System and apparatus for air flow handling in an aircraft monument

Patent metadata

Field	Value
Publication number	US-11097845-B2
Application number	US-201715647711-A
Country	US
Kind code	B2
Filing date	Jul 12, 2017
Priority date	Jul 12, 2016
Publication date	Aug 24, 2021
Grant date	Aug 24, 2021

Abstract

In an illustrative embodiment, an aircraft galley ducting assembly provides airflow to at least one compartment of an aircraft galley monument. The ducting assembly may include a supply air duct that provides a supply airflow path to a compartment that includes an inlet port mounted to a compartment surface. A return air duct may provide an exit airflow path for return air that has circulated throughout the compartment and includes an outlet port mounted to the compartment surface. An airflow adjustment apparatus with an airflow adjustment surface is positioned within the supply airflow path of the supply air duct or the exit airflow path of the return air duct to cause a modification of airflow properties for air passing across or through the airflow adjustment surface.

First claim

What is claimed is:

1. A ducting assembly for providing airflow to at least one compartment of an aircraft galley monument, the ducting assembly comprising:
a supply air duct configured to provide a supply airflow path from an external air system to a first compartment of the at least one compartment, the supply air duct including an inlet port mounted to a surface of the compartment to provide an inlet path for air flowing from the supply air duct to the compartment;
a return air duct configured to provide an exit airflow path to the external air system for return air that has circulated throughout the compartment, the return air duct including an outlet port mounted to a surface of the compartment to provide an outlet path for the return air from the compartment to the return air duct; and
an airflow adjustment apparatus including an airflow adjustment surface disposed within at least one of the supply airflow path of the supply air duct and the exit airflow path of the return air duct, the airflow adjustment surface configured to cause a modification of airflow properties for air flowing across or through the airflow adjustment surface,
wherein the airflow adjustment apparatus includes a mounting surface disposed around a periphery of the air flow adjustment surface and substantially parallel to the airflow adjustment surface, wherein the mounting surface is configured to provide one or more locations for mounting the airflow adjustment apparatus to at least one air duct wall,
wherein a shape of the airflow adjustment apparatus corresponds to a shape of an interior of the supply air duct or the return air duct such the airflow adjustment apparatus fits snugly within an interior of the supply air duct or the return air duct,
wherein the airflow adjustment apparatus includes a mounting surface positioned substantially perpendicular to the airflow adjustment surface,
wherein the airflow adjustment surface includes a plurality of apertures arranged in predetermined patterns across a length and width of the airflow adjustment surface such that the air flowing through supply air duct or the return air duct flows through the plurality of apertures,
wherein the plurality of apertures includes a first set of apertures having a first diameter and a second set of apertures having a second diameter that is larger than the first diameter,
wherein the air flowing through the first set of apertures is configured to produce a first audible tone at a first frequency, and the air flowing through the second set of apertures is configured to produce a second audible tone at a second frequency such that a mutual frequency cancellation between the first audible tone and the second audible tone is configured to prevent a prominent audible tone at a single frequency.

2. The ducting assembly of claim 1 , wherein the airflow properties include at least one of pressure, velocity, direction, and sound frequency.

3. The ducting assembly of claim 1 , wherein the airflow adjustment surface is positioned substantially perpendicular to a direction of airflow through the supply air duct or the return air duct.

4. The ducting assembly of claim 1 , wherein a wall of the supply air duct or the return air duct includes a slot disposed within the wall, wherein the airflow adjustment apparatus is configured to be inserted through the wall into an interior of the supply air duct or the return air duct.

5. The ducting assembly of claim 4 , wherein a width of the slot within the wall of the supply air duct or the return air duct corresponds to a greatest width of the airflow adjustment apparatus.

6. The ducting assembly of claim 4 , wherein the mounting surface is configured to be mounted to an outer surface of the wall at one or more mounting locations when the airflow adjustment apparatus is inserted into the slot.

7. A compartment disposed within an aircraft galley monument, the aircraft galley compartment comprising:
an enclosure configured to house an equipment item, the enclosure comprising a rear surface, an upper wall, and opposing side walls, wherein at least one of the rear surface, upper wall, or opposing side walls includes one or more air duct connections; and
a ducting assembly comprising
a supply air duct configured to provide a supply airflow path from an external air system to the enclosure, the supply air duct including an inlet port mounted to a surface of the enclosure to provide an inlet path for air flowing from the supply air duct to the enclosure,
a return air duct configured to provide an exit airflow path to the external air system for return air that has circulated throughout the enclosure, the return air duct including an outlet port mounted to a surface of the enclosure to provide an outlet path for the return air from the enclosure to the return air duct, and
an airflow adjustment apparatus including an airflow adjustment surface disposed within at least one of the supply airflow path of the supply air duct and the exit airflow path of the return air duct, the airflow adjustment surface configured to cause a modification of airflow properties for air passing across or through the airflow adjustment surface,
wherein the airflow adjustment apparatus includes a mounting surface disposed around a periphery of the air flow adjustment surface and substantially parallel to the airflow adjustment surface, wherein the mounting surface is configured to provide one or more locations for mounting the airflow adjustment apparatus to at least one air duct wall,
wherein a shape of the airflow adjustment apparatus corresponds to a shape of an interior of the supply air duct or the return air duct such the airflow adjustment apparatus fits snugly within an interior of the supply air duct or the return air duct,
wherein the airflow adjustment apparatus includes a mounting surface positioned substantially perpendicular to the airflow adjustment surface,
wherein the airflow adjustment surface includes a plurality of apertures arranged in predetermined patterns across a length and width of the airflow adjustment surface such that the air flowing through the supply air duct or the return air duct flows through the plurality of apertures,
wherein the plurality of apertures includes a first set of apertures having a first diameter and a second set of apertures having a second diameter that is larger than the first diameter,
wherein the air flowing through the first set of apertures is configured to produce a first audible tone at a first frequency, and the air flowing through the second set of apertures is configured to produce a second audible tone at a second frequency such that a mutual frequency cancellation between the first audible tone and the second audible tone is configured to prevent a prominent audible tone at a single frequency.

8. The compartment of claim 7 , wherein a wall of the supply air duct or the return air duct includes a slot disposed across a width of the wall, wherein the airflow adjustment apparatus is configured to be inserted through the wall into an interior of the supply air duct or the return air duct.

9. The compartment of claim 8 , wherein a width of the slot within the wall of the supply air duct or the return air duct corresponds to a greatest width of the airflow adjustment apparatus.

10. The compartment of claim 8 , wherein the mounting surface is configured to be mounted to an outer surface of the wall at one or more mounting locations when the airflow adjustment apparatus is inserted into the slot.

Assignees

• Be Aerospace Inc

Inventors

• Burd Peter John Leslie
• Elshaw Neil R
• Foster Sam
• Neti Venkata Prasanth Suman
• Davidson Merv
• Payne Elizabeth M
• Ray Christopher
• Siddiqui Danyal
• Kashikov Boryan

Classifications

• E05C3/004

  about an axis perpendicular to the surface on which the fastener is mounted · CPC title

• B64F5/00

  Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for · CPC title

• B64D2013/0629

  with subsystems for cooling food, catering or special loads · CPC title

• Y10T292/1043

  Swinging · CPC title

• F25D2500/02

  Geometry problems · CPC title