JPH0245470Y2 - - Google Patents
Info
- Publication number
- JPH0245470Y2 JPH0245470Y2 JP8991783U JP8991783U JPH0245470Y2 JP H0245470 Y2 JPH0245470 Y2 JP H0245470Y2 JP 8991783 U JP8991783 U JP 8991783U JP 8991783 U JP8991783 U JP 8991783U JP H0245470 Y2 JPH0245470 Y2 JP H0245470Y2
- Authority
- JP
- Japan
- Prior art keywords
- cooling water
- connecting body
- narrow part
- narrow
- water passage
- 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
Links
- 239000000498 cooling water Substances 0.000 claims description 20
- 229920003002 synthetic resin Polymers 0.000 description 2
- 239000000057 synthetic resin Substances 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
Landscapes
- Automatic Cycles, And Cycles In General (AREA)
Description
【考案の詳細な説明】
この考案は、機体の狭い部分に冷却水ホースを
通す必要がある場合の水冷エンジンの冷却水通路
に関する。[Detailed Description of the Invention] This invention relates to a cooling water passage for a water-cooled engine when it is necessary to pass a cooling water hose through a narrow part of an aircraft body.
オートバイに搭載するエンジン等では、エンジ
ンの近くに、フレーム、ラジエター、燃料タンク
等が配置され、余分なスペースが少く、冷却水ホ
ースを機体の狭い場所に通すことも必要になつて
くる。この場合、第１図に示すように、機体の狭
い場所Ａに冷却水ホースＢを通した場合、冷却水
ホースＢに曲げ方向の関係などで、部分的に低い
部分Ｃと高い部分Ｄができると、高い部分Ｄの内
側がエアー溜りＥになつて、冷却水の流れが悪く
なり、冷却に支障を来すことがある。 In engines mounted on motorcycles, the frame, radiator, fuel tank, etc. are located near the engine, and there is little extra space, making it necessary to route cooling water hoses through narrow spaces inside the aircraft. In this case, as shown in Figure 1, if the cooling water hose B is passed through a narrow space A on the aircraft, the cooling water hose B will have a partially low part C and a high part D due to the bending direction. Then, the inside of the high portion D becomes an air pocket E, which impedes the flow of cooling water and may impede cooling.
この考案は、かかる点に鑑み改善したもので、
以下本考案を第２図乃至第４図に示す実施例につ
いて説明する。 This idea is an improvement based on these points.
The present invention will be described below with reference to embodiments shown in FIGS. 2 to 4.
機体１の狭い部分２に冷却水ホースを通す必要
がある場合、狭い部分２の形状に合せて、上面が
平らな中空連結体３を非可撓性の合成樹脂等によ
つて形成する。連結体３は、機体における上下の
幅が狭い部分に対応する部位ではその分横方向に
偏平にして、一定断面積を有するようにする。
又、連結体３には、ボス４を突設して、機体１に
ビス５で締着できるようにしてある。そして、連
結体３の前後には冷却水パイプ６を連結する。 When it is necessary to pass a cooling water hose through a narrow portion 2 of the fuselage 1, a hollow connecting body 3 with a flat top surface is formed of non-flexible synthetic resin or the like to match the shape of the narrow portion 2. The connecting body 3 is made horizontally flat in areas corresponding to narrow vertical widths of the fuselage, so as to have a constant cross-sectional area.
Further, a boss 4 is provided in a protruding manner on the connecting body 3 so that it can be fastened to the body 1 with screws 5. Cooling water pipes 6 are connected before and after the connecting body 3.
しかして、連結体３は、可撓することがなく、
狭い部分２に合せた形状にできているので、位置
が安定し、上面が平らで、高い場所ができるよう
なことがない。このため、前後に冷却水パイプ６
を連結して、冷却水を通してもエアー溜りができ
ず、冷却水の良好な流れを確保できる。又、連結
体３は、形状が狭い部分２に合めてあつて、位置
が安定し、特にビス５で締着すれば、機体１の水
平方向に対する取付けが安定し、高低部分ができ
る心配がなく、誰が組付けても一定条件に組付け
できる。 Therefore, the connecting body 3 is not flexible,
Since it is shaped to fit the narrow part 2, the position is stable, the top surface is flat, and no high places are created. For this reason, the front and rear cooling water pipes 6
Even if the cooling water is connected, air pockets will not be formed and a good flow of the cooling water can be ensured. In addition, if the connecting body 3 is fitted in the narrow part 2 and its position is stable, especially if it is tightened with the screw 5, the installation in the horizontal direction of the fuselage 1 will be stable, and there will be no need to worry about the formation of high or low parts. No matter who does the assembly, it can be assembled under certain conditions.
以上説明したように、この考案は、機体の狭い
部分を通すようにした冷却水通路において、上面
が平らで、上記狭い部分に対応する部分では横幅
を広くして全長にわたつて一定断面積とした非可
撓性の中空連結体を、上記機体の狭い部分に沿つ
て配設し、その中空連結体の前後に冷却水パイプ
を連結するようにしたので、連結体を狭い部分に
合せて配置でき、高低部分ができず内部にエアー
溜りができることがないので、冷却水の良好な流
れが確保できる。又、組付けの場合も、組付け差
がないように組付けできる。そして、連結体は、
合成樹脂成形によつて安価に製作できる。又、連
結体は、冷却水通路に必要な有効断面積を容易に
確保できる利点もある。 As explained above, this idea is based on a cooling water passage that passes through a narrow part of the aircraft, with a flat top surface and a wider width in the part corresponding to the narrow part so that the cross-sectional area is constant over the entire length. A non-flexible hollow connecting body is placed along the narrow part of the aircraft body, and cooling water pipes are connected to the front and rear of the hollow connecting body, so that the connecting body can be placed in line with the narrow part. Since there are no high and low parts and no air pockets form inside, a good flow of cooling water can be ensured. Also, in the case of assembly, the assembly can be performed so that there is no difference in assembly. And the connector is
It can be manufactured inexpensively by synthetic resin molding. Further, the connecting body has the advantage that the effective cross-sectional area necessary for the cooling water passage can be easily secured.
第１図は従来例を示す部分縦断側面図、第２図
乃至第４図は本考案の一実施例を示し、第２図は
側面図、第３図は連結体の拡大側面図、第４図は
第３図−矢視横断面図である。
１……機体、２……狭い部分、３……連結体、
６……冷却水パイプ。
Fig. 1 is a partial vertical side view showing a conventional example, Figs. 2 to 4 show an embodiment of the present invention, Fig. 2 is a side view, Fig. 3 is an enlarged side view of the connecting body, The figure is a cross-sectional view taken in the direction of the arrows in FIG. 3. 1... Airframe, 2... Narrow part, 3... Connector,
6...Cooling water pipe.
Claims (1)
おいて、上面が平らで、上記狭い部分に対応する
部分では横幅を広くして全長わたつて一定断面積
とした非可撓性の中空連結体を、上記機体の狭い
部分に沿つて配設し、その中空連結体の前後に冷
却水パイプを連結するようにしたことを特徴とす
る水冷エンジンの冷却水通路。 In a cooling water passage that passes through a narrow part of the fuselage, a non-flexible hollow connecting body with a flat upper surface and a wider width in the part corresponding to the narrow part to have a constant cross-sectional area over the entire length is used. A cooling water passage for a water-cooled engine, characterized in that the cooling water passage is arranged along a narrow part of the aircraft body, and cooling water pipes are connected to the front and rear of the hollow connecting body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8991783U JPS59196518U (en) | 1983-06-14 | 1983-06-14 | Cooling water passage of water-cooled engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8991783U JPS59196518U (en) | 1983-06-14 | 1983-06-14 | Cooling water passage of water-cooled engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59196518U JPS59196518U (en) | 1984-12-27 |
| JPH0245470Y2 true JPH0245470Y2 (en) | 1990-12-03 |
Family
ID=30219814
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP8991783U Granted JPS59196518U (en) | 1983-06-14 | 1983-06-14 | Cooling water passage of water-cooled engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59196518U (en) |
-
1983
- 1983-06-14 JP JP8991783U patent/JPS59196518U/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59196518U (en) | 1984-12-27 |
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