CN2067360U - Three-stream combustion chamber - Google Patents

Three-stream combustion chamber Download PDF

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Publication number
CN2067360U
CN2067360U CN 90205918 CN90205918U CN2067360U CN 2067360 U CN2067360 U CN 2067360U CN 90205918 CN90205918 CN 90205918 CN 90205918 U CN90205918 U CN 90205918U CN 2067360 U CN2067360 U CN 2067360U
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CN
China
Prior art keywords
combustion chamber
ansa
apart
piston
annulus
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.)
Withdrawn
Application number
CN 90205918
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Chinese (zh)
Inventor
陈士尧
魏熔
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.)
Beijing Institute of Technology BIT
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Beijing Institute of Technology BIT
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 Beijing Institute of Technology BIT filed Critical Beijing Institute of Technology BIT
Priority to CN 90205918 priority Critical patent/CN2067360U/en
Publication of CN2067360U publication Critical patent/CN2067360U/en
Withdrawn legal-status Critical Current

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Abstract

The utility model relates to a combustion chamber used on a high-speed diesel. The utility model further increases the mixture gas quality of the existing combustion chamber, and reduces the depth and the heat load of the combustion chamber. The piston top of the utility model is provided with three circular ring cambered surfaces and two annular arris which are formed by crossing every two adjacent circular ring cambered surfaces, and the center of a piston crown is provided with a conical boss.

Description

Three-stream combustion chamber
The utility model relates to the combustion chamber of using on a kind of high-speed diesel engine.
Disclose a kind of combustion system with double plume on Chinese patent 88106248.0, the structure of the top land of its combustion chamber is, has inside and outside two doughnuts, and the bottom surface circular arc of two doughnuts intersects and forms a pointed arc ridge, and there is a conical boss at center, piston top.After spraying into this combustion chamber, the oil bundle has only two arc surfaces owing to the combustion chamber, can only form two strands of eddy flows, have only an ansa to play comminution of fuel, be unfavorable for further improving mixed gas quality, and the volume that ansa occupies the combustion chamber is more, under the constant situation of combustion chamber volume, be unfavorable for further reducing combustion-chamber depth.
The purpose of this utility model is to overcome above-mentioned the deficiencies in the prior art and a kind of higher mixed gas quality that has is provided, the three stream combustion chambers that combustion-chamber depth reduces.
The technical solution that the utility model is taked is: there is a conical boss at the top land centers of three stream combustion chambers, and its special character is: top land has three annulus cambered surfaces to be intersected the annular ansa form by two annulus cambered surfaces of facing mutually with two.
The utility model has following advantage than prior art:
1, mixed gas quality improves.Because three annulus cambered surfaces are arranged, after spraying into the combustion chamber, the oil bundle just formed three strands of eddy flows, and there are two ansas to play comminution of fuel, so just further improved mixed gas quality, gaseous mixture is distribution uniform in whole combustion chamber, and burning also just evenly, the heat utilization ratio height, the efficiency of combustion height.
2, the thermic load of piston reduces.Be evenly distributed by gaseous mixture, burning is even, and being heated of piston is also just even, the uniformity of temperature profile in its temperature field.
3, combustion-chamber depth reduces.Under the constant situation of combustion chamber volume, three annulus cambered surfaces have replaced two annulus cambered surfaces, the radius of curvature of each annulus cambered surface is reduced relatively, the height that is intersected two ansas that form by two annulus cambered surfaces of facing mutually is also low than an ansa, make the bottom surface, combustion chamber of piston flat relatively like this, reduce burning degree of depth purpose thereby reached.Because combustion-chamber depth reduces, the first piston ring increases apart from the distance of the burning bottom surface of piston on the piston, thereby reduces the thermic load of first ring, and the working condition of first ring is determining the overhaul phase of engine, like this, reduce the service life that first thermic load of encircling can increase engine.
The utility model will be described further in conjunction with the accompanying drawings.
Fig. 1 is a piston of combustion chamber top junction composition.
Fig. 2 is the top land vertical view.
In Fig. 1 and Fig. 2, the top land center has a conical boss 4, boss end face to be lower than plane, piston top.Top land has the arc radius R of 1,2,3, three annulus cambered surfaces of three annulus cambered surfaces 1, R 2, R 3, one of a ratio is little.Two annulus cambered surfaces of facing mutually intersect two annular ansas 5,6 of formation.The conical surface of conical boss 4 and the annulus cambered surface 3 of innermost ring are tangent.In the present embodiment, because R 1And R 2Radius less, and centre-to-centre spacing is bigger, is the height of control ansa 6, draws tangent plane 7 from annulus cambered surface 1 and intersects formation ansa 6 with annulus cambered surface 2, approximate parallel with the conical surface of conical boss 4 from the tangent plane 7 that annulus cambered surface 1 is drawn, the angle of inclination of tangent plane 7 is complementary with the jet angle of oil bundle.Annulus cambered surface 1 directly intersects with plane, piston top.
The meaning of symbol and best value are as follows in the accompanying drawing:
D is a piston diameter.
The combustion chamber openings diameter d 1=(0.66~0.8) D
The diameter d of ansa ring 6 2=(0.4~0.7) D
The diameter d of ansa ring 5 3=(0.13~0.66) D
Annulus cambered surface 1 minimum point is apart from piston top plane H 1=(0.045~0.12) D
Annulus cambered surface 2 minimum points are apart from piston top plane H 2=(0.08~0.14) D
Annulus cambered surface 3 minimum points are apart from piston top plane H 3=(0.066~0.13) D
Ansa 6 is apart from piston top plan range h 1=(0.047~0.10) D
Ansa 5 is apart from piston top plan range h 2=(0.04~0.1) D
The cone angle alpha of conical boss=120 °~150 °.

Claims (2)

1, a kind of three stream combustion chambers, there is a conical boss 4 at its top land center, it is characterized in that: top land has three annulus cambered surfaces 1,2,3 to be intersected the annular ansa 5,6 form by two annulus cambered surfaces of facing mutually with two.
2, according to the described three stream combustion chambers of claim 1, it is characterized in that:
The combustion chamber openings diameter d 1=(0.66~0.8) D
The diameter d of ansa ring 6 2=(0.4~0.7) D
The diameter d of ansa ring 5 3=(0.13~0.66) D
Annulus cambered surface 1 minimum point is apart from piston top plane H 1=(0.045~0.12) D
Annulus cambered surface 2 minimum points are apart from piston top plane H 2=(0.08~0.14) D
Annulus cambered surface 3 minimum points are apart from piston top plane H 3=(0.066~0.13) D
Ansa 6 is apart from piston top plan range h 1=(0.047~0.10) D
Ansa 5 is apart from piston top plan range h 2=(0.04~0.1) D.
CN 90205918 1990-05-10 1990-05-10 Three-stream combustion chamber Withdrawn CN2067360U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 90205918 CN2067360U (en) 1990-05-10 1990-05-10 Three-stream combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 90205918 CN2067360U (en) 1990-05-10 1990-05-10 Three-stream combustion chamber

Publications (1)

Publication Number Publication Date
CN2067360U true CN2067360U (en) 1990-12-12

Family

ID=4886601

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 90205918 Withdrawn CN2067360U (en) 1990-05-10 1990-05-10 Three-stream combustion chamber

Country Status (1)

Country Link
CN (1) CN2067360U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101737145B (en) * 2009-11-06 2011-07-20 北京理工大学 Split swirl combustion chamber
CN103397951A (en) * 2013-08-06 2013-11-20 江苏常工动力机械有限公司 Piston combustion chamber structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101737145B (en) * 2009-11-06 2011-07-20 北京理工大学 Split swirl combustion chamber
CN103397951A (en) * 2013-08-06 2013-11-20 江苏常工动力机械有限公司 Piston combustion chamber structure

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C06 Publication
PB01 Publication
C14 Grant of patent or utility model
GR01 Patent grant
C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee