JPS6344900U

JPS6344900U -

Info

Publication number: JPS6344900U
Application number: JP13862286U
Authority: JP
Priority date: 1986-09-11
Filing date: 1986-09-11
Publication date: 1988-03-25

Description

[Brief explanation of the drawing]

第１図は本考案航空機の停止標識装置の実施例
における正面図、第２図は第１図の側面図、第３
図は第１図Ａ部の拡大斜視図、第４図は第１図Ｂ
部の拡大斜視図、第５図は第１図Ｃ部の拡大斜視
図、第６図は従来の据付式サイドターゲツトの正
面図、第７図は第６図の平面図、第８図は第６図
の標識腕を旋回する状態を示す概略図、第９図は
第８図Ｄ部の拡大平面図、第１０図は従来の移動
式サイドターゲツトの正面図、第１１図は第１０
図の平面図、第１２図は第１１図Ｅ部の拡大図で
ある。１……支柱、２……標識腕、２ａ……標識腕の
ピン、３……ターゲツト（停止標識）、４……台
車、１４……支柱内筒、１４ａ……ブラケツト、
１４ｂ……勾配溝、１５……ローラ、１６……ワ
イヤロープ、１７……ブラケツト、１８……滑車
、１９……ロープリール、２０……ハンドル、２
１……案内ローラ、２３……ピン、２４……支持
台、２５……ねじ、２６……ハンドル、２８……
前後位置調整装置、３１，３１′……ストツパ、
３２……ロツクピン、３３……ピン、３４……高
さ検知指針、３５……高さ表示目盛板、３６……
傾斜検知指針、３７……傾斜表示目盛板。 Figure 1 is a front view of an embodiment of the stop sign device for an aircraft according to the present invention, Figure 2 is a side view of Figure 1, and Figure 3 is a side view of Figure 1.
The figure is an enlarged perspective view of part A in Figure 1, and Figure 4 is part B in Figure 1.
FIG. 5 is an enlarged perspective view of section C in FIG. 1, FIG. 6 is a front view of a conventional stationary side target, FIG. 7 is a plan view of FIG. 6, and FIG. 6 is a schematic diagram showing the turning state of the marking arm, FIG. 9 is an enlarged plan view of section D in FIG. 8, FIG. 10 is a front view of a conventional mobile side target, and FIG.
FIG. 12 is an enlarged view of section E in FIG. 11. 1... Strut, 2... Sign arm, 2a... Sign arm pin, 3... Target (stop sign), 4... Dolly, 14... Strut inner cylinder, 14a... Bracket,
14b... Gradient groove, 15... Roller, 16... Wire rope, 17... Bracket, 18... Pulley, 19... Rope reel, 20... Handle, 2
1... Guide roller, 23... Pin, 24... Support stand, 25... Screw, 26... Handle, 28...
Front and rear position adjustment device, 31, 31'... stopper,
32...Lock pin, 33...Pin, 34...Height detection pointer, 35...Height display scale plate, 36...
Tilt detection pointer, 37... Tilt display scale plate.

Claims

[Scope of utility model registration request]

A single stop sign device installed on the roadside of an aircraft approach line, comprising: a column supported on a trolley so that it can be raised and lowered and tilted; a sign arm that is rotatably supported at the upper end of the column and extends horizontally; and the sign. and a target suspended from the arm, and the marking arm is characterized in that when the aircraft overruns, the marking arm turns in a climbing direction in the approach direction of the aircraft, and returns to its original horizontal position when the aircraft retreats. Aircraft stop sign device.