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US4709552A Expired / Lapsed US ⏱️ 0.0 years remaining

Multiple cylinder internal combustion engine with exhaust turbochargers

Assignee: Dr Ing HCF Porsche AG
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Filing: 1987-01-30
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Granted: 1987-12-01
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Expires: 2007-01-30
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Abstract

Abstract A turbosupercharging system is provided having two turbosuperchargers of the same type and dimensions, connected in parallel. A cut-in valve is installed in an exhaust manifold in which the second turbine is installed. When the valve is closed, the entire exhaust blast coming from the engine is directed to the first turbine. In this manner, even at low engine speeds, the first turbine can deliver an effective amount of power to its compressor, thereby introducing a detectable supercharge into the cylinders of the internal combustion engine. This supercharge also holds a biased nonreturn valve which is built into the manifold pressure line of the second tubosupercharger is a closed position. When the cut-in valve is completely open the exhaust blast is divided between both turbines, thereby allowing a pressure build up in the manifold pressure line of the second turbosupercharger. This pressure builds up until the biased nonreturn valve is suddenly opened and compressed air from both compressors is delivered to the cylinders. A specially adapted control system is provided for the nonreturn valve in order to prevent power loss or pulsations due to the cutting in of the second turbosupercharger.

Inventors

  • 👤 Erwin Rutschmann
  • 👤 Khanh Tran-Van
  • 👤 Joachim Wagner

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 08:02
CPC Classifications
F; F02; F02B; F02B37/00; F02B37/007; F16; F16K; F16K15/00; F16K15/02; F16K15/06; F16K15/063; F01; F01N; F01N13/00; F01N13/08; F01N13/10; F01N13/107; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 236 words
An internal combustion engine having cylinder means in fluid communication with common manifold exhaust means, comprising: first and second turbusupercharging means in fluid communication with said common manifold exhaust means, common manifold suction means for receiving compressed air from said first and second turbosupercharging means and supplying said compressed air to said cylinder means, cut-in valve means interposed between said common manifold exhaust means and said second turbosupercharging means for controlling a flow of exhaust to said second turbosupercharging means, said cut-in valve means being responsive to an operating paramater of said engine, non-return valve means interposed between said second turbosupercharging means and said common manifold suction means for controlling a flow of compressed air from said second turbosupercharging means to said common manifold suction means, said non-return valve means being operably responsive to a pressure build-up upstream of said non-return valve means, ventilation valve means upstream of said non-return valve means for venting at least a portion of said compressed air, pressure sensor means upstream and downstream of said non-return valve means for measuring a pressure differential across said non-return valve means, and control device means connected to said pressure sensors and said ventilation valve means for closing said ventilation valve means when said pressure differential decreases below a preselected pressure valve, thereby permitting said compressed air to open said non-return valve means and pass through said common manifold suction means to said cylinder means.
Claim 2
Dependent Claim 236 words
An internal combustion engine having cylinder means in fluid communication with common manifold exhaust means, comprising: first and second turbusupercharging means in fluid communication with said common manifold exhaust means, common manifold suction means for receiving compressed air from said first and second turbosupercharging means and supplying said compressed air to said cylinder means, cut-in valve means interposed between said common manifold exhaust means and said second turbosupercharging means for controlling a flow of exhaust to said second turbosupercharging means, said cut-in valve means being responsive to an operating paramater of said engine, non-return valve means interposed between said second turbosupercharging means and said common manifold suction means for controlling a flow of compressed air from said second turbosupercharging means to said common manifold suction means, said non-return valve means being operably responsive to a pressure build-up upstream of said non-return valve means, ventilation valve means upstream of said non-return valve means for venting at least a portion of said compressed air, pressure sensor means upstream and downstream of said non-return valve means for measuring a pressure differential across said non-return valve means, and control device means connected to said pressure sensors and said ventilation valve means for closing said ventilation valve means when said pressure differential decreases below a preselected pressure valve, thereby permitting said compressed air to open said non-return valve means and pass through said common manifold suction means to said cylinder means.
Claim 3
Dependent Claim 30 words
An internal combustion engine according to claim 1, wherein said ventilation valve means vents at least a portion of said compressed air to an air filter means of said engine.
Claim 4
Dependent Claim 17 words
An internal combustion engine according to claim 1, wherein said preselected pressure differential is about 40 mbar.
Claim 5
Dependent Claim 41 words
An internal combustion engine according to claim 1, wherein said turbosupercharging means comprise turbine means receiving exhaust from said common manifold exhaust means, and commpressor means drivable by said turbine means transmitting said compressed air to said common manifold suction means.
Claim 6
Dependent Claim 25 words
An internal combustion engine according to claim 1, wherein said cut-in valve means includes electronic control means responsive to an operating parameter of said engine.

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) 1990-11-30 1991-06-01 1991-12-01 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1994-11-30 1995-06-01 1995-12-01 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1998-11-30 1999-06-01 1999-12-01 $7700.00 Window Closed / Lapsed

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