Конструирование агрегатов самолета

53 1 2 3 0 0 2 2 2 H H H H 533, 33 ; 400 ; 266, 67 ; 200 ; м м м м H H 200 ; 200 . м м k k q q q q q q q q q q = = = = ∆ = − = ∆ = − = Расчет : ( ) ( ) ( ) ( ) ( ) 3 3 0 1 2 1 1 2 2 2 3 3 3 3 3 2 2 2 2 2 2 0 1 1 1 1 1 2 2 2 2 3 4 4 4 3 2 1 3 7 2 4 60 2 ; 4 15 2 533, 33 0, 5 2 2 3 2 600 533, 33 0, 5 ; 3 200 0, 5 2 2 3 2 266, 67 200 0, 5 ; 2 3 72, 23 H м ; 27, 78 H м ; 7 к к q L q L M l M l l M l q L q L q q l q l M q q l q l M M M   + + + = − + −       − +     − ⋅ = + = + ⋅ − ⋅ + − ⋅ ⋅ = + = + ⋅ − ⋅ + ⋅ = ⋅ = ⋅ ⋅ ( ) 2 3 3 3 3 2 2 2 2 2 0 1 2 1 1 2 2 1 193, 75 H м 2, 23 1 2 1 1 27, 78 1 400 1, 5 7 200 1, 5 200 1, 5 2 200 1, 5 ; 4 60 4 15 2 200 1, 5 2 400 1, 5 600 H; 2 2 3 2 3 1 2 1 600 Н ; ; M M q L q L R l l R ⋅ + + + ⋅ =     ⋅ ⋅ ⋅ ⋅ ⋅ ⋅ = − + − +         ∆ ⋅ ⋅ ′ = + = + = ⋅ ⋅ ⋅ ⋅ ′ = = ⋅ ⋅ ⋅