Propelling nozzle for the thrust vector control for aircraft equipped with jet engines

摘要: The proposal is for a thrust nozzle aircraft fitted with jet engines especially lateral vector control, in which the upstream ends of at least two flaps (8, 12) actuated via lever-like adjusters are arranged to pivot simultaneously different angles rotation about spindles running across axis (20) and between walls (22, 23) substantially parallel square housing such way that, permanently convergent contour, narrowest cross-section formed outlet side; one end each adjuster (28, 29) engage downstream flaps, said being their movably mutually coupled other travel guide path (30) curved so as produce continuously flap angles; or more cross-sections can either be kept constant change dependently upon deflection angle.