Drone elimination muffler

Patent metadata

Field	Value
Publication number	US-10519828-B2
Application number	US-201715427892-A
Country	US
Kind code	B2
Filing date	Feb 8, 2017
Priority date	Apr 9, 2015
Publication date	Dec 31, 2019
Grant date	Dec 31, 2019

Abstract

An apparatus and method are provided for a drone elimination muffler to attenuate drone exhibited by engine exhaust systems. The drone elimination muffler comprises a hollow canister having a length and a diameter, and a tuned port comprising a first end connected to the canister and a second end connected to the exhaust system. The canister operates in concert with the tuned port as a dampener configured to substantially attenuate exhaust drone, or resonance, at one or more frequencies of engine operation. A valve is configured to switch the drone elimination muffler between a closed state in which the exhaust system operates without acoustic influence due to the drone elimination muffler, and an open state in which the drone elimination muffler directly influences the acoustic properties of the exhaust system.

First claim

What is claimed is:

1. A drone elimination muffler to attenuate drone exhibited by exhaust systems, comprising:
a canister comprising a hollow cylindrical body having a length and a diameter;
a tuned port comprising (i) a first end connected to the canister and a second end connected to the exhaust system, such that the canister and the tuned port operate in concert to substantially attenuate exhaust drone at one or more frequencies of engine operation, wherein the second end is connected to the exhaust system at an outlet of a second muffler, and (ii) a damper clamped within a joint between the canister and the exhaust system, wherein the damper comprises a perforated stainless steel sheet; and
a first thermocouple in thermal contact with the tuned port, the first thermocouple being configured to detect and monitor a temperature of the tuned port to facilitate maximizing attenuation of drone in the exhaust system by adjustably tuning the drone elimination muffler during exhaust gas temperature changes in concert with the damper.

2. The drone elimination muffler of claim 1 , wherein the tuned port comprises a short, side mounted tuned port.

3. The drone elimination muffler of claim 2 , wherein the damper comprises a 40% open perforated stainless steel sheet.

4. The drone elimination muffler of claim 1 , wherein a valve is disposed between the second end and the exhaust system so as to enable switching the drone elimination muffler between a closed state in which the exhaust system operates without acoustic influence due to the drone elimination muffler, and an open state in which the drone elimination muffler directly influences the acoustic properties of the exhaust system.

5. The drone elimination muffler of claim 1 , wherein the first thermocouple is in thermal contact with the tuned port, and a second thermocouple is in thermal contact with the canister, the first and second thermocouples being configured to respectively detect the temperature of the tuned port and a temperature of the canister.

6. The drone elimination muffler of claim 5 , wherein the first and second thermocouples are configured to respectively monitor the temperature of the tuned port and the canister so as to facilitate responding to exhaust gas temperature changes.

7. The drone elimination muffler of claim 1 , wherein the length is substantially 12 inches and the diameter is substantially 6 inches, and the tuned port comprises a length selected so as to attenuate a frequency of substantially 100 Hertz (Hz).

8. A method for attenuating drone exhibited by an exhaust system of an internal combustion engine, comprising:
providing a hollow canister having a length and a diameter suitable for use in a drone elimination muffler;
selecting a tuned port having a length and diameter suitable for operating in concert with the hollow canister to attenuate exhaust drone, wherein selecting the tuned port includes clamping a damper clamped within a joint between the hollow canister and the exhaust system, wherein the damper comprises a perforated stainless steel sheet;
connecting a first end of the tuned port to the canister and connecting a second end of the tuned port to the exhaust system, such that the canister and the tuned port substantially attenuate exhaust drone at one or more frequencies of engine operation, wherein the second end is connected to the exhaust system at an outlet of a second muffler; and
thermally connecting a first thermocouple with the tuned port, the first thermocouple being configured to detect and monitor a temperature of the tuned port to facilitate maximizing attenuation of drone in the exhaust system by adjustably tuning the drone elimination muffler during exhaust gas temperature changes in concert with the damper.

9. The method of claim 8 , wherein selecting the tuned port further comprises accounting for effects due to an operating temperature, or a temperature range, of the exhaust system.

10. The method of claim 8 , wherein providing the hollow canister further comprises maximizing a size of the drone elimination muffler so as to increase an effective bandwidth of attenuation.

11. The method of claim 8 , further comprising ensuring a natural frequency of the drone elimination muffler is substantially equal to an excitation frequency of the exhaust system so as to optimize attenuation of drone exhibited by the exhaust system.

12. The method of claim 11 , further comprising ensuring the dimensions of the drone elimination muffler do not exceed substantially a quarter wavelength of the natural frequency of the drone elimination muffler so as to minimize any effects due to standing waves within the hollow canister.

13. The method of claim 8 , wherein comprises at least a 40% open perforated stainless steel sheet.

14. The method of claim 8 , further comprising placing a first thermocouple in thermal contact with the tuned port, and placing a second thermocouple in thermal contact with the hollow canister, the first and second thermocouples being configured to respectively detect a temperature of the tuned port and a temperature of the hollow canister.

15. The method of claim 14 , further comprising configuring the first and second thermocouples to respectively monitor the temperature of the tuned port and the hollow canister for the purpose of optimizing attenuation of drone in the exhaust system during exhaust gas temperature changes.

16. The method of claim 8 , further comprising incorporating a valve into the second end of the tuned port so as to enable switching the drone elimination muffler between a closed state in which the exhaust system operates in absence of influence due to the drone elimination muffler, and an open state in which the drone elimination muffler attenuates drone exhibited by the exhaust system.

Assignees

• K&N Eng Inc

Inventors

• Williams Steve
• Mcclelland Kevin

Classifications

• F01N1/082

  by passing the exhaust gases through porous members · CPC title

• F01N1/023 Primary

  Helmholtz resonators · CPC title

• F01N2560/06

  the means being a temperature sensor · CPC title

• F01N1/02

  by using resonance · CPC title

• F01N1/163

  by means of valves · CPC title