Turbocharger pressure compensation system

Power plants – Fluid motor means driven by waste heat or by exhaust energy... – With supercharging means for engine

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60322, 123563, 285228, F02B 2904, F16L 3500

Patent

active

057911444

ABSTRACT:
A boosted charge air system which eliminates adverse effects of pressure loading on the system components incorporates a pressure compensator mounted intermediate a turbocharger compressor section outlet duct and the inlet duct of a charge air cooler. The compensator includes first and second end bellows each with a first cross sectional area, a middle bellows intermediate the first and second end bellows with an annular cross sectional area substantially equal to the first cross sectional area, first and second end flanges connecting the first and second end bellows to the outlet duct and inlet duct, respectively, and first and second annular plates connecting the middle bellows to the first and second end bellows. An internal restraining structure for the compensator includes two sets of struts interconnecting the first end flange to the second annular plate and the second end flange to the first annular plate. For applications where exhaust pressure variations induce undesirable loading on the charge air system components a compensator, as described, is incorporated intermediate the exhaust manifold outlet duct and the turbine section inlet duct for the turbocharger.

REFERENCES:
patent: 2479104 (1949-08-01), Dreyer
patent: 2568923 (1951-09-01), McNeary et al.
patent: 4495773 (1985-01-01), Inoue et al.
patent: 4848086 (1989-07-01), Inoue et al.
patent: 5072698 (1991-12-01), Fujihira et al.
patent: 5248170 (1993-09-01), Francis
patent: 5299840 (1994-04-01), Heye
C.M. Daniels; Bellows Design for Aerospace Vehicles; Apr. 17, 1962; Sections 3.4 through 3.4.3.
Report of Pre-Flight Certification Test on Inboard Fuel, Pressure-Volume Compensating Duct Assembly To NASA-MSFC Specification Control Drawing 20M02003, Rev.D (Contract No. NAS8-5097) NASA-MSFC Part No. 20M02003 Arrowhead Part No. 11714 For National Aeronautics and Space Administration; George C. Marshall Space Flight Center; Huntsville, Alabama; Jun. 18, 1965.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Turbocharger pressure compensation system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbocharger pressure compensation system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbocharger pressure compensation system will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-378255

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.