TJ-JET CHAMBER OF A GASOLINE ENGINE

Abstract: The invention relates to a new TJ-jet chamber which has broken through the conventional structure of the combustion chamber of a gasoline engine. In addition to changes of the shape of the combustion chamber and the position of the spark plug, one or two special-designed jet holes are prov­ ided. Thereby a peculiar turbulence is produced inside the combustion chamber, including a great deal of turbulence of microscale which increases the propagation speed of the flame greatly through the jet holes. With this, the flame can reach the farthest end from the spark plug at great speed as to depress detonation in the end gas and to obtain an ideal rate of heat-release. The invention can be applied to all overhead valve gasol­ ine engines.

Description: TJ-Jet Chamber of a Gasoline Engine The invention relates to the technical field of internal combustion engines and in particular to a combustion chamber of a gasoline engine. A gasoline engine is a power device in a car. To optimize its performance is the premise of the optimization of the car performance. Since last century, specialists at home and abroad have strived to attain the aim unremittingly for this purpose. At present the compression ratio of common car-used gasoline engines in foreign countries, while using unleaded gasoline (RON value 90-93), is about 8,5-9,0. Their engine performance is as follows: Minimum specific fuel consumption of 200-205 g/HP. hour maximum mean effective pressure of 9-9,5 kg/cm2, Human being, however, are not content with the achieved accomplishment and during recent decades, people have put a great deal of research into the gasoline engine and achieved a great success in this field. Especially outstanding among them are: 1) May Fireball Chamber in Switzerland, reference is made to SAE papers, Series No 790386 and 810786; 2) British High Compression Ratio Compact Chamber produced by Ricardo Ltd., reference is made to SAE papers, Series No 820166 and A.E journal Feb.-March 1982; 3) Top Chamber produced by Porsche in F.R.G., reference is made to MTZ journal May 1984. The following are other chambers developed in this field: 4) MCA-jet chamber developed by Mitsubishi CO in Japan, reference is made to "Automative Engineering" journal April 1975; 5) Tornado chamber developed by Danish University, referen ce is made to SAE papers, series No 810786; 6) Audi Combustion System in F.R.G., reference is made to West German "Automobil Industrie" journal issue 1, 2, 3, 1982. The above-mentioned former three chambers are put into trial production. Their performances are superior, though these engines had to use premium gasoline (high octane number). Premium gasoline, however, in the refining process needs more energy. In view of energy preservation these former products are not ideal. The object of this invention lies in decreasing specific fuel consumption in car-used gasoline engines, increasing economical results and saving energy. By using the lower octane number gasoline (domestic NO 70 regular gasoline RON 86), inside the chamber of gasoline engine burned the leaner gas mixture which is of benefit for reducing specific fuel consumption. In addition, it has been proved in theory and practice that an increase in the compression ratio of the gasoline engine is an effective means to decrease its specific fuel consumption. However, the compression ratio cannot be increased unlimitedly, otherwise it may cause in the engine abnormal combustiondetonations which would cause serious damage to the gasoline engine and would sharply decrease its performance. Therefore the present invention proposes a new structure of a TJ-jet chamber. As a result of this new structure, detonations inside the chamber can be depressed, the difficulties in connection with an increase of the compression ratio can be overcome and the performance of the gasoline engine can be further optimized. The TJ-jet chamber of the gasoline engine of this invention is breaking through the conventional structure of the combustion chamber of a gasoline engine. It comprises an intake valve (1), an exhaust valve (2), a combustion chamber (3), a clearance (4) between piston and cylinder head, a spark plug (5), a jet hole (6), a cylinder head (7) and a piston (8). As shown in Fig 1 and Fig 2 the combustion chamber (3) is disposed in the cylinder head, located under the exhaust valve in the shape of a cylinder. In the sidewall there exists a special hole for the jet. That's why it was named the TJ-jet chamber. The number of jet holes, their position and size are of crucial importance for the engine performance, but all these must depend on the diameter of the cylinder and the stroke of the piston. By utilizing upward compression of piston before burning fuel and expansion of gas after burning them a strong-turbulence of different scales is formed in the combustion chamber (3) and the main chamber (4). Especially, a great deal of turbulence of microscale can be produced through the jetholes. Because of this phenomenon the flame propagation speed is greatly raised and it reaches the farthest end from the spark plug at great speed, so that detonation is depressed. At the same time, in the later period of combustion, the rate of heat-release is extremely fast. Then, a sophisticated heat-release can be achieved. If domestic gasoline engine 4920 is changed over to the TJ-jet chamber with burning RON 86 gasoline, the compression ratio can be increased from 7.2 to 10, the lowest specific fuel consumption becomes 180 g/HP. hour and the maximum mean effective pressure is increased to 9.7 kg/cm2. These data have attained world advanced level. The changes of the shape of the combustion chamber (3) and the position of the spark plug, all play an active role in optimizing the performance, but the key point remain the jet holes which were special-designed. The upper end of their center is opposite the exhaust valve (2) and the lower end of their center is farthest from the spark plug. Its main roles are as follows: 1) Due to the compression of the piston1 a great deal of turbulence of microscale is formed around the spark plug which is of benefit to the ignition; 2) The mixed gases are in ignition after the flame propaga tes outward through the jet holes and the flame front can be led to the region of the detonation center as to depress the detonation; 3) Inside the TJ-jet chamber (3), the higher is the com pression ratio or load; the stronger becomes the inten sity; the less is the size of the turbulence of micro scale caused by the jet holes; therefore the more grows the propagation speed of the flame. All these functions can raise the potential of depressing detonation which always occurs during a higher compression ratio and bigger load; 4) Through the jet holes1 turbulence of microscale is pro duced inside the main chamber as soon as the flame front reaches, so that, before the short-life turbulence of microscale disappears, they have been made full use of to raise the propagation speed of the flame greatly; 5) In the course of combustion, through the jet holes 2 separate-developed combustion regions are formed, these increase the area of the flame front a great deal during the later period of combustion. However, the combustion speed is so fast that a sophisticated heat-release pat tern can be given, simultaneously the temperature of the exhaust and heat-stress become decreased. During the high load, as a result of fast speed of combustion the advanced angle of ignition will be reduced. With this there are some attached advantages: 1) It is of benefit for depressing detonation and further increasing the compression ratio; 2) The highest combustion pressure and mechanical stress can be lowered; 3) Combustion noise can be lowered; 4) Nox in the exhaust can be lowered. As compared with prior art, the key feature of this invention is, that in the case of using low octane gasoline, compression ratio is raised while domestic gasoline engine 4920 is changed over to TJ-jet chamber and its type No is 4920S. Its performance is higher than the products of foreign gasoline engine and at the same time, the fuel economy is just the same as with the gasoline engine with high compression ratio which has been developed recently abroad. Besides, Premium gasoline of high octane number is needed in foreign newly developed gasoline engines, as shown by the following table in detail. This invention can be adapted to all overhead valve engines. In the attached drawings of the invention: Fig 1 is a top view of the TJ-jet chamber; Fig 2 is a cross section view of TJ-jet chamber; The following table gives a performance comparison between gasoline engines with high compression ratio. The following embodiment works on the domestic 4920 gasoline engine which is based on said invention: : 50 so mm = 40 mm diameter of jet hole = 10 mm a = 29,5 mm b = 15 mm c = 5,5 oC= 32 ss=38 30' TABLE Performance Comparison Between Gasoline Engines With High Compression Ratio EMI6.1 <tb> <SEP> ce <tb> <SEP> IC(V <tb> <SEP> acl <tb> r, <SEP> [O <tb> b <tb> <SEP> parameter <SEP> octane <SEP> nunber <SEP> of <SEP> cmpression <SEP> lowest <SEP> specific <SEP> fuel <SEP> rnaxnturn <SEP> mean <SEP> efective <tb> <SEP> cu <tb> <SEP> -H <SEP> r <tb> <SEP> o <tb> <SEP> uz <SEP> t <tb> <SEP> o <tb> <SEP> o <tb> <SEP> n <tb> <SEP> oz <tb> <SEP> o <tb> <SEP> g <tb> <SEP> 4 <tb> <SEP> o <tb> <SEP> 04k <tb> <SEP> Q <tb> <SEP> L <SEP> r1 <tb> <SEP> O <tb> <SEP> \ <SEP> a0 <tb> <SEP> \ <SEP> EW <tb> <SEP> \ <SEP> Hk <tb> <SEP> 4J <SEP> Ss <SEP> \ <tb> car-used gasoline 90-93 8.5-9.0 200-205 9-9.5 engine abroad May Fireball chamber 97 11 180 11.4 in Switzerland (high octane NO gasoline) Ricardo high chamber in compression piston 103 11 190 10.1 ratio compact chamber chamber in British cylinder 96 11 190 9.5 head Porsche 98 10.6 191 10.3 TOP chamber in F.R.G 92 9.5 206 9.4 TU-jet chamber (invention) 86 10 190 9.7

Claims: Claims 1) An overhead-valve combustion chamber of a gasoline engi ne, characterized in that the combustion chamber (3) is located in the cylinder head (7) of a gasoline engine under the exhaust valve (2), that in the side wall there exist one or two jet holes (6), whereby the upper end of the axis of the jet holes (6) is opposite the exhaust valve (2) and at the same time the lower end of the axis of the jet holes (6) is as far remote from the spark plug (5) as possible. 2) The combustion chamber as claimed in claim 1 character ized in that its shape is nearly cylindrical, whereby the cylinder in gasoline engines of small diameter, the shape can be cylindrical with taper at the lower end. 3) The combustion chamber as claimed in claim 1 character ized in that the diameter of the jet holes (6) depends on the displacement of the gasoline engine whereby that in domestic 4920S gasoline engines is 10-12 mm. 4) The combustion chamber as claimed in claim 1 and 2 cha racterized in that the cC-angle of the jet hole in the 4920S gasoline engine is 30"-34", the (3-angle 37 -40 . 5) The combustion chamber as claimed in Claim 1 character ized in that its spark plug (5) is located below the exhaust valve (2).

Inventors: JIEPING, LIU THERMOPHYSICS ENG. DEPT., JIUJING, SHANG THERMOPHYSICS ENG. DEPT., SHINXIONG, WAN THERMOPHYSICS ENG. DEPT., YINGLONG, LIU THERMOPHYSICS ENG. DEPT., YOUJUN, LIU THERMOPHYSICS ENG. DEPT.
Applicants: TIANJIN UNIVERSITY
Application year: 1986
Main classification: F02B23
IPC codes: F02B23, F02B19, F02B1