Compartment based inlet particle separator system

Patent metadata

Field	Value
Publication number	US-9719352-B2
Application number	US-201414573926-A
Country	US
Kind code	B2
Filing date	Dec 17, 2014
Priority date	Dec 17, 2014
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

A compartment based inlet particle separator system for an aircraft that includes an auxiliary power unit (APU) system compartment is provided. The system includes a separation barrier wall, a ram air inlet opening, a diffuser, and an inlet particle separator (IPS). The separation barrier wall is disposed within the APU system compartment and divides the APU system compartment into two compartments. The ram air inlet opening is formed one of the compartments. The diffuser receives ram air from a ram air inlet opening and discharges ram air into a compartment. The IPS is disposed within the a compartment between the diffuser outlet and the APU air inlet port.

First claim

What is claimed is:

1. A compartment based inlet particle separator system for an aircraft that includes an auxiliary power unit (APU) system compartment, the system comprising:
a separation barrier wall disposed within the APU system compartment and configured to divide the APU system compartment into an air inlet compartment and an APU compartment, the separation barrier wall having an APU air inlet port formed therein that provides fluid communication between the air inlet compartment and the APU compartment;
a ram air inlet opening formed in the air inlet compartment for receiving a flow of ram air;
a diffuser disposed within the air inlet compartment and having a diffuser inlet, a diffuser outlet, a bypass port disposed between the diffuser inlet and the diffuser outlet, an inner surface that defines a cross sectional flow area, a first height and a first width adjacent the diffuser inlet, and a second height and a second width adjacent the diffuser outlet, the cross sectional flow area increasing between the diffuser inlet and the diffuser outlet, the first height greater than the second height, the first width less than the second width, the diffuser inlet coupled to receive ram air from the ram air inlet opening, the diffuser outlet in fluid communication with, and configured to discharge ram air into, the air inlet compartment, the bypass port in fluid communication with the APU air inlet port;
a plurality of flow control surfaces rotationally mounted within the diffuser and movable between a first position, in which the flow control surfaces direct ram air through the bypass port and into the APU air inlet port, and a second position, in which the flow control surfaces direct ram air through the diffuser outlet; and
an inlet particle separator (IPS) disposed within the air inlet compartment between the diffuser outlet and the APU air inlet port.

2. The system of claim 1 , wherein:
the IPS system divides the air inlet compartment into a non-filtered section and a filtered section;
the non-filtered section receives the ram air discharged from the diffuser; and
the filtered section receives filtered air discharged from the IPS system.

3. The system of claim 1 , wherein the IPS comprises a plurality of vortex panels.

4. The system of claim 1 , wherein the IPS comprises a plurality of barrier filters.

5. The system of claim 4 , wherein the barrier filters are configured as self-cleaning barrier filters.

6. The system of claim 1 , wherein the IPS comprises a multi-channel particle separator (MCPS) system.

7. The system of claim 1 , further comprising:
a bellmouth structure extending from the APU air inlet port into the air inlet compartment.

8. The system of claim 1 , wherein:
the IPS system divides the air inlet compartment into a non-filtered section and a filtered section;
the non-filtered section receives the ram air discharged from the diffuser; and
the filtered section receives filtered air discharged from the IPS system.

9. The system of claim 1 , further comprising:
an APU compartment cooling duct including a cooling air inlet and a cooling air outlet and extending through the separation barrier wall, the cooling air inlet in fluid communication with the ram air inlet opening, the cooling air outlet in fluid communication with the APU compartment.

10. An auxiliary power unit (APU) air inlet system for an aircraft that includes an APU system compartment, the APU air inlet system comprising:
a separation barrier wall disposed within the APU system compartment and configured to divide the APU system compartment into an air inlet compartment and an APU compartment, the separation barrier wall having an APU air inlet port formed therein that provides fluid communication between the air inlet compartment and the APU compartment;
a ram air inlet opening formed in the air inlet compartment for receiving a flow of ram air;
a diffuser disposed within the air inlet compartment and having a diffuser inlet, a diffuser outlet, and a bypass port disposed between the diffuser inlet and the diffuser outlet, the diffuser inlet coupled to receive ram air from the ram air inlet opening, the diffuser outlet in fluid communication with, and configured to discharge ram air into, the air inlet compartment, the bypass port in fluid communication with the APU air inlet port;
a plurality of flow control surfaces rotationally mounted within the diffuser and movable between a first position, in which the flow control surfaces direct ram air through the bypass port and into the APU air inlet port, and a second position, in which the flow control surfaces direct ram air through the diffuser outlet; and
an inlet particle separator (IPS) disposed within the air inlet compartment between the diffuser outlet and the APU air inlet port.

11. The system of claim 10 , wherein:
the IPS system divides the air inlet compartment into a non-filtered section and a filtered section;
the non-filtered section receives the ram air discharged from the diffuser; and
the filtered section receives filtered air discharged from the IPS system.

12. The system of claim 10 , wherein the IPS is selected from the group consisting of a plurality of vortex panels, a plurality of barrier filters, and a multi-channel particle separator (MCPS) system.

13. The system of claim 10 , further comprising:
a bellmouth structure extending from the APU air inlet port into the air inlet compartment.

14. The system of claim 10 , wherein the diffuser is configured as a transverse diffuser.

15. The system of claim 10 , further comprising:
an APU compartment cooling duct including a cooling air inlet and a cooling air outlet and extending through the separation barrier wall, the cooling air inlet in fluid communication with the ram air inlet opening, the cooling air outlet in fluid communication with the APU compartment.

16. An auxiliary power unit (APU) air inlet system for an aircraft that includes an APU system compartment, the APU air inlet system comprising:
a separation barrier wall disposed within the APU system compartment and configured to divide the APU system compartment into an air inlet compartment and an APU compartment, the separation barrier wall having an APU air inlet port formed therein that provides fluid communication between the air inlet compartment and the APU compartment;
a ram air inlet opening formed in the air inlet compartment for receiving a flow of ram air;
a transverse diffuser disposed within the air inlet compartment and having a diffuser inlet, a diffuser outlet, and a bypass port disposed between the diffuser inlet and the diffuser outlet, the diffuser inlet coupled to receive ram air from the ram air inlet opening, the diffuser outlet in fluid communication with, and configured to discharge ram air into, the air inlet compartment, the bypass port in fluid communication with the APU air inlet port;
a plurality of flow control surfaces rotationally mounted within the diffuser and movable between a first position, in which the flow control surfaces direct ram air through the bypass port and into the APU air inlet port, and a second position, in which the flow control surfaces direct ram air through the diffuser outlet;
an inlet particle separator (IPS) disposed within the air inlet compartment between the diffuser outlet and the APU air inlet port; and
an APU disposed within the APU compartment, the APU having an air inlet in fluid communication with the APU air inlet port.

Assignees

• Honeywell Int Inc

Inventors

• Sheoran Yogendra Yogi
• Bouldin Bruce Dan
• Alazraki Marcos
• Kowal Adam
• Robbins Rob
• Reich Jennifer Ann

Classifications

• B64D2033/0246

  comprising particle separators · CPC title

• B64D2041/002

  Mounting arrangements for auxiliary power units (APU's) · CPC title

• B64D41/00

  Power installations for auxiliary purposes · CPC title

• B64D33/00

  Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for · CPC title

• B64D2033/0213

  specially adapted for auxiliary power units (APU's) · CPC title