UA83820C2 - AERODYNAMIC CRAFT and its takeoff and landing assembly - Google Patents
AERODYNAMIC CRAFT and its takeoff and landing assemblyInfo
- 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
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.
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)
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 |
-
2005
- 2005-09-13 UA UAA200508723A patent/UA83820C2/en unknown
- 2005-11-22 RU RU2005136319/11A patent/RU2337022C2/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
RU2337022C2 (en) | 2008-10-27 |
RU2005136319A (en) | 2007-06-10 |
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