Low speed high pressure ratio turbocharger

• US 6,062,028 A
• Filed: 07/02/1998
• Issued: 05/16/2000
• Est. Priority Date: 07/02/1998
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Inventors: Arnold, Steven Don, Vrbas, Gary D.
• Primary Examiner(s): KAMEN, NOAH P
• Application Number:
  US09/109,538
• Time in Patent Office: 684 Days
• Field of Search: 60/612, 417/407
• US Class Current: 60/612
• CPC Class Codes: F02C 6/12 Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
• CPC Class Codes: F04D 25/024 the driving means being assisted by a power recovery turbine
• CPC Class Codes: F04D 29/286 multi-stage rotors
• CPC Class Codes: F04D 29/4206 especially adapted for elastic fluid pumps

Abstract

A low speed high pressure ration turbocharger incorporates a compressor impeller having impeller blades for a first stage of compression mounted on a first side of the wheel and impeller blades for a second stage of compression mounted on a second side of the wheel. Driving the dual sided compressor impeller on a common shaft from the turbine wheel allows reduction in rotational speeds while increasing compression ratio of the turbine. The scroll inlet and outlet volute for the second stage inducer are integrated with the compressor housing or other portions of the turbocharger case for compact packaging.

Claims

1. A turbocharger comprising:

a case having a turbine housing receiving exhaust gas from an exhaust manifold of an internal combustion engine at an inlet and having an exhaust outlet, a compressor housing having an air inlet and a first volute, and a center housing intermediate the turbine housing and compressor housing;

a turbine wheel carried within the turbine housing and extracting energy from the exhaust gas, said turbine wheel connected to a shaft extending from the turbine housing through a shaft bore in the center housing;

a bearing supported in the shaft bore of the center housing, said bearing supporting the shaft for rotational motion;

a compressor impeller connected to the shaft opposite the turbine wheel and carried within the compressor housing, said compressor impeller having a first plurality of impeller blades mounted on a front face proximate the air inlet, said first plurality of blades increasing the velocity of air from the air inlet and exhausting air into the first volute, said compressor impeller also having a second plurality of impeller blades mounted on a back face, said second plurality of blades increasing the velocity of air from a scroll inlet connected to the first volute, and exhausting air into a second volute having a charge air outlet connected to an inlet manifold for the engine, said scroll inlet and second volute integral to the case intermediate said compressor housing and turbine housing.

2. A turbocharger as defined in claim 1 further comprising:

a first diffuser intermediate the compressor wheel and first volute and a second diffuser intermediate the compressor wheel and the second volute, the first and second diffusers separated by a common wall extending from a peripheral circumference of the compressor wheel to the first and second volutes; and

means for creating a dynamic seal between the common wall and compressor wheel.

3. A turbocharger as defined in claim 2 wherein the common wall comprises a baffle extending from the compressor housing proximate the first volute.

4. A turbocharger as defined in claim 1 wherein the second scroll inlet and second volute are integral with the center housing containing the bearing and lubrications system.

5. A turbocharger as defined in claim 2 wherein the means for creating a dynamic seal comprises:

a seal ring received in a peripheral groove in the compressor impeller and carried by a relieved shoulder extending radially inward from the common wall proximate the impeller wheel peripheral circumference.

6. A turbocharger as defined in claim 2 wherein the means for creating a dynamic seal comprises:

an extended portion of the common wall closely received in a slot in the peripheral circumference of the impeller wheel, said extended portion having a serpentine surface on at least one side thereof.

7. A turbocharger comprising:

a case having a turbine housing receiving exhaust gas from an exhaust manifold of an internal combustion engine at an inlet and having an exhaust outlet, a compressor housing having an air inlet and a first volute, and a center housing intermediate the turbine housing and compressor housing;

a turbine wheel carried within the turbine housing and extracting energy from the exhaust gas, said turbine wheel connected to a shaft extending from the turbine housing through a shaft bore in the center housing;

a bearing supported in the shaft bore of the center housing, said bearing supporting the shaft for rotational motion;

a compressor impeller connected to the shaft opposite the turbine wheel and carried within the compressor housing, said compressor impeller having a first plurality of impeller blades mounted on a front face proximate the air inlet, said first plurality of blades increasing the velocity of air from the air inlet and exhausting air into the first volute, said compressor impeller also having a second plurality of impeller blades mounted on a back face, said second plurality of blades increasing the velocity of air from an inlet connected to the first volute, and exhausting air into a second volute having a charge air outlet connected to an inlet manifold for the engine, said second volute substantially concentrically contained within the first volute and the outlet including an interconnection section extending through an outer wall of the first volute.

8. A turbocharger as defined in claim 7 wherein the interconnection section is wedge shaped.

9. A turbocharger as defined in claim 7 further comprising:

a first diffuser intermediate the compressor wheel and first volute and a second diffuser intermediate the compressor wheel and the second volute, the first and second diffusers separated by a common wall extending from a peripheral circumference of the compressor wheel to the first and second volutes; and

means for creating a dynamic seal between the common wall and compressor wheel.