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JP2553958B2 - Cylinder head device for forced air cooling engine - Google Patents
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JP2553958B2 - Cylinder head device for forced air cooling engine - Google Patents

Cylinder head device for forced air cooling engine

Info

Publication number
JP2553958B2
JP2553958B2 JP2261865A JP26186590A JP2553958B2 JP 2553958 B2 JP2553958 B2 JP 2553958B2 JP 2261865 A JP2261865 A JP 2261865A JP 26186590 A JP26186590 A JP 26186590A JP 2553958 B2 JP2553958 B2 JP 2553958B2
Authority
JP
Japan
Prior art keywords
pipe wall
cylinder head
passage
cooling air
head device
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 - Lifetime
Application number
JP2261865A
Other languages
Japanese (ja)
Other versions
JPH04140459A (en
Inventor
信吉 岩崎
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kubota Corp
Original Assignee
Kubota Corp
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 by Kubota Corp filed Critical Kubota Corp
Priority to JP2261865A priority Critical patent/JP2553958B2/en
Publication of JPH04140459A publication Critical patent/JPH04140459A/en
Application granted granted Critical
Publication of JP2553958B2 publication Critical patent/JP2553958B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は、強制空冷式エンジンのシリンダヘッド装置
に関する。
TECHNICAL FIELD The present invention relates to a cylinder head device for a forced air cooling type engine.

[従来の技術] 従来、強制空冷式エンジンのシリンダヘッド装置とし
て、第3図(A)に示すように、シリンダヘッド51内に
冷却風通路を形成し、冷却風通路54内に排気ポート管壁
52の管壁中間寄り部53を横断状に臨ませ、管壁中間寄り
部53の上下に通路連続用隙間56・57を残したものがある この装置は、排気ポート管壁52の管壁中間寄り部53が
排気の絞り抵抗となるのを回避するため、第3図(B)
・(C)に示すように、管壁中間寄り部53の上下幅53a
と管壁終端寄り部55の上下幅55aと一致させ、かつ管壁
中間寄り部53の横幅53bを管壁終端寄り部55の寄り幅55b
と一致させ、これにより管壁中間寄り部53内の通路断面
積が管壁終端寄り部55内の通路断面積と同程度の大きさ
を保てるようにしてある。
[Prior Art] Conventionally, as a cylinder head device of a forced air cooling type engine, as shown in FIG. 3 (A), a cooling air passage is formed in a cylinder head 51, and an exhaust port pipe wall is provided in a cooling air passage 54.
There is a device in which the pipe wall intermediate portion 53 of 52 is faced in a crosswise manner, and gaps 56 and 57 for passage continuity are left above and below the pipe wall intermediate portion 53. In order to prevent the leaning portion 53 from becoming a throttle resistance of the exhaust gas, FIG. 3 (B)
・ As shown in (C), the vertical width 53a of the tube wall intermediate portion 53
And the vertical width 55a of the pipe wall end portion 55, and the lateral width 53b of the pipe wall middle portion 53 is set to the pipe wall end portion 55 side width 55b.
Therefore, the cross-sectional area of the passage in the tube wall intermediate portion 53 can be maintained at the same level as the cross-sectional area of the passage in the tube wall end portion 55.

[発明が解決しようとする課題] 上記従来技術では、次の問題がある。[Problems to be Solved by the Invention] The above-mentioned conventional techniques have the following problems.

エンジンをコンパクト化するため、シリンダヘッド51
の全高を低くしなければならない場合には、第3図
(A)に示すように、管壁中間寄り部53が比較的大きく
なるこの従来のものでは、通路連続用隙間56・57の通路
断面積が小さくなり、排気ポート管壁52の冷却性能が低
く、その過熱によりシリンダヘッド51全体に熱歪が生
じ、クラックの発生やヘッドガスケットからのガス漏れ
が生じる。
Cylinder head 51 to make the engine compact
When it is necessary to reduce the overall height of the pipe, as shown in FIG. 3 (A), the pipe wall intermediate portion 53 is relatively large. The area becomes small, the cooling performance of the exhaust port pipe wall 52 is low, and overheating thereof causes thermal strain in the entire cylinder head 51, causing cracks and gas leakage from the head gasket.

シリンダヘッド51の鋳造には、通路連続用隙間56・57
等の中空部分を形成するため、その中空部分を型どった
鋳砂の中子を用いるが、通路連続用隙間56・57が狭くな
るこの従来のものでは、通路連続用隙間56・57を型どる
中子部分が細くなり、鋳造中にここが損傷し易いうえ、
鋳造後の鋳砂抜きも狭い通路連続用隙間56・57からは行
い難く、シリンダヘッド41の鋳造が困難となる。
For casting the cylinder head 51, the passage continuity gaps 56 and 57 are used.
In order to form a hollow part such as a hollow core, a molding sand core is used to model the hollow part, but the gap 56/57 for passage continuity becomes narrower. The core part becomes thinner, and it is easy to damage it during casting.
It is also difficult to perform sand removal after casting from the narrow passage continuation gaps 56 and 57, which makes casting of the cylinder head 41 difficult.

本発明は、シリンダヘッドの全高を低く維持できなが
らも、通路連続用隙間の通路断面積を大きく確保できる
ようにすること、をその課題とする。
An object of the present invention is to make it possible to secure a large passage cross-sectional area of a passage continuation gap while keeping the overall height of a cylinder head low.

[課題を解決するための手段] 本発明は、第1図(A)に示すように、シリンダヘッ
ド1内に冷却風通路4を形成し、冷却風通路4内に排気
ポート管壁2の管壁中間寄り部3を横断状に臨ませ、第
1図(B)に示すように、管壁中間寄り部3の上下に通
路連続用隙間6・7を残した、強制空冷エンジンのシリ
ンダヘッド装置において、第1図(C)・(D)に示す
ように、排気ポート管壁2の管壁中間寄り部3は冷却風
通路4の通路形成方向に長い横偏平状に形成し、排気ポ
ート2の管壁中間寄り部3の上下幅3aは管壁終端寄り部
5の上下幅5aよりも狭く、管壁中間寄り部3の横幅3bは
管壁終端寄り部5の横幅5bよりも広く形成したものであ
る。
[Means for Solving the Problem] As shown in FIG. 1 (A), the present invention forms a cooling air passage 4 in a cylinder head 1 and a pipe of an exhaust port pipe wall 2 in the cooling air passage 4. A cylinder head device for a forced air-cooled engine in which a wall-intermediate-portion 3 is transversely faced, and passage continuation gaps 6 and 7 are left above and below the pipe wall-intermediate portion 3, as shown in FIG. 1 (B). As shown in FIGS. 1 (C) and 1 (D), the pipe wall intermediate portion 3 of the exhaust port pipe wall 2 is formed in a horizontal flat shape that is long in the passage forming direction of the cooling air passage 4. The vertical width 3a of the tube wall middle part 3 is narrower than the vertical width 5a of the tube wall end part 5 and the lateral width 3b of the tube wall middle part 3 is wider than the lateral width 5b of the tube wall end part 5. It is a thing.

[作用] 本発明は、次のように作用する。[Operation] The present invention operates as follows.

エンジンのコンパクト化を図るために、シリンダヘッ
ドの全高を低く形成しなければならない場合でも、第1
図(C)・(D)に示すように、管壁中間寄り部3はそ
の上下幅3aが管壁終端寄り部5の上下幅5aよりも狭くな
る程度に偏平化されているので、第1図(B)に示すよ
うに、通路連続用隙間6・7の通路断面積を大きく形成
できる。
Even if the overall height of the cylinder head has to be reduced in order to make the engine compact, the first
As shown in FIGS. (C) and (D), the tube wall middle portion 3 is flattened to such an extent that the vertical width 3a thereof is narrower than the vertical width 5a of the tube wall terminal end portion 5; As shown in FIG. 6B, the passage cross-sectional area of the passage continuity gaps 6 and 7 can be increased.

通路連続用隙間6・7の通路断面積を大きく形成でき
るため、通路連続用隙間6・7を型どる中子部分も太く
でき、鋳造途中にここが破損するおそれが少なくなるう
え、鋳造後の鋳砂抜きも広い通路連続用隙間6・7を介
して容易に行うことができる。
Since the passage cross-sectional areas of the passage continuity gaps 6 and 7 can be made large, the core portion that models the passage continuity gaps 6 and 7 can be made thicker, which reduces the risk of breakage during casting and also reduces The sand removal can also be easily performed through the wide passage continuation gaps 6 and 7.

第1図(C)・(D)に示すように、管壁中間寄り部
3はその横幅3bが管壁終端寄り部5の横幅5bよりも広く
なる程度に偏平化されているので、管壁中間寄り部3内
には必要な大きさの通路断面積が確保でき、ここが排気
の絞り抵抗となることはなく、掃気効率の低下を生じる
おそれはない。
As shown in FIGS. 1 (C) and (D), the tube wall middle part 3 is flattened so that the lateral width 3b thereof is wider than the lateral width 5b of the tube wall end part 5 so that the tube wall is flattened. A passage cross-sectional area of a required size can be secured in the middle portion 3, and this does not serve as throttling resistance of exhaust gas, and there is no fear that the scavenging efficiency will decrease.

[効果] 本発明は、次の効果を奏する。[Effect] The present invention has the following effects.

エンジンのコンパクト化を図るために、シリンダヘッ
ドの全高を低く形成しなければならない場合であって
も、通路連続用隙間の通路断面積を大きく形成できるの
で、排気ポート管壁の冷却性能の低下がなく、その過熱
によるシリンダヘッド全体の熱歪を防止でき、クラック
の発生やヘッドガスケットからのガス漏れを防止でき
る。
Even if the overall height of the cylinder head has to be made low in order to make the engine compact, the passage cross-sectional area of the passage continuity gap can be made large, so that the cooling performance of the exhaust port pipe wall is reduced. It is possible to prevent thermal distortion of the entire cylinder head due to the overheating, and to prevent cracks and gas leakage from the head gasket.

通路連続用隙間の通路断面積を大きく形成できるた
め、通路連続用隙間を型どる中子部分も太くでき、鋳造
途中にここが損傷するおそれがすくなくなるうえ、鋳造
後の鋳砂抜きも広い通路連続用隙間を介して容易に行う
ことができ、シリンダヘッドの製造が容易に行える。
Because the passage cross-sectional area of the passage continuity gap can be made large, the core part that molds the passage continuity gap can be made thicker, and there is less risk of damage to this core during casting, and wide sand removal after casting is also possible. This can be easily performed through the continuous gap, and the cylinder head can be easily manufactured.

[実施例] 本発明の実施例を図面に基づいて説明する。[Embodiment] An embodiment of the present invention will be described with reference to the drawings.

第2図において、符号11は縦形直列二気筒ディーゼル
エンジンを示している。
In FIG. 2, reference numeral 11 indicates a vertical in-line two-cylinder diesel engine.

このエンジン11は、クランクケース12の上側に前後方
向に並設した前後部シリンダ13・14を設け、前後部シリ
ンダ13・14の上側にヘッドガスケット15を介してシリン
ダヘッド1を組み付け、クランクケース12の前側に冷却
ファン16を収容したファンケース17を取り付けて構成し
てある。
The engine 11 is provided with front and rear cylinders 13 and 14 arranged side by side in the front-rear direction on the upper side of a crankcase 12, and the cylinder head 1 is assembled on the upper side of the front and rear cylinders 13 and 14 with a head gasket 15 interposed therebetween. A fan case 17 accommodating a cooling fan 16 is attached to the front side of the.

第1図(A)に示すように、シリンダヘッド1内に
は、ヘッド左半部の前後方向中央に前後部シリンダ13・
14の各副燃焼室18・18を一連に取り囲む油冷ジャケット
19を設け、その前後壁20・21に沿って前後部シリンダ13
・14の各吸気ポート22・23を横向きに形成し、ヘッド右
半部の前後方向中央に前後部シリンダ13・14の共通の排
気ポート24を形成する排気ポート管壁2を油冷ジャケッ
ト19の右側から右向きに形成し、ヘッド右端縁部に前後
タペット室25・26を形成し、前後タペット室25・26に沿
って前後方向に一連の冷却風通路4を形成している。
As shown in FIG. 1 (A), in the cylinder head 1, the front and rear cylinders 13
Oil cooling jacket that surrounds each of the 14 sub-combustion chambers 18 in series
19 are provided, and the front and rear cylinders 13 are provided along the front and rear walls 20 and 21.
The exhaust port pipe wall 2 forming the intake ports 22 and 23 of 14 sideways and forming the common exhaust port 24 of the front and rear cylinders 13 and 14 at the center of the front right and left direction of the head right half part of the oil cooling jacket 19 The front and rear tappet chambers 25 and 26 are formed at the right end of the head from the right side, and a series of cooling air passages 4 are formed in the front and rear direction along the front and rear tappet chambers 25 and 26.

排気ポート管壁2は二又状の管壁始端寄り部27と管壁
中間寄り部3と管壁終端寄り部5とからなり、管壁中間
寄り部3は冷却風通路4内に横断状に臨ませ、管壁終端
寄り部5は前後タペット室25・26間に形成してある。
The exhaust port pipe wall 2 comprises a bifurcated pipe wall start end portion 27, a pipe wall middle portion 3 and a pipe wall end portion 5 which are transverse to the cooling air passage 4. The pipe wall end-approximating portion 5 is formed between the front and rear tappet chambers 25 and 26.

冷却風通路4の前端部31はファンケース17(第2図参
照)に臨ませ、冷却風通路4の後端部33は大気中に解放
させ、第1図(B)に示すように、管壁中間寄り部3の
上下には通路連続用隙間6・7を残し、冷却風34を冷却
風通路4に沿ってシリンダヘッド1内の前側から後側に
通風させるようにしてある。
The front end portion 31 of the cooling air passage 4 faces the fan case 17 (see FIG. 2), and the rear end portion 33 of the cooling air passage 4 is opened to the atmosphere, and as shown in FIG. Passage continuation gaps 6 and 7 are left above and below the wall middle portion 3 to allow the cooling air 34 to flow along the cooling air passage 4 from the front side to the rear side in the cylinder head 1.

第1図(C)・(D)に示すように、排気ポート管壁
2の管壁中間寄り部3及び管壁終端寄り部5はいずれも
冷却風通路4の通路形成方向に長い横偏平の矩形状に形
成してあるが、排気ポート管壁2の管壁中間寄り部3の
上下幅3aは管壁終端寄り部5の上下幅5aよりも狭く、管
壁中間寄り部3の横幅3bは管壁終端寄り部5の横幅5bよ
りも広く形成してある。
As shown in FIGS. 1 (C) and 1 (D), the exhaust port pipe wall 2 has a pipe wall middle portion 3 and a pipe wall end portion 5 each having a lateral flat shape that is long in the passage forming direction of the cooling air passage 4. Although it is formed in a rectangular shape, the vertical width 3a of the pipe wall intermediate portion 3 of the exhaust port pipe wall 2 is narrower than the vertical width 5a of the pipe wall terminal portion 5 and the horizontal width 3b of the pipe wall intermediate portion 3 is It is formed wider than the lateral width 5b of the end portion 5 near the end of the tube wall.

第1図(B)に示すように、管壁終端寄り部5の下方
には下通路連続用隙間7から右側に分岐する冷却風分岐
通路35を形成して、管壁終端寄り部5も空冷できるよう
にし、また、第1図(A)に示すように、後タペット室
26の空壁から冷却風通路4内に後側の吸気ポート管壁36
方向に伸びる冷却風偏向壁37を突出させ、この冷却風偏
向壁37で偏向された冷却風34で後側の吸気ポート管壁36
を空冷できるようにしてある。
As shown in FIG. 1 (B), a cooling air branch passage 35 that branches to the right from the lower passage continuity gap 7 is formed below the pipe wall end portion 5 and the pipe wall end portion 5 is also air-cooled. And as shown in FIG. 1 (A), the rear tappet chamber
From the empty wall of 26 into the cooling air passage 4, the intake port pipe wall 36 on the rear side
The cooling air deflecting wall 37 extending in the direction, and the cooling air 34 deflected by the cooling air deflecting wall 37 causes the rear intake port pipe wall 36
So that it can be air-cooled.

油冷ジャケット19へのオイルの供給は、第2図に示す
ように、オイルパン38内のオイル39をオイルポンプ40の
圧送力により、リリーフバルブ41、シリンダ間ジャケッ
ト42を順に経由させて行い、油冷ジャケット19からオイ
ルパン38へのオイルもどしは、オイルクーラ43を経由さ
せて行うようになっている。
As shown in FIG. 2, the oil is supplied to the oil cooling jacket 19 through the relief valve 41 and the inter-cylinder jacket 42 in order by the oil 39 in the oil pan 38 by the pumping force of the oil pump 40. The oil is returned from the oil cooling jacket 19 to the oil pan 38 via the oil cooler 43.

第1図(A)に示すように、油冷ジャケット19の左側
には鋳砂抜き口44をあけ、ここを吸気マニホールド45の
マニホールド管壁46で蓋してある。
As shown in FIG. 1 (A), a sand removal port 44 is opened on the left side of the oil cooling jacket 19 and is covered with a manifold pipe wall 46 of the intake manifold 45.

また、油冷ジャケット19と吸気ポート22・23との間に
位置するフランジ対向部47にはガスケット48を挟んで対
向する漏洩オイル遮断溝49を設け、油冷ジャケット19内
のオイル39がフランジ対向部47での毛管現象で吸気ポー
ト22・23に浸透するのを防止できるようにしてある。
Further, a leakage oil cut-off groove 49 is provided in the flange facing portion 47 located between the oil cooling jacket 19 and the intake ports 22 and 23 so as to sandwich the gasket 48, and the oil 39 in the oil cooling jacket 19 faces the flange. The capillarity of the portion 47 prevents the permeation into the intake ports 22 and 23.

【図面の簡単な説明】[Brief description of drawings]

第1図は本発明の実施例に係るシリンダヘッド装置を説
明する図で、第1図(A)はシリンダヘッド装置の横断
面平面図、第1図(B)は第1図(A)のB−B線断面
図、第1図(C)は第1図(B)のC−C線断面図、第
1図(D)は第1図(B)のD−D線断面図である。 第2図は本発明の実施例に係るシリンダヘッド装置を組
み付けたエンジンの縦断面側面図である。 第3図は従来技術を説明する図で、第3図(A)は第1
図(B)相当図、第3図(B)は第3図(A)のB−B
線断面図、第3図(C)は第3図(A)のC−C線断面
図である。 1……シリンダヘッド、2……排気ポート管壁、3……
2の管壁中間寄り部、3a……3の上下幅、3b……3の横
幅、4……冷却風通路、5……2の管壁終端寄り部、5a
……5の上下幅、5b……5の横幅、6・7……通路連続
用隙間。
FIG. 1 is a view for explaining a cylinder head device according to an embodiment of the present invention. FIG. 1 (A) is a cross-sectional plan view of the cylinder head device, and FIG. 1 (B) is a view of FIG. 1 (A). FIG. 1 (C) is a sectional view taken along line CC of FIG. 1 (B), and FIG. 1 (D) is a sectional view taken along line DD of FIG. 1 (B). . FIG. 2 is a vertical sectional side view of an engine in which a cylinder head device according to an embodiment of the present invention is assembled. FIG. 3 is a diagram for explaining the prior art, and FIG.
FIG. 3B is equivalent to FIG. 3B, and FIG. 3B is BB of FIG. 3A.
FIG. 3C is a sectional view taken along line CC of FIG. 3A. 1 ... Cylinder head, 2 ... Exhaust port pipe wall, 3 ...
2 pipe wall middle portion, 3a …… 3 vertical width, 3b …… 3 horizontal width, 4 …… cooling air passage, 5 …… 2 pipe wall end portion, 5a
…… 5 vertical width, 5b …… 5 horizontal width, 6.7 …… Gap for continuous passage.

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】シリンダヘッド1内に冷却風通路4を形成
し、冷却風通路4内に排気ポート管壁2の管壁中間寄り
部3を横断状に臨ませ、管壁中間寄り部3の上下に通路
連続用隙間6・7を残した、強制空冷エンジンのシリン
ダヘッド装置において、 排気ポート管壁2の管壁中間寄り部3は冷却風通路4の
通路形成方向に長い横偏平状に形成し、 排気ポート2の管壁中間寄り部3の上下幅3aは管壁終端
寄り部5の上下幅5aよりも狭く、管壁中間寄り部3の横
幅3bは管壁終端寄り部5の横幅5bよりも広く形成した ことを特徴とする強制空冷式エンジンのシリンダヘッド
装置。
A cooling air passage (4) is formed in a cylinder head (1), and a pipe wall intermediate portion (3) of an exhaust port pipe wall (2) is made to face the cooling air passage (4) in a transverse manner. In a cylinder head device for a forced air-cooled engine, in which upper and lower passage gaps 6 and 7 are left, the pipe wall middle portion 3 of the exhaust port pipe wall 2 is formed in a horizontal flat shape that is long in the passage forming direction of the cooling air passage 4. However, the vertical width 3a of the pipe wall middle portion 3 of the exhaust port 2 is narrower than the vertical width 5a of the pipe wall end portion 5 and the horizontal width 3b of the pipe wall middle portion 3 is the horizontal width 5b of the pipe wall end portion 5. Cylinder head device for forced air-cooled engines characterized by being formed wider than
JP2261865A 1990-09-29 1990-09-29 Cylinder head device for forced air cooling engine Expired - Lifetime JP2553958B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2261865A JP2553958B2 (en) 1990-09-29 1990-09-29 Cylinder head device for forced air cooling engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2261865A JP2553958B2 (en) 1990-09-29 1990-09-29 Cylinder head device for forced air cooling engine

Publications (2)

Publication Number Publication Date
JPH04140459A JPH04140459A (en) 1992-05-14
JP2553958B2 true JP2553958B2 (en) 1996-11-13

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JP2261865A Expired - Lifetime JP2553958B2 (en) 1990-09-29 1990-09-29 Cylinder head device for forced air cooling engine

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JP2011247270A (en) * 2011-08-11 2011-12-08 Toyota Motor Corp Port structure of internal combustion engine

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JPH04140459A (en) 1992-05-14

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