FIELD: aviation.
SUBSTANCE: invention relates to aircraft with vertical take-off and vertical landing. Vertical take-off and vertical landing aircraft comprises fuselage, wings and jet engines. Front part of wings is made with possibility of controlled shift from wings to certain distance and controlled connection with wings. Shifted part of the wings comprises an air duct with a confuser. At the output of jet engines there are cooled compressed air accumulators with controlled gate valves. Cooled compressed air accumulators are connected by air duct with intercooler. Intercooler is connected to air ducts of shifted part of wings.
EFFECT: simplified design for vertical take-off and vertical landing.
1 cl, 2 dwg
