Invention Grant
US08166755B2 Turbocharger system with turbine bypass valve actuated by multiple-rate fluid pressure actuator
有权
涡轮增压器系统具有由多速率流体压力致动器驱动的涡轮旁通阀
- Patent Title: Turbocharger system with turbine bypass valve actuated by multiple-rate fluid pressure actuator
- Patent Title (中): 涡轮增压器系统具有由多速率流体压力致动器驱动的涡轮旁通阀
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Application No.: US12352752Application Date: 2009-01-13
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Publication No.: US08166755B2Publication Date: 2012-05-01
- Inventor: Arthur Jeanson , Jean-Luc Perrin , Jean-Yves Bodin
- Applicant: Arthur Jeanson , Jean-Luc Perrin , Jean-Yves Bodin
- 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: F02D23/00
- IPC: F02D23/00 ; F02D23/02

Abstract:
A fluid pressure actuator for a turbocharger system's turbine bypass valve comprises a piston slidable in a cylinder so as to define a chamber containing a compression spring assembly operable to exert a spring force on the piston. The cylinder can be selectively subjected to a vacuum or pressure for exerting a fluid pressure force on the piston in a direction opposite from the spring force. The spring assembly comprises a first spring arranged to be compressed by the piston throughout a first range of motion of the piston in a compression direction, and at least a second spring arranged to be compressed by the piston throughout a second range of motion that is smaller than and co-terminal with the first range of motion but to be uncompressed during an initial part of the first range of motion of the piston in the compression direction.
Public/Granted literature
- US20100175376A1 TURBOCHARGER SYSTEM WITH TURBINE BYPASS VALVE ACTUATED BY MULTIPLE-RATE FLUID PRESSURE ACTUATOR Public/Granted day:2010-07-15
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