Dual tube silencer for separate gas flows

Patent metadata

Field	Value
Publication number	US-11293664-B2
Application number	US-201815913688-A
Country	US
Kind code	B2
Filing date	Mar 6, 2018
Priority date	Mar 6, 2018
Publication date	Apr 5, 2022
Grant date	Apr 5, 2022

Abstract

Ventilation systems, aircraft, and silencers are disclosed herein. An aircraft includes a ventilation system. A ventilation system includes first and second air flow sources configured to generate first and second air flows, a silencer, a first conditioning vent, and a second conditioning vent. A divider spans an interior dimension of the housing to define a first cavity and a second cavity, where the divider restricts substantially all mass flow between the first cavity and the second cavity in the housing. First and second silencer tubes have porous portions disposed in the respective cavity and are operatively coupled with the respective air flow source to receive the respective air flow. First and second conditioning vents are operatively coupled with the respective silencer tubes to direct the respective air flows to a conditioned volume.

First claim

What is claimed is:

1. A ventilation system, comprising:
a first air flow source configured to generate a first air flow to service a first portion of a conditioned volume;
a second air flow source configured to generate a second air flow that is separate from the first air flow to service a second portion of the conditioned;
a silencer comprising:
a housing;
a divider spanning an interior dimension of the housing to define a first cavity and a second cavity, wherein the divider restricts substantially all mass flow of the first air flow and the second air flow between the first cavity and the second cavity in the housing;
a first silencer tube having a porous portion disposed in the first cavity, wherein the first silencer tube is operatively coupled with the first air flow source to receive the first air flow;
a second silencer tube having a porous portion disposed in the second cavity, wherein the second silencer tube is operatively coupled with the second air flow source to receive the second air flow;
acoustic deadening material disposed in the first cavity surrounding the first silencer tube, wherein the porous portion of the first silencer tube exposes acoustic energy of the first air flow to the acoustic deadening material in the first cavity to attenuate noise; and
acoustic deadening material disposed in the second cavity surrounding the second silencer tube, wherein the porous portion of the second silencer tube exposes acoustic energy of the second air flow to the acoustic deadening material in the second cavity to attenuate noise;
a first conditioning vent operatively coupled with the first silencer tube to direct the first air flow to the first portion of the conditioned volume; and
a second conditioning vent operatively coupled with the second silencer tube to direct the second air flow to the second portion of the conditioned volume,
wherein a position of the divider within the housing is based on a noise input at the first silencer tube and the second silencer tube.

2. The ventilation system of claim 1 , wherein the first air flow source and the second air flow source are components of an Environmental Control System (ECS) source for an aircraft, the first conditioning vent is a first cabin distribution for the aircraft, and the second conditioning vent is a second cabin distribution for the aircraft.

3. The ventilation system of claim 1 , further comprising a first upstream conduit and a second upstream conduit, wherein the first upstream conduit is operatively coupled with the first air flow source to direct the first air flow to the first silencer tube, and wherein the second upstream conduit is operatively coupled to the second air flow source to direct the second air flow to the second silencer tube.

4. The ventilation system of claim 1 , further comprising a first downstream conduit and a second downstream conduit, wherein the first downstream conduit is operatively coupled between the first silencer tube and the first conditioning vent and the second downstream conduit is operatively coupled between the second silencer tube and the second conditioning vent.

5. The ventilation system of claim 4 , wherein the first downstream conduit is substantially the same diameter as a first upstream conduit and the second downstream conduit is substantially the same diameter as a second upstream conduit.

6. The ventilation system of claim 1 , wherein the housing and the divider are formed from composite materials.

7. The ventilation system of claim 1 , wherein the divider is a metal baffle.

8. An aircraft, comprising:
a fuselage defining a conditioned volume having a first portion and a second portion;
an Environmental Control System (ECS) source configured to generate a first air flow and a second air flow separate from the first air flow to separately service the first portion and the second portion of the conditioned volume;
a first upstream conduit operatively coupled with the ECS source to receive the first air flow;
a second upstream conduit operatively coupled with the ECS source to receive the second air flow;
a silencer comprising:
a housing;
a divider spanning an interior dimension of the housing to define a first cavity and a second cavity, wherein the divider restricts substantially all mass flow between the first cavity and the second cavity in the housing;
a first silencer tube with an output port, an input port operatively coupled with the first upstream conduit, and a porous portion disposed in the first cavity;
a second silencer tube with an output port, an input port operatively coupled with the second upstream conduit, and a porous portion disposed in the second cavity;
acoustic deadening material disposed in the first cavity surrounding the first silencer tube, wherein the porous portion of the first silencer tube exposes acoustic energy of the first air flow to the acoustic deadening material in the first cavity to attenuate noise; and
acoustic deadening material disposed in the second cavity surrounding the second silencer tube, wherein the porous portion of the second silencer tube exposes acoustic energy of the second air flow to the acoustic deadening material in the second cavity to attenuate noise;

a first downstream conduit operatively coupled with the output port of the first silencer tube;
a second downstream conduit operatively coupled with the output port of the second silencer tube;
a first conditioning vent operatively coupled with the first downstream conduit and disposed in the first portion of the conditioned volume for conditioning the first portion of the conditioned volume; and
a second conditioning vent operatively coupled with the second downstream conduit and disposed in the second portion of the conditioned volume for conditioning the second portion of the conditioned volume, and
wherein the divider is positioned based on a first noise profile at the first conditioning vent and on a second noise profile at the second conditioning vent.

9. The aircraft of claim 8 , wherein the position of the divider is positioned further based on a noise input at the input port of the first silencer tube and the second silencer tube.

10. The aircraft of claim 8 , wherein the housing and the divider are formed from composite materials.

11. The aircraft of claim 8 , wherein the divider is a metal baffle.

12. The aircraft of claim 8 , wherein the first downstream conduit is substantially the same diameter as the first upstream conduit and the second downstream conduit is substantially the same diameter as the second upstream conduit.

Assignees

• Gulfstream Aerospace Corp

Inventors

• Hull Randy
• Gorton Andrew
• Lynch Kristopher

Classifications

• B64D2013/064

  comprising more than one system, e.g. dual systems · CPC title

• F24F13/20

  Casings or covers · CPC title

• F24F13/02

  Ducting arrangements · CPC title

• F24F13/24 Primary

  Means for preventing or suppressing noise · CPC title

• B64D2013/0603

  Environmental Control Systems · CPC title