Title:
FLIGHT STABILIZER OR MISSILE MOUNTED WITH THE SAME
Document Type and Number:
Japanese Patent JP2023079662
Kind Code:
A
Abstract:
To provide a flight stabilizer and a missile which can cancel swirling air without affected by a change in swirling air speed due to a change in flight speed.SOLUTION: A flight stabilizer is mounted on a missile using rotation of a propeller body as drive force, and reduces an influence of swirling air generated by a main blade body. The flight stabilizer includes a mounting part 110 capable of being mounted on the propeller body, a plurality of short blade bodies 120 extending from the mounting part 110, a rectifier 130 which is provided on the short blade bodies 120 and adjusts air speed, and an arc partition body 140 mounted on the outer periphery tip of the short blade bodies 120. Central air 101 is generated behind by the rectifier 130, and covers the periphery of a body of an airframe. Air speed of the central air 101 is adjusted to be lower than air speed of propulsion air 201 obtained by rotation of the main blade body 210 of the propeller body, and the central air 101 flows so as to be partitioned from the propulsion air 201 by the arc partition body 140.SELECTED DRAWING: Figure 1
Inventors:
HASHIMOTO SEIYA
Application Number:
JP2021193239A
Publication Date:
June 08, 2023
Filing Date:
November 29, 2021
Export Citation:
Assignee:
HASHIMOTO SEIYA
HAYASHIDA OSAMU
HAYASHIDA OSAMU
International Classes:
B64C11/18
Attorney, Agent or Firm:
Michiaki Nagai
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