Coaxial fluid vent and electronic control for a fluid valve for aircraft

Patent metadata

Field	Value
Publication number	US-11059592-B2
Application number	US-201615292776-A
Country	US
Kind code	B2
Filing date	Oct 13, 2016
Priority date	Oct 13, 2016
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

A ventilation system for ventilating a passenger compartment of an aircraft, an aircraft, and a method of operating the ventilation system are disclosed herein. The ventilation system includes, but is not limited to, a bezel, a fluid vent, an electronic sensor, and a valve. The bezel defines a bezel aperture and the fluid vent defines an axis that passes through the bezel aperture to direct a stream of air through the bezel into the passenger compartment. The electronic sensor is associated with the bezel and is configured to generate a bezel position signal. The valve is configured to vary a flow rate of the stream of air through the fluid vent based on the bezel position signal.

First claim

What is claimed is:

1. A ventilation system for ventilating a passenger compartment of an aircraft, the ventilation system comprising:
a bezel defining a bezel aperture;
a fluid vent defining an axis that passes through the bezel aperture to direct a stream of air through the bezel into the passenger compartment;
an electronic sensor associated with the bezel and configured to generate a bezel position signal, wherein the electronic sensor is a switch having a first contact, a second contact, and a third contact, the position signal indicating whether the first contact has touched the second contact or the third contact; and
a valve configured to increase a flow rate of the stream of air through the fluid vent in response to the first contact touching the second contact and the valve further configured to decrease the flow rate in response to the first contact touching the third contact as indicated by the bezel position signal wherein the bezel is rotatable to interact with the electronic sensor to command the valve.

2. The ventilation system of claim 1 , further comprising an actuator configured to adjust a position of the valve in response to a rotation of the bezel as indicated by the bezel position signal.

3. The ventilation system of claim 1 , wherein the fluid vent is at least partially disposed in the bezel aperture.

4. The ventilation system of claim 1 , wherein the fluid vent is coaxial with the bezel aperture.

5. The ventilation system of claim 1 , wherein the fluid vent is an annular fluid vent, the bezel is an annular bezel, and the annular fluid vent and the annular bezel are coaxial.

6. The ventilation system of claim 1 , further comprising a biasing element biasing the bezel to a neutral position in which the switch is open with the first contact not touching the second contact and not touching the third contact.

7. The ventilation system of claim 1 , wherein the valve is spaced apart from the fluid vent and positioned upstream of the fluid vent.

Assignees

• Gulfstream Aerospace Corp

Inventors

• Lynch Kristopher
• Lucas Mike

Classifications

• B64D2013/003

  Cabin ventilation nozzles · CPC title

• B64D13/06 Primary

  the air being conditioned (pressurising B64D13/02) · CPC title

• B64D2013/0625

  comprising means for distribution effusion of conditioned air in the cabin · CPC title