JPS62119000U

JPS62119000U -

Info

Publication number: JPS62119000U
Application number: JP290286U
Authority: JP
Priority date: 1986-01-13
Filing date: 1986-01-13
Publication date: 1987-07-28

Description

[Brief explanation of the drawing]

第１図ａ，ｂはこの考案の一実施例を示す飛翔
体のロール制御装置の一例を示す構成図およびそ
のＡ―Ａ断面拡大図、第２図ａ，ｂはこの考案の
他の実施例を示す飛翔体のロール制御装置の一例
を示す構成略図、第３図、第４図はこの考案のさ
らに他の実施例を示す飛翔体のロール制御装置の
構成略図、第５図ａ，ｂはスポイラ方式による空
気力学的ロールモーメントを発生させる可動翼の
一例を説明する構成図およびＢ―Ｂ断面拡大図、
第６図ａ，ｂは空気学力的ロールモーメントの発
生原理を説明する図、第７図は飛翔体全体の空気
力学的ロールモーメントを説明する図である。図において、１は操舵翼、２はスポイラ、３は
貫通穴、４は回転駆動軸、５は仕切材である。な
お、各図中の同一符号は同一または相当部分を示
す。 Fig. 1 a, b is a block diagram showing an example of a roll control device for a flying object showing an embodiment of this invention, and an enlarged sectional view taken along line A-A thereof, and Fig. 2 a, b is another embodiment of this invention. FIGS. 3 and 4 are schematic diagrams of the configuration of a flying object roll control device showing still another embodiment of this invention, and FIGS. A configuration diagram illustrating an example of a movable wing that generates an aerodynamic roll moment using a spoiler method, and an enlarged cross-sectional view taken along B-B.
FIGS. 6a and 6b are diagrams illustrating the principle of generation of aerodynamic roll moment, and FIG. 7 is a diagram illustrating the aerodynamic roll moment of the entire flying object. In the figure, 1 is a steering blade, 2 is a spoiler, 3 is a through hole, 4 is a rotary drive shaft, and 5 is a partition member. Note that the same reference numerals in each figure indicate the same or corresponding parts.

Claims

[Scope of utility model registration request]

In a flying object roll control device for controlling the roll moment of a flying object having a pair of control vanes, a through hole vertically penetrating through the pair of control vanes is provided at a symmetrical position of the pair of control vanes, and the 1. A roll control device for a flying object, characterized in that a spoiler protruding from the upper or lower surface of a control blade surface is rotatably provided in the through hole.