Invention Grant
US07992388B2 Method for estimating compressor output temperature for a two-stage turbocharger
有权
估计两级涡轮增压器的压缩机输出温度的方法
- Patent Title: Method for estimating compressor output temperature for a two-stage turbocharger
- Patent Title (中): 估计两级涡轮增压器的压缩机输出温度的方法
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Application No.: US11856733Application Date: 2007-09-18
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Publication No.: US07992388B2Publication Date: 2011-08-09
- Inventor: Yong Shu , Michiel J. Van Nieuwstadt , Diana D. Brehob
- Applicant: Yong Shu , Michiel J. Van Nieuwstadt , Diana D. Brehob
- Applicant Address: US MI Dearborn
- Assignee: Ford Global Technologies, LLC
- Current Assignee: Ford Global Technologies, LLC
- Current Assignee Address: US MI Dearborn
- Main IPC: F02B33/44
- IPC: F02B33/44 ; F02B33/00

Abstract:
A method for estimating the output temperature of the output compressor of a two-stage turbocharger. The method includes: storing a composite relationship relating temperature ratio across a pair of compressors of the two-stage turbocharger as a function of mass flow through such pair of compressors and pressure drop across the pair of the compressors; calculating the pressure ratio equal to the pressure at an input to the first one of the pair of compressors to the pressure at the output of the second one of the pair compressor; using the composite relationship and an output of a mass flow at the input to the first one of the pair of compressors and the calculated pressure ratio to determine the temperature ratio across the pair of compressors; and calculating the estimated output temperature of the second one of the pair of compressors by multiplying the determined temperature ratio across the pair of compressors by a temperature at the input of the first one of the pair of compressors.
Public/Granted literature
- US20090071148A1 Method for estimating compressor output temperature for a two-stage turbocharger Public/Granted day:2009-03-19
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