Invention Grant
US08573929B2 Turbocharger with turbine nozzle vanes and an annular rotary bypass valve
有权
带涡轮喷嘴叶片的涡轮增压器和环形旋转旁通阀
- Patent Title: Turbocharger with turbine nozzle vanes and an annular rotary bypass valve
- Patent Title (中): 带涡轮喷嘴叶片的涡轮增压器和环形旋转旁通阀
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Application No.: US12771434Application Date: 2010-04-30
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Publication No.: US08573929B2Publication Date: 2013-11-05
- Inventor: Alain Lombard , Michel Thirion , Nicolas Serres
- Applicant: Alain Lombard , Michel Thirion , Nicolas Serres
- Applicant Address: US NJ Morristown
- Assignee: Honeywell International Inc.
- Current Assignee: Honeywell International Inc.
- Current Assignee Address: US NJ Morristown
- Agency: Alston & Bird LLP
- Main IPC: F01D17/00
- IPC: F01D17/00

Abstract:
A turbocharger includes an annular bypass passage to allow exhaust gas to bypass the turbine wheel. An annular bypass valve is disposed in the bypass passage. The bypass valve comprises a fixed annular valve seat and a rotary annular valve member arranged coaxially with the valve seat. The valve member is disposed against the valve seat and is rotatable about the axis for selectively varying a degree of alignment between respective orifices in the valve seat and valve member. The turbine includes a nozzle having a vane assembly. In one embodiment the vane assembly has only fixed vanes. In another embodiment the vane assembly includes both fixed vanes and variable vanes, and the variable vanes are part of a rotor that rotates together with the rotary valve member.
Public/Granted literature
- US20110268559A1 Turbocharger With Turbine Nozzle Vanes and an Annular Rotary Bypass Valve Public/Granted day:2011-11-03
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