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VTOL aircraft

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VTOL aircraft

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polo, e-mail, 13.06.2011

replacing the traditional mechanical - with reducers, and shaft couplings.

Castle22r, e-mail, 16.06.2008

A truly brilliant invention.

Stingray, e-mail, 25.03.2008

Im sorry, some of the Russian language was still left over in my "cut-and-paste". Here is an even better translation:

In 1954, in the chair of "The construction and design of helicopters Moscow Aviation Institute organized a design team to develop craft-jet transport (aircraft with vertical takeoff and landing). The project is being implemented under the guidance of Academician BN Yuryeva and IP Bratuhina conjunction with the All-Union Electrotechnical Institute, where the director at that time was academician Iosifyants AG.

For the chosen landing force installation of four theatre NK-12MV capacity of 12000 bhp, which were used for Tu-95 bomber. Planned that will be the engine to propel coaxial aerial screws diameter of 6 meters.

Constructors offered komponovochnuyu original scheme off with a vertical arrangement of the fuselage on takeoff and landing. Four theatre located at the ends of the gondola wing cross small elongation (angle between consoles equaled 90 degrees Celsius), the fuselage had a rectangular cross section. It was double the bow cockpit, while the three cargo compartment. Chairs wanted to establish a pivot with the commit to ensure the comfort of the crew and desantnik changing situation in the fuselage takeoff and landing.

The estimated takeoff weight was off 50-60 tons, depending on the flight conditions and a maximum takeoff traction coaxial four screws - 90 tons. The plane carried a vertical take-off, with enough to climb layout (1.2-1.5), and then had to switch to horizontal flight.

Draft SVVP different novelty and originality layout proposed technical solutions. Some of them have been patented. The most important feature of this design has become electric transmission scheme, replacing the traditional mechanical - with reducers, and shaft couplings.

Stingray, e-mail, 25.03.2008

Here is the English translation to the Russian page:

In 1954, in the chair of "The construction and design of helicopters Moscow Aviation Institute organized a design team to develop craft-jet transport (aircraft with vertical takeoff and landing). Проект выполнялся под руководством академика Б.Н.Юрьева и И.П.Братухина совместно с Всесоюзным электротехническим институтом, где директором в то время был академик А.Г.Иосифьянц. The project is being implemented under the guidance of Academician BN Yuryeva and IP Bratuhina conjunction with the All-Union Electrotechnical Institute, where the director at that time was academician Iosifyants AG.

Для СВВП выбрали силовую установку из четырех ТВД НК-12МВ мощностью по 12000лс, которые использовались на бомбардировщике Ту-95. For the chosen landing force installation of four theatre NK-12MV capacity of 12000 bhp, which were used for Tu-95 bomber. Планировалось, что двигатели будут приводить в движение соосные воздушные винты диаметром 6 метров. Planned that will be the engine to propel coaxial aerial screws diameter of 6 meters.

Конструкторы предложили оригинальную компоновочную схему СВВП с вертикальным расположением фюзеляжа на взлете и посадке. Constructors offered komponovochnuyu original scheme off with a vertical arrangement of the fuselage on takeoff and landing. Четыре ТВД располагались в гондолах на концах крестообразного крыла малого удлинения (угол между консолями равнялся 90 градусам), фюзеляж имел прямоугольное сечение. Four theatre located at the ends of the gondola wing cross small elongation (angle between consoles equaled 90 degrees Celsius), the fuselage had a rectangular cross section. В его носовой части находилась двухместная кабина экипажа, а за ней три грузовых отсека. It was double the bow cockpit, while the three cargo compartment. Кресла хотели установить на шарнирах с фиксацией, чтобы обеспечить комфортность экипажу и десантникам при изменении положения фюзеляжа в процессе взлета и посадки. Chairs wanted to establish a pivot with the commit to ensure the comfort of the crew and desantnik changing situation in the fuselage takeoff and landing.

Расчетная взлетная масса СВВП составляла 50-60 тонн в зависимости от условий полета, а максимальная взлетная тяга четырех соосных винтов — 90 тонн. The estimated takeoff weight was off 50-60 tons, depending on the flight conditions and a maximum takeoff traction coaxial four screws - 90 tons. Самолет совершал вертикальный взлет, имея достаточную для набора высоты тяговооруженность (1.2-1.5), а затем должен был перейти к горизонтальному полету. The plane carried a vertical take-off, with enough to climb layout (1.2-1.5), and then had to switch to horizontal flight.

Проект СВВП отличался оригинальностью компоновки и новизной предлагаемых технических решений. Draft SVVP different novelty and originality layout proposed technical solutions. Некоторые из них были запатентованы. Some of them have been patented. Важнейшей особенностью этой разработки стала электрическая схема трансмиссии, заменившая традиционную механическую — с редукторами, валами и муфтами. The most important feature of this design has become electric transmission scheme, replacing the traditional mechanical - with reducers, and shaft couplings.

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