JPH0452101Y2 - - Google Patents
Info
- Publication number
- JPH0452101Y2 JPH0452101Y2 JP1985133731U JP13373185U JPH0452101Y2 JP H0452101 Y2 JPH0452101 Y2 JP H0452101Y2 JP 1985133731 U JP1985133731 U JP 1985133731U JP 13373185 U JP13373185 U JP 13373185U JP H0452101 Y2 JPH0452101 Y2 JP H0452101Y2
- Authority
- JP
- Japan
- Prior art keywords
- fuel tank
- duct pipe
- fuel
- vertical plane
- combine
- 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
Landscapes
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Description
【考案の詳細な説明】
(産業上の利用分野)
本考案は、コンバインの燃料タンクのブリーザ
構造の改良に関するものである。[Detailed Description of the Invention] (Industrial Application Field) The present invention relates to an improvement of the breather structure of a fuel tank of a combine harvester.
(従来の技術)
従来のコンバインの燃料タンクのブリーザ構造
は、第3図に示すようにキヤツブ状のブリーザ体
11′から燃料タンク3′内に逆流防止用のダクト
管5′を導入していた。しかし、エンジンのメン
テナンスのためにエンジンカバーをコンバイン本
体に開閉自在に枢着し、このエンジンカバーに燃
料タンク3′を一体的に取り付けた場合には、エ
ンジンカバーの開閉に伴つて燃料が激しく揺れ、
その勢いでダクト管5′の開口7′に燃料が流れ込
んで燃料タンク3′の外に不用意に漏れるという
問題があつた。(Prior Art) The breather structure of the fuel tank of a conventional combine has a duct pipe 5' for preventing backflow introduced into the fuel tank 3' from a cap-shaped breather body 11' as shown in Fig. 3. . However, if the engine cover is pivotally attached to the combine main body so that it can be opened and closed for engine maintenance, and the fuel tank 3' is integrally attached to this engine cover, the fuel will shake violently as the engine cover opens and closes. ,
This caused a problem in that the fuel flowed into the opening 7' of the duct pipe 5' and inadvertently leaked out of the fuel tank 3'.
(考案が解決しようとする問題点)
本考案は、上記の点に鑑みてなされたものであ
つて、その目的とするところは燃料タンクの静置
に近い状態ではダクト管の存在によつて燃料の漏
れを防止でき、また燃料タンクが激しく動いたと
してもダクト管の開口に燃料が流れ込むのを防止
することができるコンバインの燃料タンクのブリ
ーザ構造を提供するにある。(Problems to be solved by the invention) The present invention has been made in view of the above points, and its purpose is to prevent the fuel from flowing due to the presence of the duct pipe when the fuel tank is almost stationary. To provide a breather structure for a fuel tank of a combine, which can prevent fuel from leaking and can also prevent fuel from flowing into an opening of a duct pipe even if the fuel tank moves violently.
(問題点を解決するための手段)
本考案の要旨は、開閉自在にしてコンバイン本
体1に鉛直面内で開閉自在に枢着されるエンジン
カバー2に、燃料タンク3を一体的に取り付たコ
ンバインの燃料タンクのブリーザ構造において、
燃料タンク3の上板に空気抜き孔4を設け、この
空気抜き孔4から燃料タンク3内に空気抜き用ダ
クト管5を導出し、このダクト管5を上記鉛直面
内で且つ燃料タンク3の上板6に沿つて配管する
と共に、ダクト管5の先端を上記鉛直面の側方に
曲成し、ダクト管5の先端の開口7を燃料タンク
3の側壁8に接近して成るコンバインの燃料タン
クのブリーザ構造に係るものである。(Means for Solving the Problems) The gist of the present invention is that a fuel tank 3 is integrally attached to an engine cover 2 that can be opened and closed and pivoted to a combine main body 1 in a vertical plane so that it can be opened and closed. In the breather structure of the combine fuel tank,
An air vent hole 4 is provided in the upper plate of the fuel tank 3, and an air venting duct pipe 5 is led out from the air vent hole 4 into the fuel tank 3. A breather for a fuel tank of a combine harvester is constructed by arranging piping along the vertical plane, bending the tip of the duct pipe 5 to the side of the vertical plane, and making the opening 7 at the tip of the duct pipe 5 close to the side wall 8 of the fuel tank 3. It is related to the structure.
(実施例)
以下、本考案を図示の実施例に基づいて詳述す
る。(Example) Hereinafter, the present invention will be described in detail based on the illustrated example.
2はエンジンカバーであつて、第2図のように
コンバイン本体1にヒンジ9にて鉛直面内での回
転自在となるように取り付けられてある。 Reference numeral 2 denotes an engine cover, which is attached to the combine main body 1 with a hinge 9 so as to be rotatable in a vertical plane, as shown in FIG.
燃料タンク3の上板6には取り付け孔10が穿
孔されてあり、この取り付け孔10にブリーザ体
用の取付パイプ12を挿着してあり、この取付パ
イプ12内を空気抜き孔4としてある。11は空
気孔13を有するキヤツプ状のフリーザ体であつ
て、取付パイプ10に嵌着してある。5はダクト
管であつて、取付パイプ12から燃料タンク3内
に導出されてあり、このダクト管5を上記鉛直面
内で且つ燃料タンク3の上板6に沿つて配管する
と共に、ダクト管5の先端を上記鉛直面の側方に
曲成してあり(図示では略90°)、ダクト管5の先
端の開口7は燃料タンク3の側壁8に近接させて
ある。 An attachment hole 10 is bored in the upper plate 6 of the fuel tank 3, and an attachment pipe 12 for a breather body is inserted into this attachment hole 10, and the inside of this attachment pipe 12 is used as an air vent hole 4. Reference numeral 11 denotes a cap-shaped freezer body having air holes 13, which is fitted onto the mounting pipe 10. Reference numeral 5 denotes a duct pipe, which is led out from the mounting pipe 12 into the fuel tank 3. The tip of the duct pipe 5 is bent to the side of the vertical plane (approximately 90 degrees in the drawing), and the opening 7 at the tip of the duct pipe 5 is located close to the side wall 8 of the fuel tank 3.
しかしてエンジンカバー2の開閉時には、燃料
タンク3の燃料が揺れたとしても、燃料はダクト
管5の外周壁に掛かつても開口7には掛かること
はない。 Therefore, when the engine cover 2 is opened and closed, even if the fuel in the fuel tank 3 is shaken, the fuel will not be applied to the opening 7 even if it is applied to the outer circumferential wall of the duct pipe 5.
14は給油口、15はキヤツプ、16はエンジ
ンである。 14 is a fuel filler port, 15 is a cap, and 16 is an engine.
(効果)
本考案は、上述のように燃料タンクの上板に空
気抜き孔を設け、この空気抜き孔から燃料タンク
内に空気抜き用ダクト管を導出したので、燃料タ
ンクの静置に近い状態ではダクト管の存在によつ
て燃料の漏れを防止できるのは勿論のこと、ダク
ト管を上記鉛直面内で且つ燃料タンクの上板に沿
つて配管すると共に、ダクト管の先端を上記鉛直
面の側方に曲成したので、エンジンカバーの開閉
に伴う燃料タンク内の燃料の揺れ方向に対して側
方に逃げるようにダクト管の開口が向くこととな
り、したがつて燃料タンクが激しく動いたとして
も燃料がその勢いは専らダクト管の周壁に向けら
れることとなり、その結果ダクト管の開口に燃料
が流れ込むことがないという効果を奏する。(Effects) In this invention, as mentioned above, an air vent hole is provided in the upper plate of the fuel tank, and an air venting duct pipe is led out from this air vent hole into the fuel tank. Not only can fuel leakage be prevented by the presence of the duct pipe, but also by installing the duct pipe within the above vertical plane and along the upper plate of the fuel tank, and by placing the tip of the duct pipe on the side of the above vertical plane. Because of the curved shape, the opening of the duct pipe is oriented so that the fuel in the fuel tank sways to the side when the engine cover is opened and closed, so that even if the fuel tank moves violently, the fuel will not flow. The force is directed exclusively toward the peripheral wall of the duct pipe, resulting in the effect that fuel does not flow into the opening of the duct pipe.
しかもダクト管の先端の開口を燃料タンクの側
壁に近接したので、燃料が跳ね返つてダクト管の
開口に入ることがなくなるという効果を奏する。 Moreover, since the opening at the tip of the duct pipe is located close to the side wall of the fuel tank, there is an effect that the fuel will not bounce back and enter the opening of the duct pipe.
第1図a,bは本考案の実施例を示す平面図及
び破断側面図、第2図a,bは同上のエンジンカ
バーの開閉動作の説明図、第3図a,bは従来例
を示す平面図及び破断側面図である。
1……コンバイン本体、2……エンジンカバ
ー、3……燃料タンク、4……空気抜き孔、5…
…ダクト管、6……上板、7……開口、8……側
壁。
Figures 1 a and b are a plan view and a cutaway side view showing an embodiment of the present invention, Figures 2 a and b are explanatory diagrams of the opening and closing operation of the same engine cover, and Figures 3 a and b are a conventional example. They are a top view and a cutaway side view. 1... Combine main body, 2... Engine cover, 3... Fuel tank, 4... Air vent hole, 5...
...Duct pipe, 6...Top plate, 7...Opening, 8...Side wall.
Claims (1)
閉自在に枢着されるエンジンカバーに、燃料タン
クを一体的に取り付たコンバインの燃料タンクの
ブリーザ構造において、燃料タンクの上板に空気
抜き孔を設け、この空気抜き孔から燃料タンク内
に空気抜き用ダクト管を導出し、このダクト管を
上記鉛直面内で且つ燃料タンクの上板に沿つて配
管すると共に、ダクト管の先端を上記鉛直面の側
方に曲成し、ダクト管の先端の開口を燃料タンク
の側壁に近接して成るコンバインの燃料タンクの
ブリーザ構造。 In the combine fuel tank breather structure, the fuel tank is integrally attached to the engine cover, which is pivoted to the combine body in a vertical plane so that it can be opened and closed, and an air vent hole is provided in the top plate of the fuel tank. An air venting duct pipe is guided into the fuel tank from this air vent hole, and this duct pipe is piped within the vertical plane and along the upper plate of the fuel tank, and the tip of the duct pipe is connected to the side of the vertical plane. Combine fuel tank breather structure consisting of a bent opening at the tip of the duct pipe close to the side wall of the fuel tank.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1985133731U JPH0452101Y2 (en) | 1985-08-30 | 1985-08-30 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1985133731U JPH0452101Y2 (en) | 1985-08-30 | 1985-08-30 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6241224U JPS6241224U (en) | 1987-03-12 |
| JPH0452101Y2 true JPH0452101Y2 (en) | 1992-12-08 |
Family
ID=31034310
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1985133731U Expired JPH0452101Y2 (en) | 1985-08-30 | 1985-08-30 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0452101Y2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2670811B2 (en) * | 1988-07-08 | 1997-10-29 | 耕三 平野 | Air suction / exhaust device for liquid tank for carrier |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS4814963U (en) * | 1971-07-01 | 1973-02-20 | ||
| JPS4940101U (en) * | 1972-07-08 | 1974-04-09 | ||
| JPS564560U (en) * | 1979-06-25 | 1981-01-16 |
-
1985
- 1985-08-30 JP JP1985133731U patent/JPH0452101Y2/ja not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6241224U (en) | 1987-03-12 |
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