Flight body, landing method, and program
AssigneeAeronext Inc.
InventorYoichi SUZUKI
Life of this patent
Estimating the term…
Abstract
A landing method for a flight body capable of achieving both vertical takeoff and landing and improving fuel consumption while improving landing performance. A flight body, comprising: a plurality of rotary wing parts that generate at least lift; a thrust drive device; and a fixed wing, wherein the thrust drive device generates thrust on the opposite side of horizontal flight during landing. Furthermore, the thrust drive device is equipped with a propeller, which, when landing, rotates in the opposite direction to that of horizontal flight. Furthermore, the thrust drive system generates more thrust to the opposite side during an emergency crash than during a landing.
Claims6
A flight body, comprising:
- a plurality of rotary wing parts that generate at least lift;
- a thrust drive device;
- and
- a fixed wing,
- wherein the thrust drive device generates thrust on the opposite side during landing from that during horizontal flight.
A landing method for a flight body comprising a plurality of rotary wing parts that generate at least lift;
- a thrust drive device;
- and a fixed wing,
- wherein the thrust drive device generates thrust on the opposite side during landing from that during horizontal flight.
A non-transitory computer-readable storage medium storing a program that instructs a computer to execute a method of landing a flight body comprising a plurality of rotary wing parts that generate at least lift;
- a thrust drive device;
- and a fixed wing, wherein the thrust drive device generates thrust on the opposite side during landing from that during horizontal flight.
Dependencies are inferred from the claim text.