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https://gitea.msk.dinamika-avia.ru/Constanta-Design/MI-38.git
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230 lines
4.3 KiB
Plaintext
230 lines
4.3 KiB
Plaintext
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Ограничения по центровкам
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filename pics/14.svg
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\begin_layout Plain Layout
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\begin_inset Caption Standard
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\begin_layout Plain Layout
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Схема координатных осей вертолета для расчетов центровки
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\end_layout
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\end_inset
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\end_inset
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\end_layout
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\begin_layout Standard
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Начало координат - центр втулки несущего винта (ВНВ
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status open
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name "fn:ВНВ"
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Втулка несущего винта
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literal "false"
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), т.е.
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точка пересечения оси вала НВ
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с плоскостью осей горизонтальных шарниров ВНВ
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reference "fn:ВНВ"
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plural "false"
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\end_inset
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\end_layout
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\end_inset
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.
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Ось X перпендикулярна оси несущего винта, лежит в продольной плоскости
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симметрии вертолета (вперед - плюс, назад - минус).
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Ось У - ось вала несущего винта (вверх - плюс, вниз - минус).
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Поперечная ось Z - перпендикулярна плоскости осей X и У (вправо - плюс,
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влево - минус).
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\end_layout
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\begin_layout Standard
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Информация базируется на док.
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1.
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\end_layout
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\begin_layout Standard
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placement H
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wide false
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sideways false
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status open
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\align center
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\begin_inset Graphics
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filename pics/15.svg
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\end_inset
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\begin_layout Plain Layout
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\begin_inset Caption Standard
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\begin_layout Plain Layout
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Области допустимых масс и продольных центровок вертолета
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\end_layout
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\end_inset
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\end_layout
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\end_inset
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\end_layout
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\end_body
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\end_document
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