Power turbine bypass for improved compression braking

Claim 2

A turbocompound engine having a power turbine bypass control comprising: an internal combustion engine having a crankshaft, an intake manifold and an exhaust manifold; turbocharger means connected with said intake and exhaust manifolds for converting exhaust gas energy into mechanical energy for boosting intake air pressure, said turbocharger means including a first turbine connected to said exhaust manifold; power turbine means for producing mechanical energy from energy remaining in the exhaust gases exiting said first turbine, said power turbine means being coupled to the crankshaft of said engine for providing power to said crankshaft; exhaust passage means for allowing exhaust gas to bypass said power turbine, said exhaust passage means including a bypass passage and a bypass valve wherein exhaust gas from said engine passes through said power turbine means when said bypass is in a closed position and at least some of the engine exhaust gas passes through said passage to bypass said power turbine means when said bypass valve is in an open position; compression braking means for operating said engine in a compression braking mode; and bypass control means for detecting actuation of said compression braking mode and for opening said bypass valve in response to detection of compression braking actuation.

Claim 3

The turbocompound engine of claim 1, wherein said bypass valve is a variable opening valve for varying the amount of exhaust gas passing through said passage.

Claim 4

The turbocompound engine of claim 1, wherein said bypass valve includes first and second valve passages, the first valve passage directing exhaust gas toward said power turbine and the second valve passage directing gas toward said bypass passage, said bypass valve further including a diffuser connected to said second valve passage.

Claim 5

The turbocompound engine of claim 1, wherein said bypass valve includes a flapper valve.

Claim 6

The turbocompound engine of claim 1, wherein said bypass valve includes poppet valve.

Claim 7

The turbocompound engine of claim 1, wherein said bypass valve includes a butterfly valve.

Claim 8

The turbocompound engine of claim 1, wherein said bypass valve includes first and second valve passages, the first valve passage directing exhaust gas to said power turbine and the second valve passage directing exhaust gas to said bypass passage, said bypass valve further including diverter means located in said second valve passage for preventing flow of exhaust gas to said bypass passage when the diverter in a first position and for allowing exhaust gas to flow to said bypass passage when the diverter is in a second position.

Claim 9

The turbocompound engine of claim 7, further including a diffuser located at an outlet of said second valve passage.

Claim 10

The turbocompound engine of claim 8, wherein the power turbine is an axial power turbine, and wherein said bypass valve includes a translating shroud movable between a first position in which flow to the bypass passage is allowed and a second position in which flow to the bypass passage is prevented.

Claim 11

The turbocompound engine of claim 1, wherein said compression braking means includes an operator controlled switch of the engine in a compression braking mode; and said bypass control means includes means for receiving a signal indicative of said switch operation and for opening said bypass valve in response to said signal.

Claim 12

The turbocompound engine of claim 1, wherein said compression braking means includes first operator controlled switch means for producing a signal for actuating operation of compression braking, or second switch means for allowing said signal to actuate compression braking only when a fuel pump of said engine is off, and third switch means for allowing said signal to actuate compression braking only when a clutch of said engine is engaged; said bypass control means including means for determining that said first switch means has been actuated, and said second and third switch means have allowed said signal to actuate operation of compression braking means for opening the bypass in response.

Claim 13

A turbocompound engine having a power turbine bypass control comprising: an internal combustion engine having a crankshaft and an exhaust manifold; turbocharger means connected with said intake and exhaust manifolds for converting exhaust gas energy into mechanical energy for boosting intake air pressure, said turbocharger means including a first turbine connected to said exhaust manifold; power turbine means for producing mechanical from energy remaining in the exhaust gases exiting said first turbine, said power turbine means coupled to the crankshaft for providing power to the crankshaft; compression braking means for operating the engine in a compression braking mode; and exhaust pressure relief means for relieving exit pressure of exhaust gas exiting from said first turbine in response to operation of said engine in a compression braking mode.

Claim 14

A turbocompound engine having a power turbine bypass control comprising: an internal combustion engine having a crankshaft and an exhaust manifold; turbocharger means connected with said intake and exhaust manifolds for converting exhaust gas energy into mechanical energy for boosting intake air pressure, said turbocharger means including a first turbine connected to said exhaust manifold; power turbine means for producing mechanical from energy remaining in the exhaust gases exiting said first turbine, said power turbine means coupled to the crankshaft for providing power to the crankshaft; compression braking means for operating the engine in a compression braking mode; and exhaust pressure relief means for relieving exit pressure of exhaust gas exiting from said first turbine in response to operation of said engine in a compression braking mode.

Claim 15

The turbocompound engine of claim 12, wherein said exhaust pressure relief means includes bypass means for allowing of exhaust gas exiting the first turbine to bypass said power turbine.

Claim 16

A turbocompound engine having a power turbine bypass control comprising: an internal combustion engine having a crankshaft, an intake manifold and an exhaust manifold; turbocharger means connected with said intake manifold and said exhaust manifold for converting exhaust gas energy into mechanical energy for boosting intake air pressure, said turbocharger means including a first turbine having an inlet and an outlet; a first passage connecting said exhaust manifold to said first turbine inlet; a second turbine having an inlet and outlet and an output shaft for supplying mechanical power to said engine crankshaft; a second passage connected to said first turbine outlet; a third passage connected to said second turbine outlet; compression brake means for converting said internal combustion engine into an air compressor in response to a control signal; braking control means for producing said braking control signal; a fourth passage connecting said second and said third passage; a bypass valve for moving between an open position in which exhaust gas is allowed to pass through said fourth passage and a closed position in which exhaust gas is prevented from flowing through said fourth passage; bypass control means connected with said braking control means for moving said bypass valve to its open position upon receipt of said braking control signal.

Claim 17

A turbocompound engine having a power turbine bypass control comprising: an internal combustion engine having a crankshaft, an intake manifold and an exhaust manifold; turbocharger means connected with said intake manifold and said exhaust manifold for converting exhaust gas energy into mechanical energy for boosting intake air pressure, said turbocharger means including a first turbine having an inlet and an outlet; a first passage connecting said exhaust manifold to said first turbine inlet; a second turbine having an inlet and outlet and an output shaft for supplying mechanical power to said engine crankshaft; a second passage connected to said first turbine outlet; a third passage connected to said second turbine outlet; compression brake means for converting said internal combustion engine into an air compressor in response to a control signal; braking control means for producing said braking control signal; a fourth passage connecting said second and said third passage; a bypass valve for moving between an open position in which exhaust gas is allowed to pass through said fourth passage and a closed position in which exhaust gas is prevented from flowing through said fourth passage; bypass control means connected with said braking control means for moving said bypass valve to its open position upon receipt of said braking control signal.