Compressor in an exhaust gas turbocharger of an internal combustion engine and method for operating the compressor
View Patent ↗In a compressor of an exhaust gas turbocharger for an internal combustion engine including a compressor wheel which is rotatably mounted in a compressor inlet duct and an auxiliary rotor wheel arranged so as to be movable axially between a coupled position in engagement with the compressor wheel and a decoupled position, disengaged from the compressor wheel, an adjustable guide vane structure is provided which is movable by an adjusting element together with the auxiliary rotor wheel and a contoured flow control ring for controlling the combustion air flow to the compressor wheel and to the auxiliary rotor wheel.
1. A method for operating a compressor for an internal combustion engine, the compressor comprising a compressor wheel ( 8 ) rotatably supported in an inlet duct ( 19 ) of the compressor ( 5 ), a coaxial auxiliary rotor wheel ( 10 ) arranged in the inlet housing ( 19 ) so as to be axially movable between a coupled position with the compressor wheel ( 8 ) and a decoupled position, wherein, in the coupled position, the compressor wheel ( 8 ) and the auxiliary rotor wheel ( 10 ) are rotationally fixedly connected, and, in the decoupled position, the auxiliary rotor wheel ( 10 ) is decoupled from the compressor wheel ( 8 ), and an adjustable guide vane structure ( 21 ) for variably adjusting the effective inlet flow cross section to the auxiliary rotor wheel ( 10 ) arranged in the compressor inlet duct ( 19 ) upstream of the auxiliary rotor wheel ( 10 ), said method comprising the steps of:
at low engine loads and low engine speeds, moving the auxiliary rotor wheel ( 10 ) into the coupled position with the compressor wheel ( 8 ) and moving the guide vane structure ( 21 ) into the blocking position,
at low engine loads and mid-range engine speeds, moving the auxiliary rotor wheel ( 10 ) into the coupled position with the compressor wheel ( 8 ) and moving the guide vane structure ( 21 ) into an opening position, and
at high engine loads, decoupling the auxiliary rotor wheel ( 10 ) from the compressor wheel ( 8 ).
2. A compressor in an exhaust gas turbocharger for an internal combustion engine, including a compressor housing with an inlet duct ( 19 ), a compressor wheel ( 8 ) rotatably supported in the compressor inlet duct ( 19 ), an auxiliary rotor wheel ( 10 ) disposed in the inlet duct ( 19 ) upstream of the compressor wheel ( 8 ) and coaxially with the compressor wheel ( 8 ), the auxiliary rotor wheel ( 10 ) being axially movable between a coupled position with the compressor wheel ( 8 ) and a decoupled position, wherein, in the coupled position, the compressor wheel ( 8 ) and the auxiliary rotor wheel ( 10 ) are rotationally engaged and, in the decoupled position, the auxiliary compressor wheel ( 10 ) is decoupled from the compressor wheel ( 8 ), an adjustable guide vane structure ( 21 ) for variably adjusting the effective inlet flow cross-section to the auxiliary rotor wheel ( 10 ) arranged in the compressor inlet duct ( 19 ), and a common adjusting element ( 11 ) for adjusting the axial position of the auxiliary rotor wheel ( 10 ) and the position of the guide vane structure ( 21 ).
3. The compressor as claimed in claim 2 , wherein the adjusting element ( 11 ) is arranged axially displaceably in the compressor inlet duct ( 19 ) in axial alignment with the auxiliary rotor wheel ( 10 ).
4. The compressor as claimed in claim 3 , wherein the auxiliary rotor wheel ( 10 ) includes an engagement element ( 26 ) which, upon movement of the auxiliary rotor wheel ( 10 ) toward the compressor wheel ( 8 ) by the adjusting element ( 11 ), initially moves the auxiliary rotor wheel ( 10 ) from the decoupled position into the coupled position, and subsequently, upon further movement of the auxiliary rotor wheel ( 10 ), the vane structure ( 21 ) is moved from a maximum opening position to a blocking position.
5. The compressor as claimed in claim 2 , wherein the guide vane structure ( 21 ) is supported by a contoured ring ( 22 ) which is movable into contact with a housing wall section ( 30 ) of the compressor inlet duct ( 19 ).
6. The compressor as claimed in claim 4 , wherein, in the blocking position, the vane structure grating ( 21 ) is received in a die plate ( 23 ), and a spring element ( 25 ) is disposed between the die plate ( 23 ) and the guide vane structure ( 21 ) for biasing the guide vane structure ( 21 ) into the opening position out of the die plate ( 23 ).
7. The compressor as claimed in claim 2 , wherein a second guide vane structure ( 34 ) is provided in the compressor inlet duct ( 19 ), the second guide vane structure ( 34 ) being arranged between the auxiliary rotor wheel ( 10 ) and the compressor wheel ( 8 ).
8. The compressor as claimed in claim 5 , wherein the second guide vane structure ( 34 ) is supported on the contoured ring ( 22 ).
9. The compressor as claimed in claim 2 , wherein the auxiliary rotor wheel ( 10 ) is a turbine wheel with a radial flow inlet.
10. The compressor as claimed in claim 2 , wherein the auxiliary rotor wheel ( 10 ) includes the coupling element ( 26 ) which, in the coupled position, is rotationally fixedly coupled to the compressor wheel ( 8 ).
11. The compressor as claimed in claim 10 , wherein the coupling element ( 26 ) is axially movably supported by the auxiliary rotor wheel ( 10 ), and a spring element ( 27 ) is arranged between the coupling element ( 26 ) and the auxiliary rotor wheel ( 10 ) biasing the coupling element ( 26 ) toward the compressor wheel ( 8 ).
12. The compressor as claimed in claim 11 , wherein the coupling element ( 26 ) is a friction cone which, in the coupled position, is in frictional contact with the compressor wheel ( 8 ).