JPS6113199U

JPS6113199U - Steering device for guided flight vehicles

Info

Publication number: JPS6113199U
Application number: JP9661584U
Authority: JP
Inventors: 隆二郎黒崎
Original assignee: 三菱電機株式会社
Priority date: 1984-06-27
Filing date: 1984-06-27
Publication date: 1986-01-25

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

[Brief explanation of the drawing]

第１図は従来の誘導飛しよ′う体の誘導制御部と操舵翼
の概略図、第２図は操舵翼に舵角をとらせた場合の概略
図、第３図はこの考案による機体の制御部と操舵翼との
取り付けを示す概略図、第４図、第５図はこの考案によ
る操舵部、操舵翼の動作例を示す図である。図中、１は機体の誘導部、２は制御部、３は操舵翼、４
は従来の装置の操舵軸、また５はピン、６はこの考案で
の操舵軸、７はアーム、８は駆動ピン、９はスライド溝
である。Ａは空気の流れ、Ｂは空力中心点、Ｃ，Ｄ，Ｅは中心線
、Ｆ，Ｆ５，Ｆ８は空気力、δは舵角、θは操舵角、れ
は最大舵角、θＭは最大操舵角、またＭＩ−Ｉｇ ’Ｍ
ｐはモーメント、Ｘ，ｚは座標軸である。なお、図中同一あるいは相当部分には同一符号を付して
示してある。Figure 1 is a schematic diagram of the guidance control unit and steering blade of a conventional guided flying vehicle, Figure 2 is a schematic diagram of the steering blade when the steering angle is adjusted, and Figure 3 is the aircraft based on this invention. 4 and 5 are diagrams showing an example of the operation of the steering section and the steering vane according to this invention. In the figure, 1 is the guidance section of the aircraft, 2 is the control section, 3 is the steering wing, and 4
5 is a steering shaft of the conventional device, 5 is a pin, 6 is a steering shaft in this invention, 7 is an arm, 8 is a drive pin, and 9 is a slide groove. A is air flow, B is aerodynamic center point, C, D, E are center lines, F, F5, F8 are aerodynamic forces, δ is steering angle, θ is steering angle, is maximum steering angle, θM is maximum steering corner, also MI-Ig'M
p is a moment, and X and z are coordinate axes. It should be noted that the same or corresponding parts in the figures are indicated by the same reference numerals.

Claims

[Scope of utility model registration request]

A steering wing provided on the guided flight body, a pin that rotatably engages the steering wing and the aircraft body, an arm attached perpendicular to the aircraft steering axis, a pin attached to the tip of this arm, and a steering system in which this pin moves back and forth. A steering device for a guided flying body, characterized in that a sliding groove is provided on the centerline of the wing on the side where the wing is attached to the aircraft body.