JPS6034096U

JPS6034096U - extension structure

Info

Publication number: JPS6034096U
Application number: JP12652283U
Authority: JP
Inventors: 信義井村
Original assignee: 三菱電機株式会社
Priority date: 1983-08-16
Filing date: 1983-08-16
Publication date: 1985-03-08

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) [Abstract] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

[Brief explanation of drawings]

第１図はコイル状に折りたたまれた従来の伸展構造物を
示す図、第２図は一部伸展した従来の伸展構造物を示す
図、第３図は伸展後の従来の伸展構造物を示す斜視図、
第４図は第３図の平面図、第５図は従来の伸展構造物の
用途の一例を示す図、第６図はこの考案の伸展構造物を
示す図、第７図および第８図はこの考案の特徴を有する
指向調整用ケーブルを説明するための図である。図において５は伸展構造物、６はフレキシブル太陽電池
パドル、７は調整用ケーブル、８はドラム、９はモータ
、１０は大型展開型アンテナ、１１は人工衛星である。なお、図中同一あるいは相当部分には同一符号を付して
示しである。Figure 1 shows a conventional extension structure folded into a coil, Figure 2 shows a conventional extension structure partially extended, and Figure 3 shows a conventional extension structure after extension. Perspective view,
FIG. 4 is a plan view of FIG. 3, FIG. 5 is a diagram showing an example of the use of the conventional extension structure, FIG. 6 is a diagram showing the extension structure of this invention, and FIGS. 7 and 8 are FIG. 3 is a diagram for explaining a directivity adjustment cable having the features of this invention. In the figure, 5 is an extension structure, 6 is a flexible solar battery paddle, 7 is an adjustment cable, 8 is a drum, 9 is a motor, 10 is a large deployable antenna, and 11 is an artificial satellite. It should be noted that the same or equivalent parts in the figures are indicated by the same reference numerals.

Claims

[Scope of utility model registration request]

In an extension structure that is attached to a satellite body and extends a flexible solar battery paddle, deployable antenna, etc. in space, the satellite body and the solar battery paddle or deployable antenna, etc. are connected, and the length of the connection is determined. An extension structure characterized by comprising a cable that adjusts the directivity direction of the solar cell paddle, deployable antenna, etc. by changing the direction.