Patent US4526143A successfully refreshed from Google Patents.
US4526143A
Expired / Lapsed
US
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Direct injection internal combustion engine of compression ignition type
Assignee: Toyota Central R&D Labs Inc
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Filing: 1983-08-26
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Granted: 1985-07-02
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Expires: 2003-08-26
Abstract
Abstract A direct injection internal combustion engine of compression ignition type is provided with a piston cavity offset from the piston center and with an injection nozzle which injects a hollow conical fuel spray having a tangential velocity component and relatively weak penetration into a swirl set up in the combustion chamber. The injection geometry and the offset are such that squish and swirl flows interact to form an excellent air-fuel mixture over the whole volume of the cavity without forming local fuel concentrations or wetting the cavity wall.
Inventors
- 👤 Yujiro Oshima
- 👤 Taro Aoyama
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 06:49
CPC Classifications
F; F02; F02B; F02B23/00; F02B23/02; F02B23/06; F02B23/0675; F02B23/0645; F02B23/066; F02B3/00; F02B3/06; F02B1/00; F02B1/02; F02B1/04; F02B75/00; F02B75/12; F02B2075/125; F02B2275/00; F02B2275/14; F02B2275/40; F02B23/0618; F02B23/0621; F02B23/0624; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 15
Claim 1
Independent Claim
149 words
A direct injection internal combustion engine of a compression ignition type, in which a fuel is injected into air supplied into a combustion chamber and compressed by a piston so that the fuel may be ignited and burned, comprising: intake means including means for supplying the swirling intake air into said combustion chamber; said combustion chamber comprising a substantially semi-spherical cavity formed in the top surface of said piston, the center of said cavity being offset with respect to the central axis of said piston top surface by an eccentricity Os as satisfies the following relationship, where D is the diameter of said piston, 0.02<Os/D<0.15; and fuel injection nozzle means for injecting a fuel spray having a large tangential velocity component with respect to the axis of an injection portion and an axial velocity along the forward direction of the swirling flow of intake air formed in said cavity.
Claim 2
Dependent Claim
149 words
A direct injection internal combustion engine of a compression ignition type, in which a fuel is injected into air supplied into a combustion chamber and compressed by a piston so that the fuel may be ignited and burned, comprising: intake means including means for supplying the swirling intake air into said combustion chamber; said combustion chamber comprising a substantially semi-spherical cavity formed in the top surface of said piston, the center of said cavity being offset with respect to the central axis of said piston top surface by an eccentricity Os as satisfies the following relationship, where D is the diameter of said piston, 0.02<Os/D<0.15; and fuel injection nozzle means for injecting a fuel spray having a large tangential velocity component with respect to the axis of an injection portion and an axial velocity along the forward direction of the swirling flow of intake air formed in said cavity.
Claim 3
Dependent Claim
115 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 1, wherein said fuel injection nozzle means comprises a fuel injection nozzle positioned with respect to said cavity to inject said fuel spray within an angular range of 225 degrees with respect to cavity circumference, whose value comprises the addition of a circumferential angle of 45 degrees oriented oppositely of the direction of said swirling flow formed in said cavity, to a semi-circle located on the eccentric side of said cavity and determined by a straight line extending through the cavity center and intersecting at a right angle the straight line joining the piston center and the cavity center.
Claim 4
Dependent Claim
51 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 2, wherein said fuel injection nozzle is positioned with respect to said cavity to inject said fuel spray within a range of 90 to 180 degrees in terms of the circumferential angle of said cavity.
Claim 5
Dependent Claim
67 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 1, wherein said fuel injection nozzle means comprises a fuel injection nozzle positioned with respect to said cavity to inject fuel with a spray diverging angle to cause the most divergent portion of said fuel spray to be confined between the central axis and an inner circumferential wall of said cavity.
Claim 6
Dependent Claim
65 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 1, wherein said fuel injection nozzle means comprises a fuel injection nozzle positioned with respect to said cavity to inject said fuel spray in a hollow conical configuration such that the outer boundaries of said conical configuration fall between said cavity central axis and an inner circumferential wall thereof.
Claim 7
Dependent Claim
63 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 1, said offset being sufficiently large to insure that squish flows whose strengths vary circumferentially of said cavity interact with said swirling flow such that an air-fuel mixture is formed in said cavity such that said fuel is prevented from colliding upon an inner circumferential cavity wall.
Claim 8
Dependent Claim
40 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 1, wherein said fuel injection nozzle means comprises a swirl injection nozzle positioned in the vicinity of a throttled inlet opening of said cavity.
Claim 9
Dependent Claim
83 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 7, wherein said swirl injection nozzle comprises a slit type swirl injection nozzle comprising a swirl injection nozzle of the slit type comprising a nozzle body of a hollow cylindrical body having a injection port at end portion thereof, a needle tip, having a groove-shaped slit extends along an outer circumferential wall thereof and a conical tip portion at end portion thereof, inserted into said nozzle body.
Claim 10
Dependent Claim
31 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 8, wherein the diameter of said injection port is within 0.3 mm and 1.0 mm.
Claim 11
Dependent Claim
36 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 1, wherein said intake means comprises a helical port positioned in the vicinity of a port of said intake means.
Claim 12
Dependent Claim
33 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 1, wherein the ratio eccentricity Os of said cavity and the diameter of said piston is 0.042.
Claim 13
Dependent Claim
66 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 1, wherein the cavity formed in said piston top surface has a throttled inlet opening, the remaining portion of said cavity being allowed to have a larger area, such that the ratio of the inlet opening area A to the piston top surface area Ao satisfies the following relationship: 0.07<A/Ao<0.25.
Claim 14
Dependent Claim
54 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 12, wherein said throttled inlet opening has a notch positioned at said throttled inlet opening of said cavity and in the vicinity of said nozzle, so as to avoid the collision of fuel spray and said nozzle body.
Claim 15
Dependent Claim
37 words
A direct injection internal combustion engine of a compression ignition type as set forth in claim 12, wherein the diameter of said throttled inlet opening is from 0.7 to 0.8 of the maximum diameter of said cavity.
References Cited (Backward Citations)
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US2110365A
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US4207843A
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GB2000222A
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JPS54109507A
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JPS5713215A
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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) | 1988-07-01 | 1988-12-31 | 1989-07-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-07-01 | 1992-12-31 | 1993-07-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-07-01 | 1996-12-31 | 1997-07-02 | $7700.00 | Window Closed / Lapsed |