Disclosed is a lifting, stabilising, propulsive arrangement for vertical take-off and landing aircraft, which uses: rotary wings; lifting, propulsive, stabilising turbines or fans on the trailing edges of the wings and tail assembly; and centrifugal or tangential turbines disposed on the sides of the fuselage and on the leading and trailing edges of the wings, or centrifugal or tangential turbines disposed on the sides of the fuselage and inside the wings. The centrifugal or tangential turbines on the fuselage are fixed and only generate lift, and those on the wings rotate with the wings and generate lift during vertical flight and thrust during horizontal flight. In the arrangement, horizontal stabilising fans are added on the tips of the wings or horizontal stabiliser and steering fans are added on the vertical stabiliser.
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