RU2015136819A - Ekranolet - Google Patents

Ekranolet Download PDF

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Publication number
RU2015136819A
RU2015136819A RU2015136819A RU2015136819A RU2015136819A RU 2015136819 A RU2015136819 A RU 2015136819A RU 2015136819 A RU2015136819 A RU 2015136819A RU 2015136819 A RU2015136819 A RU 2015136819A RU 2015136819 A RU2015136819 A RU 2015136819A
Authority
RU
Russia
Prior art keywords
ekranolet
fuselage
engines
transmission
shaped
Prior art date
Application number
RU2015136819A
Other languages
Russian (ru)
Other versions
RU2612067C1 (en
Inventor
Владимир Васильевич Яковлев
Original Assignee
Федеральное государственное унитарное предприятие "Сибирский научно-исследовательский институт авиации им. С.А. Чаплыгина"
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 Федеральное государственное унитарное предприятие "Сибирский научно-исследовательский институт авиации им. С.А. Чаплыгина" filed Critical Федеральное государственное унитарное предприятие "Сибирский научно-исследовательский институт авиации им. С.А. Чаплыгина"
Priority to RU2015136819A priority Critical patent/RU2612067C1/en
Application granted granted Critical
Publication of RU2612067C1 publication Critical patent/RU2612067C1/en
Publication of RU2015136819A publication Critical patent/RU2015136819A/en

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60V—AIR-CUSHION VEHICLES
    • B60V1/00—Air-cushion
    • B60V1/14—Propulsion; Control thereof

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)

Claims (3)

1. Экранолет, содержащий два фюзеляжа, объединенных общим днищем, с двигателями в каждом фюзеляже, с винтами в кольцевых каналах и трансмиссией от каждого двигателя, поворотную створку, хвостовое оперение коробчатого вида, отличающийся тем, что двигатели экранолета имеют каждый свою трансмиссию, объединенную редуктором общей втулки соосных воздушных винтов в едином кольцевом канале.1. The ekranolet, containing two fuselages, united by a common bottom, with engines in each fuselage, with screws in the annular channels and transmission from each engine, a rotary shutter, a tail unit box-shaped, characterized in that the ekranolet engines have each its own transmission, combined by a gearbox common sleeve coaxial propellers in a single annular channel. 2. Экранолет по п.1, отличающийся тем, что имеет только одну створку, отклоняющую общий поток от соосных винтов под фюзеляж.2. The ekranolet according to claim 1, characterized in that it has only one leaf deflecting the total flow from the coaxial screws under the fuselage. 3. Экранолет по п.1, отличающийся тем, что хвостовое оперение имеет Δ-видную форму с рулями высоты и направления, образующими замкнутый контур, у которого отсутствует эффект концевого перетекания.3. The ekranolet according to claim 1, characterized in that the tail unit is Δ-shaped with elevators and directions that form a closed loop, which does not have the effect of end overflow.
RU2015136819A 2015-08-28 2015-08-28 Surface-effect airborne ship RU2612067C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2015136819A RU2612067C1 (en) 2015-08-28 2015-08-28 Surface-effect airborne ship

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2015136819A RU2612067C1 (en) 2015-08-28 2015-08-28 Surface-effect airborne ship

Publications (2)

Publication Number Publication Date
RU2612067C1 RU2612067C1 (en) 2017-03-02
RU2015136819A true RU2015136819A (en) 2017-03-10

Family

ID=58453928

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015136819A RU2612067C1 (en) 2015-08-28 2015-08-28 Surface-effect airborne ship

Country Status (1)

Country Link
RU (1) RU2612067C1 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4071207A (en) * 1975-09-09 1978-01-31 Piasecki Aircraft Corporation Vertical take-off aircraft
RU2111877C1 (en) * 1996-06-11 1998-05-27 Акционерное общество открытого типа "Нижегородский авиастроительный завод "Сокол" Engine-propulsor plant of dynamic air cushion vehicle
US6719079B2 (en) * 2002-09-17 2004-04-13 William Larry Jones Ground effect vehicle using a frontal ram air stream and aerodynamic lift
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
RU2550568C2 (en) * 2012-07-02 2015-05-10 Владимир Васильевич Яковлев Hovercarft
RU2557631C1 (en) * 2014-02-06 2015-07-27 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Hovercraft

Also Published As

Publication number Publication date
RU2612067C1 (en) 2017-03-02

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20190829