Конструирование агрегатов самолета

54 1 2 1 1 0 1 1 2 1 2 2 2 2 2 4 2 2 2 2 4 3 3 2 2 3 1, 5 400 1, 5 0, 5 200 1, 5 1, 5 2 0, 5 150 H; 1 2 1 3 150 Н ; 2 2 2 3 1, 5 200 1, 5 0, 5 200 1, 5 2 2 1, 5 1 2 1 3 к L q L l q L L R l l l R L q L l q L R L l l l   −       ′ = + − =       ⋅ −   ⋅     = + + ⋅ − =   ⋅   ′ =   −   ∆     ′′ = + − =   ⋅     ⋅ −   ⋅   = + + ⋅ ⋅ ⋅ △ 2 2 2 2 2 2 2 2 3 3 3 3 2 1 1 1 1 3 2 2 1 2 2 2 1 2 0, 5 150 H; 150 Н ; 200 1, 5 200 1, 5 300 Н ; 2 2 3 2 1 2 1 3 300 Н ; 193, 75 72, 23 600 422, 68 H; 1, 5 193, 75 72, 23 150 150 1, 5 к R q L q L R l l R M M R R L M M M M R R R L L   − =     ′′ = ∆ ⋅ ⋅ ′ = + = + = ⋅ ⋅ ⋅ ⋅ ′ = − − −   ′ = + = + =     − − ′ ′′ = + − + = − −  = + − 2 27, 78 193, 75 ; 1, 5 625, 01 Н ; R +    +         =