US3946565A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Intercooler fan and compressor construction
Assignee: Wallace Murray Corp
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Filing: 1974-08-29
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Granted: 1976-03-30
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Expires: 1994-08-29
Abstract
Abstract A turbocharger for an internal combustion engine. The turbocharger is coupled to an air-to-air heat exchanger (intercooler) to cool the compressed air just prior to its entry into the engine. The turbocharger has axially spaced turbine, compressor, and fan rotors to thereby preclude undesired mixing of air streams.
Inventors
- 👤 John Frederick Cutler
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 21:40
CPC Classifications
F; F01; F01P; F01P5/00; F01P5/02; F01P5/08; F02; F02B; F02B29/00; F02B29/04; F02B29/0406; F02B29/0425; F02B29/0431; F02B37/00; F02B37/005; F02C; F02C6/00; F02C6/04; F02C6/10; F02C6/12; F04; F04D; F04D25/00; F04D25/16; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
145 words
A turbocharger compressor of the centrifugal type and adapted to be driven by exhaust gases from the exhaust manifold of an internal combustion engine, a turbine rotor and a compressor rotor connected to and axially spaced from each other along a rotor shaft, said turbine rotor adapted to be driven by exhaust gases, compressor input and output chambers contiguous to said compressor rotor, the improvement comprising, a fan rotor coupled to and axially located along said rotor shaft at a point different from the axial locations of said turbine and compressor rotors, a duct surrounding said fan, said duct being open at one end thereof to ambient, a seal surrounding said rotor shaft to preclude mixing between gases passing through the compressor and gases passing through the duct, whereby rotation of said fan rotor causes a pressure differential and consequent air flow in the duct.
Claim 2
Dependent Claim
145 words
A turbocharger compressor of the centrifugal type and adapted to be driven by exhaust gases from the exhaust manifold of an internal combustion engine, a turbine rotor and a compressor rotor connected to and axially spaced from each other along a rotor shaft, said turbine rotor adapted to be driven by exhaust gases, compressor input and output chambers contiguous to said compressor rotor, the improvement comprising, a fan rotor coupled to and axially located along said rotor shaft at a point different from the axial locations of said turbine and compressor rotors, a duct surrounding said fan, said duct being open at one end thereof to ambient, a seal surrounding said rotor shaft to preclude mixing between gases passing through the compressor and gases passing through the duct, whereby rotation of said fan rotor causes a pressure differential and consequent air flow in the duct.
Claim 3
Dependent Claim
32 words
The turbocharger of claim 1 wherein said compressor rotor is positioned between said turbine and said fan rotors, and wherein said fan rotor is located at one end of said rotor shaft.
Claim 4
Dependent Claim
108 words
The turbocharger of claim 1 including: a. an internal combustion engine having an intake and an exhaust manifold, b. an air-to-air intercooler having a first air flowpath therethrough in heat exchange relation with a second flowpath therethrough, c. the input of said first intercooler flowpath opening to ambient, d. the output of said first intercooler flowpath coupled to the other end of said fan duct, e. the input of said second intercooler flowpath coupled to said output chamber of said compressor rotor, f. the output of said second intercooler flowpath coupled to said intake manifold, g. the output of said exhaust manifold adapted to rotate said turbine rotor.
Claim 5
Dependent Claim
16 words
The turbocharger of claim 1 wherein said fan is positioned between said turbine and compressor rotors.
Claim 6
Dependent Claim
34 words
The turbocharger of claim 4 wherein the pitch of said fan is such as to blow air in said duct towards said turbine rotor to thereby cool a housing associated with the turbine rotor.
Claim 7
Dependent Claim
16 words
The turbocharger of claim 4 wherein said duct is in the form of an annular chamber.
Claim 8
Dependent Claim
29 words
The turbocharger of claim 6 wherein said duct which is in the form of an annular chamber has a wall common to one of the chambers at said compressor.
Claim 9
Dependent Claim
16 words
The turbocharger of claim 1 wherein said seal is carried by a portion of said compressor.
References Cited (Backward Citations)
FR388991A
Cited
FR752844A
Cited
CH173387A
Cited
GB499357A
Cited
US2682365A
Cited
US2918787A
Cited
US3143103A
Cited
US3781126A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-03-30 | 1979-09-29 | 1980-03-30 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-03-30 | 1983-09-29 | 1984-03-30 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-03-30 | 1987-09-29 | 1988-03-30 | $7700.00 | Window Closed / Lapsed |