US5406795A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Exhaust manifold to turbine casing flanges
Assignee: Cummins Engine IP Inc
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Filing: 1994-01-21
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Granted: 1995-04-18
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Expires: 2014-01-21
Abstract
Abstract An internal combustion engine has a turbocharger inlet flange mounted to the outlet flange of the exhaust manifold of the engine. The exhaust gas flow out of the manifold is through two ports having a centrally located guide wall directing flow from the manifold out the flange into the turbocharger inlet. The two ports are trapezoidal in shape with a short common dividing wall which, for each port, blends at a short radius into two diverging straight walls, one at each end of the common wall, and which blend from their ends into the outer wall of the port, resulting in trapezoidal port shape. The inlet flange of the turbocharger casing has ports matching and in registry with the two ports of the exhaust manifold flange.
Inventors
- 👤 Jonathan H. Raub
- 👤 Glenn L. Baker
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 08:27
CPC Classifications
F; F02; F02B; F02B67/00; F02B67/10; F01; F01D; F01D9/00; F01D9/02; F01D9/026; F01N; F01N13/00; F01N13/08; F01N13/10; F01N13/107; F02B37/00; F02B37/02; F02B37/025; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 31
Claim 1
Independent Claim
82 words
An internal combustion engine exhaust manifold flange, for receiving thereon a turbocharger casing inlet flange, and wherein: the exhaust manifold flange has four outer corners and two exhaust ports inboard of the corners, the ports having a common dividing wall, each port having two generally straight walls extending outward from the dividing wall toward two of the corners, and each port having an outer wall extending generally parallel to the dividing wall whereby each of the ports has a generally trapezoidal shape.
Claim 2
Dependent Claim
82 words
An internal combustion engine exhaust manifold flange, for receiving thereon a turbocharger casing inlet flange, and wherein: the exhaust manifold flange has four outer corners and two exhaust ports inboard of the corners, the ports having a common dividing wall, each port having two generally straight walls extending outward from the dividing wall toward two of the corners, and each port having an outer wall extending generally parallel to the dividing wall whereby each of the ports has a generally trapezoidal shape.
Claim 3
Dependent Claim
35 words
The exhaust manifold flange of claim 1 and further comprising, for each port: transition walls between the dividing wall and the two outwardly extending walls, and between the outwardly extending walls and the outer wall.
Claim 4
Dependent Claim
28 words
The flange of claim 2 wherein: the length of the dividing wall is less than the length of any other wall of the port except the transition walls.
Claim 5
Dependent Claim
30 words
The flange of claim 2 and wherein: each of the transition walls between the dividing wall and the outwardly extending walls has at least one radius less than 7 mm.
Claim 6
Dependent Claim
35 words
The flange of claim 2 and wherein: each of the transition walls between the dividing wall and time outwardly extending walls has a length not exceeding eight percent of the internal perimeter of the port.
Claim 7
Dependent Claim
48 words
The flange of claim 5 and wherein: each of the transition walls between the outwardly extending walls and the outer wall has a short straight portion and a curved portion at each end of the short straight portion; and the two ports are mirror images of each other.
Claim 8
Dependent Claim
55 words
An exhaust inlet flange in a turbocharger casing and wherein: the flange has exhaust inlet porks matching the porks of the exhaust manifold flange of claim 1, the exhaust inlet flange being fastened to the manifold flange, with the inlet ports of the inlet flange in registry with the porks of the exhaust manifold flange.
Claim 9
Dependent Claim
57 words
The combination of claim 7 and wherein: the turbocharger inlet flange has a face which is symmetrical about a first plane which is perpendicular to the face and contains the dividing wall, and the face is symmetrical about a second plane which is perpendicular to the face and to the dividing wall and bisects the dividing wall.
Claim 10
Dependent Claim
74 words
An exhaust inlet flange in a turbocharger casing and wherein: the flange has four outer corners and two exhaust inlet ports inboard of the corners, the ports having a common dividing wall, each port having two generally straight walls extending outward from the dividing wall toward two of the corners, and each pork having an outer wall extending generally parallel to the dividing wall whereby each of the ports has a generally trapezoidal shape.
Claim 11
Dependent Claim
74 words
An exhaust inlet flange in a turbocharger casing and wherein: the flange has four outer corners and two exhaust inlet ports inboard of the corners, the ports having a common dividing wall, each port having two generally straight walls extending outward from the dividing wall toward two of the corners, and each pork having an outer wall extending generally parallel to the dividing wall whereby each of the ports has a generally trapezoidal shape.
Claim 12
Dependent Claim
33 words
The flange of claim 9 and further comprising, for each port: transition walls between the dividing wall and the two outwardly extending walls, and between the outwardly extending walls and the outer wall.
Claim 13
Dependent Claim
27 words
The flange of claim 10 wherein: the length of the dividing wall is less than the length of any other wall of the port except transition walls.
Claim 14
Dependent Claim
32 words
The flange of claim 10 and wherein: each of the transition walls between the dividing wall and the outwardly extending walls is curved with at least one radius less than 7 mm.
Claim 15
Dependent Claim
35 words
The flange of claim 12 and wherein: each of the transition walls between the dividing wall and the outwardly extending walls has a length not exceeding eight percent of the internal perimeter of the port.
Claim 16
Dependent Claim
49 words
The flange of claim 10 and wherein: each of the transition walls between the outwardly extending walls and the outer wall has a short straight portion and a short curved portion at each end of the short straight portion; and the two ports are mirror images of each other.
Claim 17
Dependent Claim
121 words
An internal combustion engine exhaust manifold outlet to turbocharger inlet assembly comprising: an exhaust manifold outlet portion having four outer corners and two exhaust outlet ports inboard of the corners, the ports having a common dividing wall, each port having two generally straight walls extending outward from the dividing wall toward two of the corners, and each port having an outer wall extending generally parallel to the dividing wall whereby each of the ports has a generally trapezoidal shape; and a turbocharger inlet portion mounted to the exhaust manifold outlet portion and having two exhaust inlet ports in registry with the outlet ports of the exhaust manifold and having a generally trapezoidal shape matching the shape of the exhaust outlet ports.
Claim 18
Dependent Claim
121 words
An internal combustion engine exhaust manifold outlet to turbocharger inlet assembly comprising: an exhaust manifold outlet portion having four outer corners and two exhaust outlet ports inboard of the corners, the ports having a common dividing wall, each port having two generally straight walls extending outward from the dividing wall toward two of the corners, and each port having an outer wall extending generally parallel to the dividing wall whereby each of the ports has a generally trapezoidal shape; and a turbocharger inlet portion mounted to the exhaust manifold outlet portion and having two exhaust inlet ports in registry with the outlet ports of the exhaust manifold and having a generally trapezoidal shape matching the shape of the exhaust outlet ports.
Claim 19
Dependent Claim
37 words
The assembly of claim 15 and wherein: the length of the dividing wall between each of the two ports of a portion is less than the length of any of the other three walls of the ports.
Claim 20
Dependent Claim
52 words
The assembly of claim 15 and wherein: the exhaust manifold outlet portion is a flange with a bolt hole in each of the four corners; the turbocharger inlet portion is a flange with a bolt hole in each of the corners; and bolts received in the bolt holes fasten the flanges together.
Claim 21
Dependent Claim
39 words
The assembly of claim 17 and further comprising: a gasket sandwiched between the flanges and having a port in registry with the ports of the flanges and shaped like the ports of the flanges but without the dividing wall.
Claim 22
Dependent Claim
147 words
In a turbocharger casing for mounting to an engine exhaust manifold outlet flange, the improvement comprising: a turbine intake passageway inlet face having outer corners for receiving fasteners for connection to an engine exhaust manifold flange, the shape of the face being symmetrical with respect to a first plane perpendicular to the face, and the shape of the face being symmetrical with respect to a second plane perpendicular to the face and to the first plane, exhaust inlet port means in the face and having two pairs of diverging walls, one pair of walls diverging with reference to the second plane of symmetry toward two of the corners on one side of the first plane of symmetry, and the other pair of walls diverging with respect to the second plane of symmetry toward two of the corners on the opposite side of the first plane of symmetry.
Claim 23
Dependent Claim
147 words
In a turbocharger casing for mounting to an engine exhaust manifold outlet flange, the improvement comprising: a turbine intake passageway inlet face having outer corners for receiving fasteners for connection to an engine exhaust manifold flange, the shape of the face being symmetrical with respect to a first plane perpendicular to the face, and the shape of the face being symmetrical with respect to a second plane perpendicular to the face and to the first plane, exhaust inlet port means in the face and having two pairs of diverging walls, one pair of walls diverging with reference to the second plane of symmetry toward two of the corners on one side of the first plane of symmetry, and the other pair of walls diverging with respect to the second plane of symmetry toward two of the corners on the opposite side of the first plane of symmetry.
Claim 24
Dependent Claim
74 words
The improvement of claim 19 and further comprising: a center wall in the casing at the face and lying in the first plane of symmetry and dividing the inlet port means into two inlet ports whereby the center wall is common to the two inlet ports, the first pair of walls extending from one side of the center wall, and the second pair of walls extending from the other side of the center wall.
Claim 25
Dependent Claim
26 words
The improvement of claim 20 and wherein: each wall of each pair extends from the common wall at an angle of between 120 and 125 degrees.
Claim 26
Dependent Claim
38 words
The improvement of claim 21 and wherein: each wall of a pair blends into an end of the common wall in a transition blend whose length is no greater than eight percent of the perimeter of the port.
Claim 27
Dependent Claim
35 words
The improvement of claim 22 and wherein: each port has an outer wall extending between the outer ends of the walls of the pair and which is about twice as long as the common wall.
Claim 28
Dependent Claim
33 words
The improvement of claim 23 and wherein: the combination of the common wall and the pair of walls and the outer wall of a port provides a generally trapezoidal shape of the port.
Claim 29
Dependent Claim
40 words
The improvement of claim 20 and wherein: an outer perimeter wall of the flange is scalloped with a first curve through the first plane above the second plane and a second curve through the first plane below the second plane.
Claim 30
Dependent Claim
15 words
The improvement of claim 25 and wherein the curves are centered in the first plane.
Claim 31
Dependent Claim
82 words
The improvement of claim 25 and wherein the outer perimeter wall includes straight portions extending from the curves out to the corners, two of the straight portions diverging with reference to the second plane as they extend out from the curves to the corner on one side of the first plane, and two of the straight portions diverging with reference to the second plane as they extend out from the curves to the corners on the opposite side of the first plane.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1998-04-17 | 1998-10-17 | 1999-04-18 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2002-04-17 | 2002-10-17 | 2003-04-18 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2006-04-17 | 2006-10-17 | 2007-04-18 | $7700.00 | Window Closed / Lapsed |