Cascade for turbomachines

Blade cascade arrangement for turbomachinery in axial construction with two positioned relative to each other firmly, a different number of blades in each constant blade pitch having Leitschaufelgittern and with an arranged between these blade grid. DOLLAR A The blades of the first Leitschaufelgitters have in a first partial area T1 of the grid sequentially on a same axial offset delta M, DOLLAR A of the axial offset delta M is selected depending on the blade number ratio Z1 / Z2 of the two guide blade so that it the effective flow cross-section at Z1> Z2 enlarged, reduced at Z1 <Z2, and DOLLAR a, the blades of the first Leitschaufelgitters have in a second partial area T2 of the grid sequentially in a rotation to delta M opposite to possibly changing Axial -DELTA n on.