Inlet diffusers for a two-stage engine charge air system

Patent metadata

Field	Value
Publication number	US-10422304-B2
Application number	US-201615176802-A
Country	US
Kind code	B2
Filing date	Jun 8, 2016
Priority date	Jun 8, 2016
Publication date	Sep 24, 2019
Grant date	Sep 24, 2019

Abstract

An aftercooler is provided comprising a housing, an outlet diverter coupled to the housing and having an outlet port, and an inlet diffuser comprising a forward wall having a peripheral rim coupled to the housing, an upper wall connected to the forward wall, a lower wall connected to the forward wall, a first side wall connected to the upper wall and the lower wall and having a first end disposed adjacent the peripheral rim and a second end disposed adjacent an inlet port of the inlet diffuser, a second side wall connected to the upper wall and the lower wall and having a first end disposed adjacent the peripheral rim and a second end disposed adjacent the inlet port, and a plurality of fins disposed within an interior volume of the inlet diffuser collectively distributing air across an outlet opening of the inlet diffuser for delivery to the housing.

First claim

We claim:

1. A system, comprising:
an engine having a first cylinder bank and a second cylinder bank disposed in a VEE configuration, each of the first and second cylinder banks having a centerline that lies in a plane that passes through a crankshaft centerline, the planes defining a VEE above the crankshaft centerline;
a low pressure turbocharger mounted within the VEE;
an intercooler mounted within the VEE and coupled to the low pressure turbocharger to cool compressed air from the low pressure turbocharger;
a high pressure turbocharger mounted within the VEE and coupled to an output of the intercooler; and
an aftercooler mounted within the VEE and coupled to the high pressure turbocharger to cool compressed air from the high pressure turbocharger;
wherein the intercooler comprises an inlet diffuser coupled to an outlet of a compressor of the low pressure turbocharger, the inlet diffuser being configured to distribute air across an outlet opening of the inlet diffuser for delivery to a housing of the intercooler;
wherein the inlet diffuser of the intercooler further comprises a forward wall having a peripheral rim, a pair of side walls, a lower wall connected to the side walls and an upper wall, the lower wall extending from the peripheral rim to a central area of the inlet diffuser and comprising an opening configured to couple to the outlet of the compressor of the low pressure turbocharger; and
wherein each side wall is connected between the lower wall and the upper wall and tapers in width from a first end adjacent the peripheral rim to a second end adjacent a central area of the inlet diffuser of the intercooler.

2. The system of claim 1 , wherein the aftercooler comprises an inlet diffuser coupled to an outlet of a compressor of the high pressure turbocharger, the inlet diffuser of the aftercooler being configured to distribute air across an outlet opening of the inlet diffuser of the aftercooler for delivery to a housing of the aftercooler.

3. The system of claim 2 , wherein the inlet diffuser of the aftercooler further comprises a forward wall having a peripheral rim with a plurality of through holes for receiving fasteners to secure the inlet diffuser of the aftercooler to the housing of the aftercooler.

4. The system of claim 3 , wherein the inlet diffuser of the aftercooler further comprises a pair of side walls, a lower wall and an upper wall, each side wall being connected between the lower wall and the upper wall and having a first end disposed adjacent the peripheral rim and a second end disposed adjacent an inlet port of the inlet diffuser of the aftercooler.

5. The system of claim 4 , wherein the upper wall and the lower wall taper in width from the inlet port to a first end of the inlet diffuser of the aftercooler and from the inlet port to a second end of the inlet diffuser of the aftercooler.

6. The system of claim 4 , wherein the inlet diffuser of the aftercooler further comprises a plurality of fins disposed within an interior volume of the inlet diffuser of the aftercooler and extending between the upper wall and the lower wall, the plurality of fins collectively distributing air across an outlet opening of the inlet diffuser of the aftercooler for delivery to a housing of the aftercooler.

7. The system of claim 1 , wherein the opening is disposed in the central area.

8. The system of claim 1 , wherein the inlet diffuser of the intercooler further comprises a plurality of ribs extending between the upper wall and the forward wall.

9. An inlet diffuser for an aftercooler, comprising:
a forward wall having a peripheral rim with a plurality of through holes for receiving fasteners to secure the inlet diffuser to a housing of the aftercooler;
an upper wall connected to the forward wall;
a lower wall connected to the forward wall;
a first side wall connected to the upper wall and the lower wall and having a first end disposed adjacent the peripheral rim and a second end disposed adjacent an inlet port of the inlet diffuser;
a second side wall connected to the upper wall and the lower wall and having a first end disposed adjacent the peripheral rim and a second end disposed adjacent the inlet port; and
a plurality of fins disposed within an interior volume of the inlet diffuser and extending between the upper wall and the lower wall, the plurality of fins collectively distributing air across an outlet opening of the inlet diffuser for delivery to the housing of the aftercooler;
wherein the plurality of fins includes a first fin which is substantially straight and slanted toward a first end of the inlet diffuser such that one end of the first fin adjacent the inlet port is farther from the first end of the inlet diffuser than another end of the first fin adjacent the forward wall;
wherein the plurality of fins includes a second fin which is substantially straight, partially disposed within the inlet port, and slanted toward a second end of the inlet diffuser such that one end of the second fin adjacent the inlet port is farther from the second end of the inlet diffuser than another end of the second fin adjacent the forward wall;
wherein the plurality of fins includes a third fin which is substantially straight and slanted toward the first end of the inlet diffuser such that one end of the third fin adjacent the inlet port is farther from the first end of the inlet diffuser than another end of the third fin adjacent the forward wall;
wherein the plurality of fins includes a fourth fin which is substantially straight and slanted toward the second end of the inlet diffuser such that one end of the fourth fin adjacent the inlet port is farther from the second end of the inlet diffuser than another end of the fourth fin adjacent the forward wall; and
wherein the plurality of fins includes a fifth fin which is curved in an elongated S-shape and slanted toward the second end of the inlet diffuser such that one end of the fifth fin adjacent the inlet port is farther from the second end of the inlet diffuser than another end of the fifth fin adjacent the forward wall, the one end being disposed within inlet port.

10. The inlet diffuser of claim 9 , wherein the upper wall and the lower wall taper in width from the inlet port to a first end of the inlet diffuser and from the inlet port to a second end of the inlet diffuser.

11. The inlet diffuser of claim 9 , wherein the first side wall is longer than the second side wall and the inlet port is offset from a central region of the inlet diffuser.

12. The inlet diffuser of claim 9 , wherein the plurality of fins includes a sixth fin which is partially curved at a first end and slanted toward the second end of the inlet diffuser such that the first end which is disposed within the inlet port is farther from the second end of the inlet diffuser than a second end of the sixth fin disposed adjacent the forward wall.

13. A system, comprising:
an engine having a first cylinder bank and a second cylinder bank disposed in a VEE configuration, each of the first and second cylinder banks having a centerline that lies in a plane that passes through a crankshaft centerline, the planes defining a VEE above the crankshaft centerline;
a low pressure turbocharger mounted within the VEE;
an intercooler mounted within the VEE and coupled to the low pressure turbocharger to cool compressed air from the low pressure turbocharger;
a high pressure turbocharger mounted within the VEE and coupled to an output of the intercooler; and
an aftercooler mounted within the VEE and coupled to the high pressure turbocharger to cool compressed air from the high pressure turbocharger;
wherein the intercooler comprises

Assignees

• Cummins Inc

Inventors

• Ntone Francois
• Saad Philipe F
• Lewis Jr Rick Vaughan
• Tsai Johnny C
• Ajotikar Nikhil Jayant

Classifications

• F02B37/013

  with exhaust-driven pumps arranged in series · CPC title

• F02B37/004

  with exhaust drives arranged in series · CPC title

• F02B67/10

  of charging or scavenging apparatus · CPC title

• F02M26/22 Primary

  with coolers in the recirculation passage · CPC title

• F02B5/02

  Methods of operating · CPC title