The invention discloses a binary vector nozzle structure and an aircraft with the same. In the binary vector nozzle structure, an upper fixed convergence adjusting piece is connected with a circular rotating square section; a lower fixed convergence adjusting piece is connected with the circular rotating square section; an upper adjustable convergence adjusting piece is arranged in a chute in theupper fixed convergence adjusting piece; a lower adjustable convergence adjusting piece is arranged in a chute in the lower fixed convergence adjusting piece; a first actuating cylinder is connected with the upper adjustable convergence adjusting piece; a second actuating cylinder is connected with the lower adjustable convergence adjusting piece; one side of the upper adjustable convergence adjusting piece is hinged to one side of an upper expansion adjusting piece; one side of the lower adjustable convergence adjusting piece is hinged to one side of a lower expansion adjusting piece; one endof an upper pull rod is hinged to the upper fixed convergence adjusting piece; the other end of the upper pull rod is hinged to the upper expansion adjusting piece; one end of a lower pull rod is hinged to the lower fixed convergence adjusting piece; and the other end of the lower pull rod is hinged to the lower expansion adjusting piece. The binary vector nozzle structure is simple in structureand easy to realize motion adjustment.