公开(公告)号：US10414491B2

公开(公告)日：2019-09-17

申请号：US15521896

申请日：2015-11-26

Applicant: Kazem Milani

Inventor： Kazem Milani

IPC: B64C27/20 ,  B64C29/00

Abstract: Disclosed herein is a vertical take-off and landing (VTOL) aircraft. The vertical take-off and landing aircraft includes a single wing, a plurality of engines, a first set of propellers on a first side of the single wing, a second set of propellers on a second side of the single wing, a first power transfer unit, a second power transfer unit, landing gears connected to the single wing, and a fuselage with a capacity of 100 passengers connected to the single wing. The plurality of engines includes a first engine mounted to the first side of the single wing and a second engine mounted to the second side of the single wing.

公开(公告)号：US20180029704A1

公开(公告)日：2018-02-01

申请号：US15521896

申请日：2015-11-26

Applicant: KAZEM Milani

Inventor： KAZEM Milani

IPC: B64C29/00 ,  B64C27/20

CPC classification number: B64C29/0033 ,  B64C27/20

Abstract: Not requiring aileron, elevator, rudder, flap, slat, horizontal and vertical stabilizer and not transferring vibration to the fuselageIn this invention the engine and fuselage (hanging under wing) are the same as those in other airplane but the wing (just one) is different,It has rectangular shape with triangular leading edge and consists of wing box(embedded in wing) to which four rotating taper tubes are attached, each with a propeller, that is, one pair for each side of wing box.There are two turbo shaft engines, each engine runs one pair of propellers, via shafts and gear boxes.Now smooth rotation of taper tube will tilt the propeller up to 90′ using stepper motor, so propeller can tilt from horizontal (takeoff and landing) mode to vertical(cruise)mode.also change of propeller's pitch angle or tilt of propeller or engine power adjusting separately or in combination, act as flight control surfaces, providing all flight directions including pitch, yaw, bank,Heading, etc