JPH035190Y2 - - Google Patents

Info

Publication number
JPH035190Y2
JPH035190Y2 JP1984037277U JP3727784U JPH035190Y2 JP H035190 Y2 JPH035190 Y2 JP H035190Y2 JP 1984037277 U JP1984037277 U JP 1984037277U JP 3727784 U JP3727784 U JP 3727784U JP H035190 Y2 JPH035190 Y2 JP H035190Y2
Authority
JP
Japan
Prior art keywords
band
fuselage
thick part
protrusion
attached
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP1984037277U
Other languages
Japanese (ja)
Other versions
JPS60148191U (en
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP3727784U priority Critical patent/JPS60148191U/en
Publication of JPS60148191U publication Critical patent/JPS60148191U/en
Application granted granted Critical
Publication of JPH035190Y2 publication Critical patent/JPH035190Y2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Axle Suspensions And Sidecars For Cycles (AREA)
  • Package Frames And Binding Bands (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)

Description

【考案の詳細な説明】 この考案は、オートバイのクツシヨンタンクの
取付け等に用いる締着バンドに関する。
[Detailed Description of the Invention] This invention relates to a fastening band used for attaching a cushion tank of a motorcycle.

オートバイのクツシヨンに連結されたタンク
を、機体のパイプに取付けるような場合、通常
は、機体の取付け位置に合せて受座を設け、この
受座にタンクを重ね、締着バンドで機体とタンク
を巻付けて取付けるようになされており、そのた
め受座と締着バンドの二つの部品が最低限必要で
あつた。
When attaching a tank connected to a motorcycle cushion to a pipe on the fuselage, normally a catch is provided to match the mounting position of the fuselage, the tank is stacked on this catch, and the fuselage and tank are secured with a tightening band. It was designed to be installed by winding it around, so at least two parts were required: a catch and a fastening band.

この考案は、かかる点に鑑み、締着バンドだけ
で、機体に取着体を安定して取付けることがで
き、製造コストが安価になるように改善したもの
で、以下図面に示す本考案の実施例について説明
する。
In view of these points, this invention has been improved so that the attachment body can be stably attached to the aircraft body using only the tightening band, and the manufacturing cost is low.The invention is implemented as shown in the drawings below. Let's discuss an example.

図に示す実施例では、機体1である鋼管製のフ
レームに、クツシヨンユニツト2に連結した取着
体3である円筒形のタンクを取付ける場合を示し
たものである。バンド4は、弾性体を用いて所定
の形状に型成形するもので、一端に厚肉部5を一
体に形成する。厚肉部5は、外側面が機体1に添
う形状にしてあり、内側面が取着体3に添う形状
にしてある。そしてこの厚肉部5は機体1と取着
体3との対向面間を横断する高さを有している。
バンド4の両端には、掛止金具6を差込んで取付
ける。厚肉部5側の掛止金具6は、機体1に巻け
るU字状の形状にしてあつて、先端が鍵形に曲げ
てある。他の側の掛止金具6はリング形である。
バンド4の他端には、手掛け7が一体に成形して
ある。また、厚肉部5には、機体1側の面の中央
に孔8が設けてあつて、機体1に溶着した突起9
に挿入できるようにしてある。
In the embodiment shown in the figure, a cylindrical tank, which is a mounting body 3 connected to a cushion unit 2, is attached to a steel pipe frame, which is a machine body 1. The band 4 is molded into a predetermined shape using an elastic body, and has a thick portion 5 integrally formed at one end. The thick portion 5 has an outer surface shaped to conform to the fuselage body 1, and an inner surface shaped to conform to the attachment body 3. The thick portion 5 has a height that extends across the opposed surfaces of the body 1 and the attachment body 3.
The latches 6 are inserted into both ends of the band 4 to attach them. The hook 6 on the side of the thick part 5 has a U-shape that can be wrapped around the body 1, and its tip is bent into a key shape. The latch 6 on the other side is ring-shaped.
A handle 7 is integrally formed on the other end of the band 4. Further, the thick portion 5 has a hole 8 provided in the center of the surface on the body 1 side, and a protrusion 9 welded to the body 1.
It can be inserted into.

作用について説明する。 The effect will be explained.

バンド4は、厚肉部5の外側面を機体1に合せ
る。そして、機体1の突起9に孔8を嵌合せて位
置決めする。こうして、厚肉部5を機体1に合せ
て、厚肉部5側の掛止金具6を機体1に巻く。次
に、厚肉部5の内側面に取着体3を合せ、バンド
4を取着体3に巻付け、手掛け7を引張つてバン
ド4に張力を与え、外端の掛止金具6を厚肉部5
側の掛止金具6に掛止める。こうして、機体1に
取着体3をバンド4で締着することができる。厚
肉部5は、取着体3を受ける受座になると共に、
厚肉部5も弾性体であるので、取着体3の緩衝材
にもなる。
The band 4 aligns the outer surface of the thick portion 5 with the body 1. Then, the projection 9 of the body 1 is fitted into the hole 8 for positioning. In this way, the thick part 5 is aligned with the body 1, and the hook 6 on the side of the thick part 5 is wound around the body 1. Next, the attaching body 3 is aligned with the inner surface of the thick part 5, the band 4 is wound around the attaching body 3, the handle 7 is pulled to apply tension to the band 4, and the outer end latch fitting 6 is attached to the thick wall part 5. Meat part 5
Hang it on the latch fitting 6 on the side. In this way, the attachment body 3 can be fastened to the body 1 with the band 4. The thick portion 5 serves as a seat for receiving the attachment body 3, and
Since the thick portion 5 is also an elastic body, it also serves as a cushioning material for the attachment body 3.

したがつて、この考案によれば、締着バンドで
機体に取着体を取付けるとき、その厚肉部の孔を
機体の突起に嵌合させることにより位置決めさ
れ、ずれ動くことなく機体と取着体との間に厚肉
部を介在させることができ、締着作業が容易にな
ると同時に位置ずれを生じることがない。また機
体と取着体との対向面間を横断して厚肉部が介在
するので、締着バンドを締付けても両者の中心間
距離が一定に保たれ、作業者による取付誤差の発
生が皆無となる。さらに機体の突起に厚肉部の孔
が嵌合しているので、締着バンドの巻締め時にそ
の反力を作業者自身で受持つ必要がなく、作業性
の向上につながるなどの種々の効果がある。
Therefore, according to this invention, when attaching the attaching body to the fuselage body using a fastening band, the hole in the thick part of the attachment body is fitted into the protrusion of the fuselage body to determine the position, and it can be attached to the fuselage body without shifting. A thick portion can be interposed between the body and the body, making the tightening work easier and at the same time preventing misalignment. In addition, since there is a thick part intervening between the facing surfaces of the machine body and the attachment body, the distance between the centers of the two remains constant even when the tightening band is tightened, and there is no installation error caused by the operator. becomes. Furthermore, since the hole in the thick wall part fits into the protrusion of the machine body, there is no need for the operator to bear the reaction force when tightening the fastening band, leading to various effects such as improved work efficiency. There is.

【図面の簡単な説明】[Brief explanation of the drawing]

図は本考案の一実施例を示し、第1図は側面
図、第2図は第1図A矢視拡大図、第3図はバン
ドの展開図である。 1……機体、3……取着体、4……バンド、5
……厚肉部、6……掛止金具、8……孔、9……
突起。
The figures show one embodiment of the present invention, in which Fig. 1 is a side view, Fig. 2 is an enlarged view taken in the direction of arrow A in Fig. 1, and Fig. 3 is a developed view of the band. 1... Airframe, 3... Mounting body, 4... Band, 5
... Thick wall part, 6 ... Latching fitting, 8 ... Hole, 9 ...
protrusion.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 弾性体からなるバンドの一端に機体と取着体と
の対向面間を横断して置かれる厚肉部を一体に形
成し、この厚肉部の外側面を機体に添う形状に形
成するとともに内側面を取着体に添う形状に形成
し、前記機体に突起を、厚肉部にこの突起が嵌入
する孔をそれぞれ設け、バンドの両端には互いに
掛着し得る掛止金具を取付けてなり、前記厚肉部
の孔を機体の突起に嵌合して厚肉部を機体と取着
体との間に介在させたのち取着体にバンドを巻付
け、外端の掛止金具を引張つて機体に巻いた掛止
金具に掛止めるようにしたことを特徴とする締着
バンド。
A thick part is integrally formed at one end of the band made of an elastic material, and is placed across the facing surfaces of the fuselage and the attached body. The side surface is formed in a shape that follows the attachment body, a protrusion is provided on the body, a hole into which the protrusion fits is provided in the thick part, and latching metal fittings that can be attached to each other are attached to both ends of the band, After fitting the hole of the thick part into the protrusion of the fuselage body so that the thick part is interposed between the fuselage body and the attachment body, wrap the band around the attachment body, and pull the latching metal fitting at the outer end. A fastening band characterized by being latched onto a latching metal fitting wrapped around the aircraft body.
JP3727784U 1984-03-15 1984-03-15 fastening band Granted JPS60148191U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3727784U JPS60148191U (en) 1984-03-15 1984-03-15 fastening band

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3727784U JPS60148191U (en) 1984-03-15 1984-03-15 fastening band

Publications (2)

Publication Number Publication Date
JPS60148191U JPS60148191U (en) 1985-10-01
JPH035190Y2 true JPH035190Y2 (en) 1991-02-08

Family

ID=30543213

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3727784U Granted JPS60148191U (en) 1984-03-15 1984-03-15 fastening band

Country Status (1)

Country Link
JP (1) JPS60148191U (en)

Also Published As

Publication number Publication date
JPS60148191U (en) 1985-10-01

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