Ventilation system and method of assembly

Patent metadata

Field	Value
Publication number	US-9550574-B2
Application number	US-201113288796-A
Country	US
Kind code	B2
Filing date	Nov 3, 2011
Priority date	Nov 3, 2011
Publication date	Jan 24, 2017
Grant date	Jan 24, 2017

Abstract

A ventilation system for ventilating a passenger compartment of an aircraft is disclosed herein. The ventilation system includes, but is not limited to, a nozzle that is adapted to be mounted proximate an interior of the aircraft and that is configured to direct a stream of air into the passenger compartment. The ventilation system further includes a valve that is spaced apart from the nozzle and positioned upstream of the nozzle, the valve configured to control a flow of air to the nozzle. The ventilation system still further includes a conduit that fluidly couples the valve to the nozzle. The conduit is configured to convey the flow of air from the valve to the nozzle.

First claim

What is claimed is:

1. A ventilation system for ventilating a passenger compartment of an aircraft, the ventilation system comprising:
a nozzle adapted to be mounted proximate an interior of the aircraft and configured to direct a stream of air into the passenger compartment;
a valve spaced apart from the nozzle and positioned upstream of the nozzle, the valve configured to control a flow of air to the nozzle; and
a conduit fluidly coupling the valve to the nozzle, the conduit configured to convey the flow of air from the valve to the nozzle,
wherein the nozzle includes a transitional section having a first cross-sectional area at an upstream portion of the transitional section and a second cross-sectional area at a downstream portion of the transitional section and wherein the first cross-sectional area is greater than the second cross-sectional area, wherein the nozzle includes a pintle disposed in the transitional section, and wherein the transitional section comprises a pathway surface and the pintle comprises a pintle surface, and wherein a segment of the pathway surface is substantially equidistant from a corresponding segment of the pintle surface,
wherein the pintle is attached to the nozzle via a plurality of tabs and wherein each tab of the plurality of tabs extends through a pathway formed by the pathway surface of the transitional section and the pintle surface of the pintle and wherein each tab is at least partially configured as an airfoil.

2. The ventilation system of claim 1 , wherein the nozzle is configured to accelerate the flow of air as the flow of air flows through the nozzle, thereby forming the stream of air.

3. The ventilation system of claim 1 , wherein the first cross-sectional area and the second cross-sectional area each have a generally circular configuration.

4. The ventilation system of claim 1 , wherein the nozzle is adjustable.

5. The ventilation system of claim 4 , wherein the nozzle has a generally spherical periphery.

6. The ventilation system of claim 1 , wherein the valve is an electronically actuatable valve.

7. The ventilation system of claim 1 , wherein the conduit comprises a hose.

8. A ventilation system for ventilating a passenger compartment of an aircraft, the ventilation system comprising:
a nozzle adapted to be mounted proximate an interior of the aircraft and configured to direct a stream of air into the passenger compartment;
a valve spaced apart from the nozzle and positioned upstream of the nozzle, the valve configured to control a flow of air to the nozzle;
a conduit fluidly coupling the valve to the nozzle, the conduit configured to convey the flow of air from the valve to the nozzle; and
a muffler fluidly coupled with the conduit such that the flow of air passes through the muffler, the muffler configured to absorb sound energy from the flow of air when the flow of air flows through the muffler,
wherein the nozzle includes a transitional section having a first cross-sectional area at an upstream portion of the transitional section and a second cross-sectional area at a downstream portion of the transitional section and wherein the first cross-sectional area is greater than the second cross-sectional area, wherein the nozzle includes a pintle disposed in the transitional section, and wherein the transitional section comprises a pathway surface and the pintle comprises a pintle surface, and wherein a segment of the pathway surface is substantially equidistant from a corresponding segment of the pintle surface,
wherein the pintle is attached to the nozzle via a plurality of tabs and wherein each tab of the plurality of tabs extends through a pathway formed by the pathway surface of the transitional section and the pintle surface of the pintle and wherein each tab is at least partially configured as an airfoil.

9. The ventilation system of claim 8 , wherein the muffler is a straight-through muffler.

10. The ventilation system of claim 8 , wherein the muffler is disposed between a first section of the conduit and a second section of the conduit.

11. A method of assembling a ventilation system for ventilating a passenger compartment of an aircraft, the method comprising the steps of:
gathering a valve, a conduit, and a nozzle, wherein the nozzle includes a transitional section having a first cross-sectional area at an upstream portion of the transitional section and a second cross-sectional area at a downstream portion of the transitional section and wherein the first cross-sectional area is greater than the second cross-sectional area, wherein the nozzle includes a pintle disposed in the transitional section, and wherein the transitional section comprises a pathway surface and the pintle comprises a pintle surface, and wherein a segment of the pathway surface is substantially equidistant from a corresponding segment of the pintle surface, attaching the pintle to the nozzle via a plurality of tabs and extending each tab of the plurality of tabs through a pathway formed by the pathway surface of the transitional section and the pintle surface of the pintle and configuring each tab at least partially as an airfoil;
mounting the nozzle proximate the passenger compartment of the aircraft such that the nozzle is arranged to vent into the passenger compartment;
positioning the valve proximate the passenger compartment in a location spaced apart from the nozzle; and
connecting the conduit between an output of the valve an inlet of the nozzle such that the valve and nozzle are fluidly coupled with one another via the conduit and configured to provide ventilation to the passenger compartment of the aircraft.

12. The method of claim 11 , further comprising the steps of gathering a muffler and connecting the muffler to the conduit such that the muffler is disposed between the valve and the nozzle and such that the muffler is fluidly coupled with both the nozzle and the valve.

Assignees

• Davis Allen
• Lynch Kristopher
• White Adam
• Grovenstein J R
• Gulfstream Aerospace Corp

Inventors

• Davis Allen
• Lynch Kristopher
• White Adam
• Grovenstein J R

Classifications

• Y10T29/49826

  Assembling or joining · CPC title

• B64D13/00 Primary

  Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space · CPC title

• B60H1/3442

  the frame being spherical · CPC title

• B64D2013/003

  Cabin ventilation nozzles · CPC title

• B60H2001/3478

  acting on additional damper doors · CPC title