Air induction system having an acoustic resonator

Patent metadata

Field	Value
Publication number	US-9366173-B2
Application number	US-201414530777-A
Country	US
Kind code	B2
Filing date	Nov 2, 2014
Priority date	Nov 2, 2014
Publication date	Jun 14, 2016
Grant date	Jun 14, 2016

Abstract

A resonator for attenuating sound waves produced by an engine is provided. The resonator includes a housing. The housing includes first, second and third portions defining first, second and third working chambers, respectively. The first, second and third portions cooperate to define a substantially T-shaped resonator operable to attenuate sound produced by the engine.

First claim

What is claimed is:

1. A resonator for attenuating sound waves produced by an engine, the resonator comprising:
a resonator housing including first, second and third portions defining first, second and third working chambers, respectively;
wherein the first, second and third portions cooperate to define a substantially T-shaped resonator operable to attenuate sound produced by the engine;
the resonator is adapted to attenuate sound waves produced by the engine having at least two different frequencies;
a coupling member having a first opening, a second opening and a third opening, wherein the first, second and third portions extend from the first, second and third openings, respectively;
wherein the first portion has a first end connected to an air induction system of the engine, and a second end connected to and in fluid communication with the coupling member;
wherein the second and third portions each have a first end connected to and in fluid communication with the coupling member and are oriented generally perpendicular to the first portion;
wherein the second end of the first portion is arranged to slide within or otherwise telescope relative to the coupling member such that the length of the first portion is adjustable for tuning the resonator.

2. The resonator of claim 1 , wherein
the second portion and/or third portion is arranged to slide within or otherwise telescope relative to the coupling member such that the length of the second portion and/or third portion is adjustable for tuning the resonator.

3. The resonator of claim 1 , wherein
the resonator is adapted to attenuate sound waves produced by the engine having three dominant frequencies.

4. The resonator of claim 1 , wherein
the resonator has a first effective length Leff 1 for attenuating sound waves defined by Leff 1 =(Lc/Lb)*Lc+Lb+La, where Lc is a length of the third portion, Lb is a length of the second portion, and La is a length of the first portion.

5. The resonator of claim 4 , wherein
the resonator has a second effective length Leff 2 for attenuating sound waves defined by Leff 2 =Lc+Lb.

6. The resonator of claim 5 , wherein
the resonator has a third effective length Leff 3 for attenuating sound waves defined by Leff 3 =Lc+La.

7. The resonator of claim 1 , wherein
the resonator defines first, second, and third effective lengths for respectively alternating first, second, and third distinct frequencies.

8. An air induction system for attenuating sound waves produced by an engine, the air induction system comprising:
a conduit for transmitting a source of intake air to an engine; and
a resonator including first, second, and third portions, the first portion having a first end connected to and in fluid communication with the conduit, the second and third portions in fluid communication with a second end of the first portion and oriented generally perpendicular to the first portion;
wherein the resonator is adapted to attenuate sound waves produced by the engine having at least two different frequencies;
a coupling member having a first opening, a second opening and a third opening, wherein the first, second and third portions extend from the first, second and third openings, respectively;
wherein the second end of the first portion is connected to and in fluid communication with the coupling member;
wherein the second and third portions each have a first end connected to and in fluid communication with the coupling member and are oriented generally perpendicular to the first portion;
wherein the second end of the first portion is arranged to slide within or otherwise telescope relative to the coupling member such that the length of the first portion is adjustable for tuning the resonator.

9. The air induction system of claim 8 , wherein
the second portion and/or third portion is arranged to slide within or otherwise telescope relative to the coupling member such that the length of the second portion and/or third portion is adjustable for tuning the resonator.

10. The air induction system of claim 8 , wherein
the resonator is adapted to attenuate sound waves produced by the engine having three distinct frequencies.

11. The resonator of claim 8 , wherein
the resonator has a first effective length Leff 1 for attenuating sound waves defined by Leff 1 =(Lc/Lb)*Lc+Lb+La, where Lc is a length of the third portion, Lb is a length of the second portion, and La is a length of the first portion.

12. The resonator of claim 11 , wherein
the resonator has a second effective length Leff 2 for attenuating sound waves defined by Leff 2 =Lc+Lb.

13. The resonator of claim 12 , wherein
the resonator has a third effective length Leff 3 for attenuating sound waves defined by Leff 3 =Lc+La.

14. The air induction system of claim 8 , wherein
the resonator defines first, second, and third effective lengths for respectively alternating first, second, and third distinct frequencies.

15. A method of attenuating sound waves produced by an engine, the method comprising:
providing a resonator in fluid communication with a conduit for delivering a source of intake air to the engine, the resonator having a T-shape, including a first portion, a second portion and a third portion;
tuning the resonator by sliding or otherwise telescoping the first and/or second and/or third portions to change the length of the respective first, second or third portions;
attenuating sound waves produced by the engine having a first frequency with a first effective length defined by the resonator;
attenuating sound waves produced by the engine having a second frequency with a second effective length defined by the resonator; and
attenuating sound waves produced by the engine having a third frequency with a third effective length defined by the resonator.

16. The method of claim 15 , wherein:
the first effective length Leff 1 is defined by Leff 1 =(Lc/Lb)*Lc+Lb+La, where Lc is a length of the third portion, Lb is a length of the second portion, and La is a length of the first portion;
the second effective length Leff 2 is defined by Leff 2 =Lc+Lb; and
the third effective length is defined by Leff 3 =Lc+La.

Assignees

• Mann & Hummel Gmbh

Inventors

• Mah Keat
• Patel Manish

Classifications

• F01N13/007 Primary

  Apparatus used as intake or exhaust silencer · CPC title

• F01N1/04

  having sound-absorbing materials in resonance chambers · CPC title

• F02M35/1261 Primary

  Helmholtz resonators · CPC title

• F01N1/023

  Helmholtz resonators · CPC title

• F01N1/02 Primary

  by using resonance · CPC title