JPH0373621U - - Google Patents

Info

Publication number
JPH0373621U
JPH0373621U JP13632489U JP13632489U JPH0373621U JP H0373621 U JPH0373621 U JP H0373621U JP 13632489 U JP13632489 U JP 13632489U JP 13632489 U JP13632489 U JP 13632489U JP H0373621 U JPH0373621 U JP H0373621U
Authority
JP
Japan
Prior art keywords
wall
exhaust port
water jacket
cylinder
cooling structure
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.)
Pending
Application number
JP13632489U
Other languages
Japanese (ja)
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 JP13632489U priority Critical patent/JPH0373621U/ja
Publication of JPH0373621U publication Critical patent/JPH0373621U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

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

第1図は本考案に係る2サイクルエンジンのシ
リンダ部分の断面図、第2図は第1図の−線
断面図である。 尚、図面中1……シリンダ、3……排気ポート
、5……厚肉部、W……ウオータージヤケツト、
W1……延長部である。
FIG. 1 is a sectional view of a cylinder portion of a two-stroke engine according to the present invention, and FIG. 2 is a sectional view taken along the line -- in FIG. In the drawings, 1... cylinder, 3... exhaust port, 5... thick wall part, W... water jacket,
W1... is an extension part.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 2サイクルエンジンのシリンダの壁部内にウオ
ータージヤケツトを形成した冷却構造において、
前記シリンダの壁部を排気ポート周囲で厚肉に形
成し、この厚肉部内に前記ウオータージヤケツト
を延長して形成し、この延長部分で前記排気ポー
トの周囲を囲繞したことを特徴とする2サイクル
エンジンの冷却構造。
In a cooling structure in which a water jacket is formed within the cylinder wall of a two-stroke engine,
2. The wall of the cylinder is formed thick around the exhaust port, the water jacket is extended into the thick wall, and the extended portion surrounds the exhaust port. Cycle engine cooling structure.
JP13632489U 1989-11-24 1989-11-24 Pending JPH0373621U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13632489U JPH0373621U (en) 1989-11-24 1989-11-24

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13632489U JPH0373621U (en) 1989-11-24 1989-11-24

Publications (1)

Publication Number Publication Date
JPH0373621U true JPH0373621U (en) 1991-07-24

Family

ID=31683536

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13632489U Pending JPH0373621U (en) 1989-11-24 1989-11-24

Country Status (1)

Country Link
JP (1) JPH0373621U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106545432A (en) * 2016-10-19 2017-03-29 北京航空航天大学 A kind of semi-wet formula water cooling system towards two-stroke Heavy End Aviation Fuel piston engine combination type combustor
CN107060986A (en) * 2016-10-19 2017-08-18 北京航空航天大学 One kind is used for the piston-engined combined type combustion chamber of two stroke Heavy End Aviation Fuels
CN108661818A (en) * 2018-05-31 2018-10-16 长沙光华航空科技有限公司 A kind of engine liquid cold cylinder cylinder body and the engine liquid cooling cylinder with the cylinder body

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60132049A (en) * 1983-12-19 1985-07-13 Honda Motor Co Ltd Cooling water mechanism for 2 cycle engine

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60132049A (en) * 1983-12-19 1985-07-13 Honda Motor Co Ltd Cooling water mechanism for 2 cycle engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106545432A (en) * 2016-10-19 2017-03-29 北京航空航天大学 A kind of semi-wet formula water cooling system towards two-stroke Heavy End Aviation Fuel piston engine combination type combustor
CN107060986A (en) * 2016-10-19 2017-08-18 北京航空航天大学 One kind is used for the piston-engined combined type combustion chamber of two stroke Heavy End Aviation Fuels
CN108661818A (en) * 2018-05-31 2018-10-16 长沙光华航空科技有限公司 A kind of engine liquid cold cylinder cylinder body and the engine liquid cooling cylinder with the cylinder body

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