RU2013103120A - HYDROPLANE VERTICAL TAKEOFF AND LANDING AND DEVICE FOR REJECTING THE ENGINE DRAFT VECTOR - Google Patents
HYDROPLANE VERTICAL TAKEOFF AND LANDING AND DEVICE FOR REJECTING THE ENGINE DRAFT VECTOR Download PDFInfo
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- RU2013103120A RU2013103120A RU2013103120/11A RU2013103120A RU2013103120A RU 2013103120 A RU2013103120 A RU 2013103120A RU 2013103120/11 A RU2013103120/11 A RU 2013103120/11A RU 2013103120 A RU2013103120 A RU 2013103120A RU 2013103120 A RU2013103120 A RU 2013103120A
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- engines
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- rejecting
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- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1. Гидросамолет вертикального взлета и посадки, содержащий центроплан, две консоли крыла, силовую установку, фюзеляжи-лодки с встроенными в их конструкцию надувными поплавками и кабинами экипажа, разнесенное вертикальное и горизонтальное оперение, струйные рули, отличающийся тем, что центроплан имеет форму обратного V, а в центре тяжести самолета, в верхней точке V, содержится пакет двигателей с устройством для отклонения вектора тяги.2. Устройство для отклонения вектора тяги, являющееся продолжением выпускного тракта двигателей, отличающееся тем, что выпускной тракт, переходящий в квадратное или прямоугольное сечение, в зависимости от количества двигателей в пакете и направляющий поток газов вниз под углом 90°, образован рядом поворотных направляющих лопаток, где лопатки со стороны выпускного тракта повторяют форму свода, а с другой стороны имеют профиль крыла, при этом нижний срез устройства снабжен рядом поворотных заслонок.1. A seaplane of vertical take-off and landing, comprising a center wing, two wing consoles, a power plant, boat fuselages with inflatable floats and crew cabs integrated in their structure, spaced vertical and horizontal tail units, jet rudders, characterized in that the center wing has the form of a reverse V and in the center of gravity of the aircraft, at the upper point V, contains a package of engines with a device for deviating the thrust vector. 2. A device for rejecting the thrust vector, which is a continuation of the exhaust tract of the engines, characterized in that the exhaust path, turning into a square or rectangular section, depending on the number of engines in the package and directing the gas flow downward at an angle of 90 °, is formed by a series of rotary guide vanes, where the blades on the side of the exhaust tract follow the shape of the arch, and on the other hand they have a wing profile, while the lower section of the device is equipped with a number of rotary dampers.
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Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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RU2013103120/11A RU2549588C2 (en) | 2013-01-23 | 2013-01-23 | Vtol hydroplane and engine thrust vector deflector |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2013103120/11A RU2549588C2 (en) | 2013-01-23 | 2013-01-23 | Vtol hydroplane and engine thrust vector deflector |
Publications (2)
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RU2013103120A true RU2013103120A (en) | 2014-07-27 |
RU2549588C2 RU2549588C2 (en) | 2015-04-27 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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RU2013103120/11A RU2549588C2 (en) | 2013-01-23 | 2013-01-23 | Vtol hydroplane and engine thrust vector deflector |
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RU (1) | RU2549588C2 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2605466C1 (en) * | 2015-09-07 | 2016-12-20 | Закрытое акционерное общество "Институт телекоммуникаций" | Vertical take-off and landing aircraft |
RU2612036C1 (en) * | 2015-12-30 | 2017-03-02 | Илья Александрович Турченко | Aircraft module pulling lifting force |
RU2641359C1 (en) * | 2016-10-12 | 2018-01-17 | Публичное акционерное Общество "Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева" (ПАО "ТАНТК им. Г.М. Бериева") | Jet-propelled amphibious aircraft (hydroaeroplane) |
RU2672539C1 (en) * | 2017-07-07 | 2018-11-15 | Федеральное государственное унитарное предприятие "Сибирский научно-исследовательский институт авиации им. С.А.Чаплыгина" | Vertical take-off and landing aircraft |
RU180623U1 (en) * | 2018-01-25 | 2018-06-19 | Закрытое акционерное общество "Институт телекоммуникаций" | VERTICAL TAKEOFF AND LANDING PLANE |
RU2755561C1 (en) * | 2020-06-25 | 2021-09-17 | Александр Васильевич Горобец | Vertical takeoff and landing seaplane and pneumatic takeoff and landing apparatus |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4301980A (en) * | 1978-12-29 | 1981-11-24 | General Dynamics Corporation | Propulsion system for a V/STOL airplane |
RU2111896C1 (en) * | 1996-09-30 | 1998-05-27 | Петраков Валерий Михайлович | Polyfuselage seaplane |
US6592073B1 (en) * | 2002-02-26 | 2003-07-15 | Leader Industries, Inc. | Amphibious aircraft |
RU27051U1 (en) * | 2002-09-02 | 2003-01-10 | Орестов Игорь Александрович | POWER UNIT WITH CONTROLLED PISTON VECTOR |
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2013
- 2013-01-23 RU RU2013103120/11A patent/RU2549588C2/en active
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Publication number | Publication date |
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RU2549588C2 (en) | 2015-04-27 |
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