Exhaust gas turbine of a turbocharger for an internal combustion engine

Claim 2

In an turbocharger for an internal combustion engine having a housing defining an exhaust gas turbine portion including a rotor and defining a surrounding exhaust flow inlet duct with an annular nozzle opening therefrom to the rotor for directing exhaust gas flow to the rotor and having a guide-blade cascade of guide blades with their angular orientation relative to the flow direction through the nozzle opening being selectively settable by means of a guide-blade adjusting device for varying the effective flow cross-section of the nozzle opening, characterized by a gap setting device ( 14 , 15 , 16 , 17 ) for selectively changing dimension of the gap at the ends of the guide-blade cascade ( 11 ) and the casing ( 10 ) between a substantially zero gap dimension and a maximum gap dimension.

Claim 3

The exhaust gas turbine portion as set forth in claim 1 in which an annular piston ( 14 ) is reciprocally supported by the casing wall adjacent the end portion of the guide-blade cascade ( 11 ), the casing ( 10 ) and the annular piston ( 14 ) defining a pressure space ( 15 ) to which fluid pressure can be selectively directed for controlling movement of the annular piston ( 14 ) relative to the end portions of the guide blades ( 12 ) of the guide-blade cascade ( 11 ).

Claim 4

The exhaust gas turbine portion as set forth in claim 2 and with a spring ( 25 ) urging the annular piston ( 14 ) toward the end portion of the guide-blade cascade ( 11 ).

Claim 5

The exhaust gas turbine portion as set forth in claim 2 including pins ( 26 ) provided to guide and center the annular piston ( 14 ).

Claim 6

The exhaust gas turbine portion as set forth in claim 2 and the annular piston ( 14 ) having an elastic coated end ( 27 ) facing the end portions of the guide-blades cascade ( 11 ).

Claim 7

The exhaust gas turbine potion as set forth in claim 2 in which the pressure space ( 15 ) partially defined by the annular piston ( 14 ) is selectively connected to a pressure-regulating device ( 19 ).

Claim 8

The exhaust gas turbine portion as set forth in claim 6 in which the pressure-regulating device ( 19 ) is connected to an engine control device ( 21 ) by a control line ( 20 ) for modulation of pressure in the pressure space in accord with engine operation.

Claim 9

The exhaust gas turbine portion as set forth in one of claims 2 , 6 , and 7 including a three-way valve ( 19 ) for alternately controlling pressurization of the pressure space ( 15 ) and having two pressure activation lines ( 17 , 22 ) provided for the pressure space ( 15 ) and a stop position.

Claim 10

The exhaust gas turbine portion as set forth in claim 8 in which one of the two pressure activation lines is connected to a source of fluid pressure ( 18 ) which generates a substantial pressure, and the other of the two pressure activation lines is connected to the flow duct ( 7 ) wherein the pressure of the source of fluid pressure ( 18 ) is higher than the pressure from the flow duct ( 7 ).

Claim 11

In an turbocharger for an internal combustion engine having a housing defining an exhaust gas turbine portion including a rotor and defining a surrounding exhaust flow inlet duct with an annular nozzle opening therefrom to the rotor for directing exhaust gas flow to the rotor and having a guide-blade cascade of guide blades with their angular orientation relative to the flow direction through the nozzle opening being selectively settable by means of a guide-blade adjusting device for varying the effective flow cross-section of the nozzle opening, characterized by a gap setting device ( 14 , 15 , 16 , 17 ) for selectively changing dimension of the gap at the ends of the guide-blade cascade ( 11 ) and the casing ( 10 ) between a substantially zero gap dimension and a maximum gap dimension.

Claim 12

In an turbocharger for an internal combustion engine having a housing defining an exhaust gas turbine portion including a rotor and defining a surrounding exhaust flow inlet duct with an annular nozzle opening therefrom to the rotor for directing exhaust gas flow to the rotor and having a guide-blade cascade of guide blades with their angular orientation relative to the flow direction through the nozzle opening being selectively settable by means of a guide-blade adjusting device for varying the effective flow cross-section of the nozzle opening, characterized by a gap setting device ( 14 , 15 , 16 , 17 ) for selectively changing dimension of the gap at the ends of the guide-blade cascade ( 11 ) and the casing ( 10 ) between a substantially zero gap dimension and a maximum gap dimension.

Claim 13

The exhaust gas turbine portion as set forth in claim 10 in which an annular piston ( 14 ) is reciprocally supported by the casing wall adjacent the end portion of the guide-blade cascade ( 11 ), the casing ( 10 ) and the annular piston ( 14 ) defining a pressure space ( 15 ) to which fluid pressure can be selectively directed for controlling movement of the annular piston ( 14 ) relative to the end portions of the guide blades ( 12 ) of the guide-blade cascade ( 11 ).

Claim 14

The exhaust gas turbine portion as set forth in claim 11 in which the annular piston ( 14 ) has a central thin-walled configuration.

Claim 15

The exhaust gas turbine portion as set forth in claim 11 and including at least one pin bearing ( 29 ) mounted in a bore ( 30 ) formed in the annular piston ( 14 ) and engaging the end of the guide blades ( 12 ) away from the guide-blade cascade adjusting device ( 13 ).

Claim 16

The exhaust gas turbine portion as set forth in claim 12 and including at least one pin bearings ( 29 ) extending through bores ( 38 ) in an extension ring portion ( 37 ) of the annular piston ( 14 ) and inserted in bearing bores ( 39 ) in the casing ( 10 ) away from the guide-blade cascade adjusting device ( 13 ).

Claim 17

The exhaust gas turbine portion as set forth in claim 11 in which a damping ring ( 33 ) is supported within the annular piston ( 14 ) between it and the casing ( 10 ) and a spring ( 34 ) urges the annular piston ( 14 ) and damping ring ( 33 ) apart from one another, an interspace ( 35 ) is defined between the annular piston ( 14 )and the damping ring ( 33 ) with at least one throttle bore ( 36 )connecting the piston space ( 15 ) and the interspace ( 35 ).

Claim 18

A regulatory system for an exhaust gas turbine portion of an exhaust gas turbocharger for an internal combustion engine including a rotor and having a casing defining a surrounding exhaust flow inlet duct with an annular nozzle opening therefrom to the rotor for directing exhaust gas flow to the rotor and having a guide-blade cascade of guide blades with their angular orientation relative to the flow direction through the nozzle opening being selectively settable by means of a guide-blade cascade adjusting device for varying the effective flow cross-section of the nozzle opening, characterized in that a gap setting device ( 14 , 15 ) is controlled by a pressure regulating device ( 19 ) for selectively providing a gap dimension between the gap setting device ( 14 ) and the ends of the guide-blade cascade ( 11 ) between a substantially zero dimension gap and a maximum dimension gap.

Claim 19

A regulatory system for an exhaust gas turbine portion of an exhaust gas turbocharger for an internal combustion engine including a rotor and having a casing defining a surrounding exhaust flow inlet duct with an annular nozzle opening therefrom to the rotor for directing exhaust gas flow to the rotor and having a guide-blade cascade of guide blades with their angular orientation relative to the flow direction through the nozzle opening being selectively settable by means of a guide-blade cascade adjusting device for varying the effective flow cross-section of the nozzle opening, characterized in that a gap setting device ( 14 , 15 ) is controlled by a pressure regulating device ( 19 ) for selectively providing a gap dimension between the gap setting device ( 14 ) and the ends of the guide-blade cascade ( 11 ) between a substantially zero dimension gap and a maximum dimension gap.

Claim 20

A turbocharger for an internal combustion engine having a housing defining an exhaust gas turbine portion including a rotor and defining a surrounding exhaust flow inlet duct with an annular nozzle opening leading from said inlet duct to the rotor for directing exhaust gas flow to the rotor, and a guide-blade structure disposed in said nozzle opening and having guide blades whose angular orientation relative to the flow direction through the nozzle opening is selectively settable by means of a guide-blade adjusting device connected to one axial end of said guide blade structure for varying the effective flow cross-section of the nozzle opening, a gap setting device disposed adjacent the other axial end of said guide blade structure for selectively changing the dimension of the axial gap between the other axial end of the guide-blade structure and the housing between a substantially zero gap dimension and a maximum gap dimension, said gap setting device including an annular piston reciprocally supported in the wall of said housing adjacent the other axial end of the guide-blade structure, said annular piston defining at its end opposite said guide blades a pressure space to which fluid under pressure can be selectively directed for controlling axial movement of the annular piston relative to the axial end of the guide blades of the guide-blade structure for adjusting any gap between the annular piston and the guide-blade structure.

Claim 21

A turbocharger for an internal combustion engine having a housing defining an exhaust gas turbine portion including a rotor and defining a surrounding exhaust flow inlet duct with an annular nozzle opening leading from said inlet duct to the rotor for directing exhaust gas flow to the rotor, and a guide-blade structure disposed in said nozzle opening and having guide blades whose angular orientation relative to the flow direction through the nozzle opening is selectively settable by means of a guide-blade adjusting device connected to one axial end of said guide blade structure for varying the effective flow cross-section of the nozzle opening, a gap setting device disposed adjacent the other axial end of said guide blade structure for selectively changing the dimension of the axial gap between the other axial end of the guide-blade structure and the housing between a substantially zero gap dimension and a maximum gap dimension, said gap setting device including an annular piston reciprocally supported in the wall of said housing adjacent the other axial end of the guide-blade structure, said annular piston defining at its end opposite said guide blades a pressure space to which fluid under pressure can be selectively directed for controlling axial movement of the annular piston relative to the axial end of the guide blades of the guide-blade structure for adjusting any gap between the annular piston and the guide-blade structure.

Claim 22

A turbocharger according to claim 17 , further comprising a spring urging said annular piston toward said guide blade structure.

Claim 23

A turbocharger according to claim 17 , wherein pins are provided between said housing and said annular piston for guiding and centering said annular piston.

Claim 24

A turbocharger according to claim 17 , wherein said annular piston has an elastic coated end facing said guide blade structure.

Claim 25

A turbocharger according to claim 17 , wherein said pressure space, which is partially defined by said annular piston, is connected to a pressure supply line which includes a pressure-regulating device.

Claim 26

A turbocharger according to claim 17 , wherein said pressure-regulating device is connected to an engine control device by a control line for controlling the pressure in the pressure space in accordance with engine operating conditions.

Claim 27

A turbocharger according to claim 17 , wherein a three-way valve is provided for alternatively controlling pressurization of said pressure space by way of a first and a second pressurization line for the pressure space.

Claim 28

A turbocharger according to claim 23 , wherein said first pressurization line is connected to a source of fluid pressure and said second pressurization line is connected to a flow duct, wherein the pressure of the source of fluid pressure is higher than the pressure in the flow duct.