US4401071A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Injection and mixture formation process and apparatus to implement same
Assignee: MAN AG
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Filing: 1981-01-07
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Granted: 1983-08-30
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Expires: 2001-01-07
Abstract
Abstract The invention sets forth a method and apparatus for improving the injection and mixture of fuel and air in air-compressing combustion engines. The fuel is admitted into a rotationally symmetrical combustion chamber in such a manner that all droplets of the fuel stream are finely atomized at all speed and/or load ranges of the engine, and that the complete spray on entering the combustion chamber is so broken up that, from the combustion chamber wall to a point approximately one third of the combustion chamber radius, the broken-up spray matches the combustion chamber geometry, the injection of the fuel being effected in such a manner as to match the velocity and/or density distribution of the combustion air which rotates in the combustion chamber.
Inventors
- 👤 Hans-Jurgen Zurner
- 👤 Wolfram Emmerling
- 👤 Werner Steimer
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 01:30
CPC Classifications
F; F02; F02B; F02B23/00; F02B23/02; F02B23/06; F02B23/0645; F02B23/0669; F02B23/0636; F02B23/066; F02B23/0666; F02B2275/00; F02B2275/14; F02B2275/40; F02B23/0618; F02B23/0621; F02B23/0624; F02B3/00; F02B3/06; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
229 words
Process for introducing and mixing combustion air and fuel in air compressing, self-igniting, internal combustion engines having a piston crown formed with a rotation-symmetrical combustion chamber having a substantially flat bottom wall and a circumferential side wall, the inner diameter of said chamber increasing in a direction toward said bottom wall, in which combustion air is caused to be rotated about a longitudinal axis of the combustion chamber, and wherein a cylinder head is provided with a fuel injection nozzle in the region of a rim of the combustion chamber at an angle relative to said longitudinal axis and substantially in the direction of rotation of the combustion air, comprising the steps of injecting at least one spray of fuel into said chamber in the direction of air rotation and, in such a manner, that the individual droplets of fuel in said spray are finely atomized in all operating ranges of the engine and a substantially fuel-free zone is formed at the center of said combustion chamber, the radius of said zone being approximately one-third the radius of said chamber; and effecting a break-up of said at least one spray in such a manner that the broken-up spray is distributed throughout the zone between said fuel-free zone and said side wall and surrounding said fuel-free zone and generally conforms to the geometry of said side wall of said chamber.
Claim 2
Dependent Claim
229 words
Process for introducing and mixing combustion air and fuel in air compressing, self-igniting, internal combustion engines having a piston crown formed with a rotation-symmetrical combustion chamber having a substantially flat bottom wall and a circumferential side wall, the inner diameter of said chamber increasing in a direction toward said bottom wall, in which combustion air is caused to be rotated about a longitudinal axis of the combustion chamber, and wherein a cylinder head is provided with a fuel injection nozzle in the region of a rim of the combustion chamber at an angle relative to said longitudinal axis and substantially in the direction of rotation of the combustion air, comprising the steps of injecting at least one spray of fuel into said chamber in the direction of air rotation and, in such a manner, that the individual droplets of fuel in said spray are finely atomized in all operating ranges of the engine and a substantially fuel-free zone is formed at the center of said combustion chamber, the radius of said zone being approximately one-third the radius of said chamber; and effecting a break-up of said at least one spray in such a manner that the broken-up spray is distributed throughout the zone between said fuel-free zone and said side wall and surrounding said fuel-free zone and generally conforms to the geometry of said side wall of said chamber.
Claim 3
Dependent Claim
54 words
Injection and mixture formation process as in claim 1, wherein--viewed in a longitudinal section through the combustion chamber--the entire air for combustion is enriched with fuel from said side wall up to approximately one third of the combustion chamber radius (r n ) between the combustion chamber bottom wall and the combustion chamber rim.
Claim 4
Dependent Claim
82 words
Injection and mixture formation process as in claim 1 wherein the fuel is introduced into the combustion chamber in a manner that the centre of the broken-up fuel spray--viewed in plan looking on the combustion chamber--forms a tangent to a circle whose diameter (2×r w ) amounts to 0.6 to 0.7 times the combustion chamber diameter (D B ), and in that, viewed in projection, the fuel spray extends at an angle (δ) of 40° to 50° relative to said longitudinal axis.
Claim 5
Dependent Claim
36 words
Injection and mixture formation process as in claim 3, wherein a free trajectory of said fuel spray entrained by the rotating air is at least equal to 0.8 times the combustion chamber diameter (D B ).
Claim 6
Dependent Claim
25 words
Injection and mixture formation process as in claim 4, wherein the total spray cone angle (α) of the fuel spray is between 35° and 45°.
Claim 7
Dependent Claim
104 words
Injection and mixture formation process as in claim 1 wherein the fuel is introduced into the combustion chamber through a two-hole nozzle producing a main and a secondary fuel spray and in such a manner that the center of the broken-up main fuel spray, viewed in plan looking on the combustion chamber, forms a tangent to a circle whose diameter (2×r w ) amounts to 0.6 to 0.7 times the combustion chamber diameter (D B ), and when viewed in projection, the main fuel spray extends at an angle (δ) of between 40° and 50° relative to the longitudinal axis of the combustion chamber.
Claim 8
Dependent Claim
29 words
Injection and mixture formation process as in claim 1 wherein the rotating frequency of the air for combustion in the cylinder is between 130 and 155 H z .
Claim 9
Dependent Claim
34 words
Injection and mixture formation process as in claim 1 wherein the rotating frequency of the air for combustion in the cylinder of supercharged internal combustion engines is between 140 and 165 H z .
References Cited (Backward Citations)
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1986-08-29 | 1987-02-28 | 1987-08-30 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-08-29 | 1991-02-28 | 1991-08-30 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-08-29 | 1995-02-28 | 1995-08-30 | $7700.00 | Window Closed / Lapsed |