING DESIGNS
WO2016053739A3 (en) Nose attitude control of a rotary wing aircraft
UA106677C2 (en) INTEGRAL AERODYNAMIC COMPONENT PLANE
CN103847954B (en) Telescopic wing
WO2017123346A3 (en) Uav with wing-plate assemblies providing efficient vertical takeoff and landing capability
WO2015143098A3 (en) Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades
RU2013103120A (en) HYDROPLANE VERTICAL TAKEOFF AND LANDING AND DEVICE FOR REJECTING THE ENGINE DRAFT VECTOR
RU2014119525A (en) HELICOPTER - A SPEED HELICOPTER AIRCRAFT
RU2013115878A (en) METHOD FOR MANAGING, STABILIZING AND CREATING AN ADDITIONAL AIRCRAFT LIFTING POWER
RU2014106059A (en) SCREEN PLAN
CN203032936U (en) Passenger helicopter
EA201700013A1 (en) AIRCRAFT VERTICAL TAKE-OFF AND LANDING
RU2015130267A (en) UNMANNED AERIAL VERTICAL OR SHORT TAKEOFF AND LANDING (OPTIONS)
RU2579381C1 (en) Vertical take-off or landing aircraft
RU167275U1 (en) AIRCRAFT
CN104554734A (en) Jet-propelled helicopter
RU145288U1 (en) AIRCRAFT
EA201100731A1 (en) METHOD OF IMPLEMENTING THE TAKEOFF WITHOUT CUTTING OR LITTING WITHOUT RUN OF A CONVERTOPLAN
RU2016116178A (en) METHOD OF VERTICAL MOVEMENT AND SUSPENSION OF AIRPLANE IN AIR
RU168888U1 (en) Aircraft
RU2015149094A (en) Application of a method of flight with asymmetric thrust for landing an aircraft in crosswind
RU2015135410A (en) Helicopter vertical take-off
PL414124A1 (en) Vertical takeoff and landing aircraft

Legal Events

Date Code Title Description
FA93 Acknowledgement of application withdrawn (no request for examination)

Effective date: 20170220

FZ9A Application not withdrawn (correction of the notice of withdrawal)

Effective date: 20170504