UA83820C2 - AERODYNAMIC CRAFT and its takeoff and landing assembly - Google Patents

AERODYNAMIC CRAFT and its takeoff and landing assembly

Info

Publication number
UA83820C2
UA83820C2 UAA200508723A UAA200508723A UA83820C2 UA 83820 C2 UA83820 C2 UA 83820C2 UA A200508723 A UAA200508723 A UA A200508723A UA A200508723 A UAA200508723 A UA A200508723A UA 83820 C2 UA83820 C2 UA 83820C2
Authority
UA
Ukraine
Prior art keywords
wing
center
section
craft
air
Prior art date
Application number
UAA200508723A
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Геннадий Алексеевич Павлов
Original Assignee
Геннадий Алексеевич Павлов
Вакулин Владимир Михайлович
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 Геннадий Алексеевич Павлов, Вакулин Владимир Михайлович filed Critical Геннадий Алексеевич Павлов
Priority to UAA200508723A priority Critical patent/UA83820C2/en
Priority to RU2005136319/11A priority patent/RU2337022C2/en
Publication of UA83820C2 publication Critical patent/UA83820C2/en

Links

Landscapes

  • Toys (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention relates to transportation facilities on dynamic air cushion, in particular to the wing-in-ground effect crafts. An aerodynamic craft has a fuselage and a wing, which consists of center section and arrow-shaped consoles installed with positive dihedral angle. Consoles are isolated from the center section by floaters. Horizontal tail assembly is installed above vertical tail assembly. Power plant has pusher propellers arranged in the ring nozzles. Floaters have stern top lugs, to which the consoles with hanging ailerons are pinned. Center wing section can have S-shaped aerodynamic profile, negative dihedral angle and negative sweepback on the trailing edge. The housing of wing-in-ground effect craft can be made with possibility of assembling and disassembling during operation into separate units. The takeoff and landing assembly of wing-in-ground effect craft includes floaters on the boards of center wing section, enclosure of static air cushion from the front and wing flap from behind of center wing section, which are retracted. Air conduit in the dorsal fin removes a part of the air flow from the propellers into the space under center wing section. Air intake device has rotary folds, which are made in the form of parts of side planking of dorsal fin and provide for opening or closing the inlets of air conduit of the supercharging of static air cushion. Rotary folds on the lower surface of center wing section provide for opening or closing the outlets of said air conduit. Synchronizing device for installation and retraction of the enclosure of static air cushion with turning of the folds of inlets and outlets of air conduit of supercharging is provided.
UAA200508723A 2005-09-13 2005-09-13 AERODYNAMIC CRAFT and its takeoff and landing assembly UA83820C2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
UAA200508723A UA83820C2 (en) 2005-09-13 2005-09-13 AERODYNAMIC CRAFT and its takeoff and landing assembly
RU2005136319/11A RU2337022C2 (en) 2005-09-13 2005-11-22 Hovercraft and its alighting gear

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAA200508723A UA83820C2 (en) 2005-09-13 2005-09-13 AERODYNAMIC CRAFT and its takeoff and landing assembly

Publications (1)

Publication Number Publication Date
UA83820C2 true UA83820C2 (en) 2008-08-26

Family

ID=38311977

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA200508723A UA83820C2 (en) 2005-09-13 2005-09-13 AERODYNAMIC CRAFT and its takeoff and landing assembly

Country Status (2)

Country Link
RU (1) RU2337022C2 (en)
UA (1) UA83820C2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
RU2471660C2 (en) * 2011-02-11 2013-01-10 Общество С Ограниченной Ответственностью "Экранопланостроительное Объединение "Орион" Hovercraft
RU2466888C1 (en) * 2011-05-10 2012-11-20 Общество С Ограниченной Ответственностью "Экранопланостроительное Объединение "Орион" Hovercraft
RU2581511C1 (en) * 2014-10-24 2016-04-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Московский авиационный институт (национальный исследовательский университет)" (МАИ) Hovercraft

Also Published As

Publication number Publication date
RU2337022C2 (en) 2008-10-27
RU2005136319A (en) 2007-06-10

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