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US5178109A Expired / Lapsed US ⏱️ 0.0 years remaining

Heat-insulating engine with swirl chambers

Assignee: Isuzu Motors Ltd
•
Filing: 1992-03-13
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Granted: 1993-01-12
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Expires: 2012-03-13
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Abstract

Abstract This invention relates to a heat-insulating engine with swirl chambers which reduces a throttle loss due to the communication ports and increases the speed of a vortex flow within swirl chambers. The heat-insulating engine with swirl chambers comprises small communication ports each with a small passage area and large communication ports each with a large passage area formed at the lower portions of the swirl chamber blocks constituting heat-insulating swirl chambers, and control valves provided to large communication ports. During the compression stroke, the control valves close the large communication ports, and open the same ports during the expansion stroke after fuel injection and on rise in pressure in the swirl chambers. Accordingly, during the compression stroke, air is sent into the swirl chambers at high speed via small communication ports to increase a vortex flow speed within the swirl chambers. During the expansion stroke, the large communication ports being open, combustion gas and flame are forced into the main combustion chambers from the swirl chambers to reduce a throttle loss.

Inventors

  • 👤 Hideo Kawamura

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 18:54
CPC Classifications
F; F02; F02B; F02B19/00; F02B19/02; F02B19/16; F02B19/165; F02B77/00; F02B77/11; F02F; F02F7/00; F02F7/0085; F02F7/0087; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12

Claims Analysis

Total Claims: 15
Claim 1
Independent Claim 201 words
In a heat-insulating engine with swirl chambers, comprising a cylinder block constituting cylinders, a cylinder head fixed to said cylinder block, swirl chamber blocks disposed inside hole portions formed in said cylinder head and constituting swirl chambers having a heat-insulating structure, pistons reciprocating inside said cylinders, main chambers formed at said piston heads of said pistons, communication ports for communicating said main chambers with said swirl chambers, formed in said swirl chamber blocks, and fuel injection nozzles having injection ports thereof opening to said swirl chambers, and sequentially operated in a cycle of an intake stroke, a compression stroke, an expansion stroke and an exhaust stroke; the improvement characterized in that the heat-insulating engine with swirl chambers futher comprises: said communication ports including small communication ports having a small passage area and large communication ports having a large passage area, formed in said swirl chamber blocks; and control valves for opening and closing said large communication ports, said control valves closing said large communication ports during said compression stroke and opening said large communication ports at the time of the pressure rise of said swirl chambers during said expansion stroke after the injection of the fuel from said fuel injection nozzles.
Claim 2
Dependent Claim 201 words
In a heat-insulating engine with swirl chambers, comprising a cylinder block constituting cylinders, a cylinder head fixed to said cylinder block, swirl chamber blocks disposed inside hole portions formed in said cylinder head and constituting swirl chambers having a heat-insulating structure, pistons reciprocating inside said cylinders, main chambers formed at said piston heads of said pistons, communication ports for communicating said main chambers with said swirl chambers, formed in said swirl chamber blocks, and fuel injection nozzles having injection ports thereof opening to said swirl chambers, and sequentially operated in a cycle of an intake stroke, a compression stroke, an expansion stroke and an exhaust stroke; the improvement characterized in that the heat-insulating engine with swirl chambers futher comprises: said communication ports including small communication ports having a small passage area and large communication ports having a large passage area, formed in said swirl chamber blocks; and control valves for opening and closing said large communication ports, said control valves closing said large communication ports during said compression stroke and opening said large communication ports at the time of the pressure rise of said swirl chambers during said expansion stroke after the injection of the fuel from said fuel injection nozzles.
Claim 3
Dependent Claim 31 words
A heat-insulating engine with swirl chambers according to claim 1, wherein the passage area of said small communication ports is not greater than 0.9% of the sectional area of said cylinder.
Claim 4
Dependent Claim 31 words
A heat-insulating engine with swirl chambers according to claim 1, wherein said passage area of said large communication ports is not greater than 3% of the sectional area of said cylinder.
Claim 5
Dependent Claim 45 words
A heat-insulating engine with swirl chambers according to claim 1, wherein the air introduced from said main chambers into said swirl chambers through said small communication ports having a small passage area during said compression stroke forms a strong vortex flow inside said swirl chambers.
Claim 6
Dependent Claim 64 words
A heat-insulating engine with swirl chambers according to claim 4, wherein the fuel is injected from said fuel injection nozzle into said vortex flow formed inside said swirl chambers, said fuel and the air mix to form a fuel-air mixture, said fuel-air mixture is ignited, said ignited fuel-air mixture burns rapidly and forms a combustion flame, and the pressure inside said swirl chambers rises.
Claim 7
Dependent Claim 62 words
A heat-insulating engine with swirl chambers according to claim 5, wherein said control valves are opened during said expansion stroke, so that said combustion flame inside said swirl chambers flows out at a stretch from said swirl chambers to said main chambers during said expansion stroke, mixes with the air existing inside said main chambers, shortens the combustion time and burns satisfactorily.
Claim 8
Dependent Claim 30 words
A heat-insulating engine with swirl chambers according to claim 1, wherein said control valves open said large communication ports at a pressure above a predetermined pressure inside said swirl chambers.
Claim 9
Dependent Claim 39 words
A heat-insulating engine with swirl chambers according to claim 1, wherein said control valves are actuated by electromagnetic force, and the opening time and valve lift quantity thereof are controlled in response to the operating state of said engine.
Claim 10
Dependent Claim 32 words
A heat-insulating engine with swirl chambers according to claim 1, wherein said control valves open said large communication ports in response to a pressure inside said swirl chambers above a predetermined pressure.
Claim 11
Dependent Claim 27 words
A heat-insulating engine with swirl chambers according to claim 1, wherein said swirl chamber blocks are constituted in a heat-insulating structure by a highly heat-resistant ceramic material.
Claim 12
Dependent Claim 22 words
A heat-insulating engine with swirl chambers according to claim 1, wherein said control valves are made of a highly heat-resisting ceramic material.
Claim 13
Dependent Claim 38 words
A heat-insulating engine with swirl chambers according to claim 1, wherein said large communication ports are formed on the center side of said cylinders and said small communication ports are formed on the peripheral side of said cylinders.
Claim 14
Dependent Claim 62 words
A heat-insulating engine with swirl chambers according to claim 1, wherein said swirl chambers formed in said swirl chamber blocks are formed so that the section thereof in the axial direction of said cylinders are square wall surfaces and are formed in the square form with respect to the flowing direction of the air vortex flow introduced from said small communication ports.
Claim 15
Dependent Claim 35 words
A heat-insulating engine with swirl chambers according to claim 13, wherein the fuel injected from said injection ports of said fuel injection nozzles is directed so as to impinge obliquely against said square wall surfaces.

References Cited (Backward Citations)

US2552657A Cited
US3168083A Cited
US4424780A Cited
US4300497A Cited
JPS5921024A Cited
US4854281A Cited
JPS6419616A Cited
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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) 1996-01-12 1996-07-13 1997-01-12 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2000-01-12 2000-07-13 2001-01-12 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2004-01-12 2004-07-13 2005-01-12 $7700.00 Window Closed / Lapsed

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