|
CN111396189A
|
|
Sequential two-stage supercharging system for constant-pressure exhaust pipe
|
|
CN111350550A
|
|
Sealing structure of bypass assembly of turbocharger
|
|
CN111365118A
|
|
Compact sequential two-stage supercharging system
|
|
CN111022344A
|
|
Air compressor with supercharging and inter-cooling functions for fuel cell
|
|
CN110617145A
|
|
Prevent turbo charger bypass valve structure of leakage
|
|
CN110454441A
|
|
A kind of inlet distortion restraint device and the centrifugal compressor with the device
|
|
CN110469546A
|
|
A kind of structure to reduce compressor efficiency decaying
|
|
CN110005477A
|
|
A kind of two-stage turbocharger hydrnstaticiaxis seal structure
|
|
CN110056424A
|
|
A kind of split type power turbine structure containing hydrostatic seal
|
|
CN110005518A
|
|
A kind of split type power turbine structure with pressure autocompensation
|
|
CN110043492A
|
|
A kind of fuel cell compressor oil gas sealing mechanism
|
|
CN110005630A
|
|
A kind of fuel cell air compressor machine bearing group mechanism
|
|
CN108952950A
|
|
A kind of efficient turbocharger of highly integrated shafting
|
|
CN108757049A
|
|
Exhaust gas bypass turbine of the whirlpool end with air inlet mixing device
|
|
CN108561189A
|
|
A kind of exhaust gas bypass turbine of the asymmetric with fixed guide vane
|
|
CN108561188A
|
|
Integrated high efficiency turbine with outlet restraining structure
|
|
CN108487985A
|
|
Integrated form exhaust gas bypass turbine of the whirlpool end with airflow management device
|
|
US2017009645A1
|
|
Balanced vanes and integrated actuation system for a variable geometry turbocharger
|
|
US2016003196A1
|
|
Quad layer passage variable geometry turbine for turbochargers in exhaust gas recirculation engines
|
