VERTICAL FLIGHT SYSTEM MAINLY APPLYING PROPULSION PRINCIPLE (PRESSURE THRUST FORCE) OF ROCKET AND RE-USE TYPE SPACE SHUTTLES SUCH AS (COMPRESSION) AIR CIRCULATION TYPE LOCALLY CONVERTING THE SAME SYSTEM (PORTION THEREOF)

摘要

PROBLEM TO BE SOLVED: To widely provide vertical take-off and landing planes that eliminate the need for particularly high performance (high cost) engine and still more have superior propulsion efficiency, and re-use type space shuttles applying a portion of the vertical flight system of the special VTOL.;SOLUTION: A vertical flight system is configured by: operating suction/intake air fans (f) arranged in a recess area of an interval space between the front and back of a body and the left and right main wing (a); generating wind power on a horizontal line facing a machine body and causing the rising wind from an air intake under the plane body to thereby push up the plane; previously making the air from a predetermined inlet flow in toward a main propulsion/vertical flight air bag (c) in an area under both wings to highly increase the pressure in the bag to the maximum; downwardly injecting the main propellant at a stretch through a lid of a high-speed nozzle under the gas bag; and continuously injecting the compressed air downward from the latter outlet, while adjusting a balance between an air intake amount from air compressors and an air discharge amount from the air nozzle, and filling the air timely (in the vertical flight) from the former suction inlet.;COPYRIGHT: (C)2016,JPO&INPIT