The thermoaerodynamic design philosophy and features of the centrifugal compressor and the axial turbine of the turbocharger GZ680 are discussed.
本文介绍了GZ680增压器的离心压气机与轴流透平的气动热力学设计思想及特点。
2
The conclusions redound to the developing and extending of axial-flow constant press turbocharger with variable nozzle ring, and lay a foundation for later work.
所获结论有助于带可变喷嘴环的轴流式定压涡轮增压器研制与推广，为以后的研究工作奠定基础。
3
This paper presents a method for thermodynamic calculation of the axial flow turbocharger turbine with variable geometry nozzle.