Granted Patent B2

US 10,495,113 · App. 15/431,798 · Granted Dec 3, 2019

Inventors: Bhushan Singh Gautam (Karnataka, IN); Gladys Gaude (Girmont, FR)

Assignee: GARRETT TRANSPORATION I INC.

F04D29/665F02B33/40F02B33/44F02B37/00F02M35/10157F02M35/1266F04D17/10F04D29/4206Y02T10/144

Abstract

Claims (57)

1. An acoustic damper comprising:

an upstream wall with an inlet aperture;

a downstream wall with an outlet aperture;

a first resonator with a first cylinder that is attached at a first end to the upstream wall and that is attached at a second end to the downstream wall, the upstream wall, the downstream wall, and the first cylinder cooperating to define a chamber;

a second resonator with a second cylinder attached to the upstream wall and surrounded by the first cylinder in the chamber;

a third resonator with a third cylinder that is attached to the upstream wall and surrounded by the second cylinder;

wherein the first resonator, the second resonator, and the third resonator are arranged in-parallel; and

wherein the first resonator, the second resonator, and the third resonator are configured to cooperatively attenuate acoustic energy associated with a fluid flowing from the inlet aperture to the outlet aperture.

2. The acoustic damper of claim 1 , wherein the acoustic damper defines an axis;

wherein the first resonator and the second resonator are substantially coaxial with respect to the axis.

3. The acoustic damper of claim 1 , wherein the first resonator extends along an axis between the upstream wall and the downstream wall;

wherein the first resonator has a first length measured along the axis;

wherein the second resonator has a second length measured along the axis;

wherein the third resonator has a third length measured along the axis;

wherein the first length is greater than the second length; and

wherein the second length is greater than the third length.

4. The acoustic damper of claim 1 , wherein the first resonator extends along an axis between the upstream wall and the downstream wall;

wherein a first radial gap is defined between the first cylinder and the second cylinder;

wherein a second radial gap is defined between the second cylinder and the third cylinder; and

wherein the first radial gap is substantially equal to the second radial gap.

5. The acoustic damper of claim 1 , wherein at least one of the first cylinder and the second cylinder is a right cylinder with an upstream end and a downstream end that are coaxially aligned with a common axis;

wherein the common axis is straight.

6. The acoustic damper of claim 5 , wherein the at least one of the first cylinder and the second cylinder is a right circular cylinder.

7. The acoustic damper of claim 1 , further comprising an inlet pipe with an inlet passage that is in fluid communication with the inlet aperture; and

wherein the inlet pipe is configured to be attached to a compressor section of a turbocharger.

8. An acoustic damper comprising:

a first resonator with a first hollow cylinder that extends about an axis in a circumferential direction, the first hollow cylinder extending along the axis between an upstream wall and a downstream wall, the first hollow cylinder having a first length measured along the axis;

a second resonator with a second hollow cylinder that extends about the axis in the circumferential direction, the second hollow cylinder having a second length measured along the axis;

a third resonator with a third hollow cylinder that extends about the axis in the circumferential direction, the third hollow cylinder having a third length measured along the axis;

wherein the second hollow cylinder is surrounded by the first hollow cylinder and the third hollow cylinder is surrounded by the second hollow cylinder;

wherein the first length is greater than the second length and the second length is greater than the third length; and

wherein the first hollow cylinder, the second hollow cylinder, and the third hollow cylinder are configured to cooperatively attenuate acoustic energy associated with a fluid flowing through the acoustic damper.

9. The acoustic damper of claim 8 ,

wherein the first hollow cylinder includes a first end and a second end, and wherein the second hollow cylinder includes a third end and a fourth end;

wherein the first end and the third end are attached to the upstream wall;

wherein the second end is attached to the downstream wall; and

wherein the fourth end is spaced apart from the downstream wall.

10. The acoustic damper of claim 8 , wherein the first cylinder and the second cylinder are substantially coaxial and centered on the axis.

11. The acoustic damper of claim 10 ,

wherein the upstream wall includes an upstream aperture and the downstream wall includes a downstream aperture; and

wherein the upstream aperture and the downstream aperture are substantially centered on the axis.

12. The acoustic damper of claim 10 , wherein the first cylinder and the second cylinder are right circular cylinders.

13. The acoustic damper of claim 8 , further comprising an inlet pipe with an inlet passage that is in fluid communication with the first and second hollow cylinders; and

wherein the inlet pipe is configured to be attached to a compressor section of a turbocharger.

14. A vehicle engine system comprising:

a turbocharger with a compressor section, the compressor section having a housing; and

an acoustic damper that is in fluid communication with the housing, the acoustic damper configured to receive airflow from the compressor section;

the acoustic damper including:

an upstream wall with an inlet aperture configured to receive airflow from the compressor section;

a downstream wall with an outlet aperture configured to receive outlet airflow from the acoustic damper;

a first resonator with a first cylinder that is attached at a first end to the upstream wall and that is attached at a second end to the downstream wall, the first cylinder having a first length measured from the first end to the second end, the upstream wall, the downstream wall, and the first cylinder cooperating to define a chamber;

a second resonator with a second cylinder attached to the upstream wall and surrounded by the first cylinder in the chamber, the second cylinder having a second length that is less than the first length;

a third resonator with a third cylinder that is attached to the upstream wall and surrounded by the second cylinder, the third cylinder having a third length that is less than the second length;

wherein the first resonator, the second resonator, and the third resonator are arranged in-parallel; and

wherein the first resonator, the second resonator, and the third resonator are configured to cooperatively attenuate acoustic energy associated with the airflow from the inlet aperture to the outlet aperture.

15. The vehicle engine system of claim 14 , wherein the acoustic damper defines an axis;

wherein the first resonator and the second resonator are substantially coaxial with respect to the axis.

Assignments (8)

Continuity (1)