RU2453473C2 - Vertical take-off and landing aircraft-aeromobile - Google Patents
Vertical take-off and landing aircraft-aeromobile Download PDFInfo
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- RU2453473C2 RU2453473C2 RU2007135611/11A RU2007135611A RU2453473C2 RU 2453473 C2 RU2453473 C2 RU 2453473C2 RU 2007135611/11 A RU2007135611/11 A RU 2007135611/11A RU 2007135611 A RU2007135611 A RU 2007135611A RU 2453473 C2 RU2453473 C2 RU 2453473C2
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- fuselage
- wing
- landing
- vertical take
- landing aircraft
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Abstract
Description
Изобретение относится к широкофюзеляжным самолетам короткого взлета и посадки.The invention relates to wide-body aircraft for short take-off and landing.
Известны широкофюзеляжные самолеты, в которых фюзеляж имеет поперечное сечение в виде круга или даже яйцеобразный, острием вверх, например Боинг-747, /http://photobox.ru/ [1], и не создает подъемной силы, а является только нагрузкой на несущее крыло. Для взлета и посадки таких самолетов требуется аэродром длиной несколько километров, а движители выполняют, в основном, роль «тяни - толкай».Wide-body airplanes are known in which the fuselage has a cross section in the form of a circle or even an egg-shaped one, with its tip pointing upwards, for example, a Boeing 747, / http://hothotox.ru/ [1], and does not create lifting force, but is only a load on the carrier wing. For the take-off and landing of such aircraft, an airfield of several kilometers is required, and the propulsors perform mainly the “push-push” role.
Задача изобретения - сокращение разбега и пробега самолета и повышение его аэродинамического качества.The objective of the invention is to reduce the takeoff and run of the aircraft and increase its aerodynamic quality.
Решение задачи осуществляется за счет включения фюзеляжа в создание подъемной силы и за счет интенсивного обдува щелевого крыла еще на старте воздушным потоком от движителей, которые создают тягу с помощью пропеллеров, винтовентиляторов или реактивной струи. Для чего фюзеляж выполнен несущим, удобообтекаемым, преимущественно, каплеобразным в плане и с продольным профилем в виде крыла, с координатами всех точек поверхности фюзеляжа на линиях вращения (второго порядка), а щелевое крыло установлено с возможностью его обдува напорной струей от движителей, что обеспечивает короткий взлет и посадку, а также высокие аэродинамические характеристики самолета.The solution to the problem is due to the inclusion of the fuselage in the creation of lifting force and due to intensive blowing of the slotted wing even at the start of the air stream from propulsors that create traction using propellers, propeller fans or a jet stream. For this, the fuselage is made of a bearing, streamlined, mainly droplet in plan and with a longitudinal profile in the form of a wing, with the coordinates of all points of the surface of the fuselage on the lines of rotation (second order), and a slotted wing is installed with the possibility of blowing it with a pressure jet from propulsors, which ensures short take-off and landing, as well as high aerodynamic characteristics of the aircraft.
На фиг.1 - показан общий вид самолета короткого взлета и посадки, на фиг.2 - вид сверху, на фиг.3 - вид сбоку, на фиг.4 - вид спереди, на фиг.5 - вид сзади.Figure 1 - shows a General view of the aircraft short take-off and landing, figure 2 is a top view, figure 3 is a side view, figure 4 is a front view, figure 5 is a rear view.
Обозначены: 1 - фюзеляж, 2 - щелевое крыло, 3 - винтовентилятор, 4 - двигатель, 5 - элевоны, 6 - хвостовое оперение.Designated: 1 - fuselage, 2 - slot wing, 3 - propeller fan, 4 - engine, 5 - elevons, 6 - tail.
Самолет короткого взлета и посадки имеет фюзеляж 1, который выполнен несущим, удобообтекаемым, преимущественно каплеобразным в плане и с продольным профилем в виде крыла, с координатами всех точек поверхности фюзеляжа на линиях вращения (второго порядка), а щелевое крыло 2 установлено с возможностью его обдува напорной струей от движителей 3, 4.The short take-off and landing aircraft has a fuselage 1, which is made of a bearing, streamlined, mainly drop-shaped in plan and with a longitudinal profile in the form of a wing, with the coordinates of all points of the surface of the fuselage on the rotation lines (second order), and a slotted
Включение фюзеляжа в создание подъемной силы и интенсивный обдув щелевого крыла мощным потоком воздуха от движителей обеспечивают короткий взлет и посадку и высокие аэродинамические характеристики самолета.The inclusion of the fuselage in the creation of lifting force and intensive blowing of the slot wing with a powerful stream of air from the propulsors provide a short take-off and landing and high aerodynamic characteristics of the aircraft.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2007135611/11A RU2453473C2 (en) | 2007-09-25 | 2007-09-25 | Vertical take-off and landing aircraft-aeromobile |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2007135611/11A RU2453473C2 (en) | 2007-09-25 | 2007-09-25 | Vertical take-off and landing aircraft-aeromobile |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2007135611A RU2007135611A (en) | 2009-03-27 |
RU2453473C2 true RU2453473C2 (en) | 2012-06-20 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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RU2007135611/11A RU2453473C2 (en) | 2007-09-25 | 2007-09-25 | Vertical take-off and landing aircraft-aeromobile |
Country Status (1)
Country | Link |
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RU (1) | RU2453473C2 (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB467670A (en) * | 1935-12-14 | 1937-06-14 | Alexander Davidson Garden | Improvements in aircraft |
RU2174484C2 (en) * | 1999-06-29 | 2001-10-10 | Безруков Юрий Иванович | Vertical take-off and landing aircraft - disk-type flying vehicle |
RU2282560C2 (en) * | 2004-11-19 | 2006-08-27 | Карклин Андрей Михайлович | Aircraft with lifting fuselage |
RU2302976C1 (en) * | 2006-03-24 | 2007-07-20 | Вячеслав Петрович Кондратьев | Light aircraft |
-
2007
- 2007-09-25 RU RU2007135611/11A patent/RU2453473C2/en not_active IP Right Cessation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB467670A (en) * | 1935-12-14 | 1937-06-14 | Alexander Davidson Garden | Improvements in aircraft |
RU2174484C2 (en) * | 1999-06-29 | 2001-10-10 | Безруков Юрий Иванович | Vertical take-off and landing aircraft - disk-type flying vehicle |
RU2282560C2 (en) * | 2004-11-19 | 2006-08-27 | Карклин Андрей Михайлович | Aircraft with lifting fuselage |
RU2302976C1 (en) * | 2006-03-24 | 2007-07-20 | Вячеслав Петрович Кондратьев | Light aircraft |
Also Published As
Publication number | Publication date |
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RU2007135611A (en) | 2009-03-27 |
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Date | Code | Title | Description |
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MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20150926 |