Passive particle separation system

Patent metadata

Field	Value
Publication number	US-10836504-B2
Application number	US-201815963911-A
Country	US
Kind code	B2
Filing date	Apr 26, 2018
Priority date	Apr 26, 2018
Publication date	Nov 17, 2020
Grant date	Nov 17, 2020

Abstract

One embodiment is a passive particle separation system including a plenum; an inlet for feeding outside air into the plenum, wherein the outside air has particles entrained therewith; a housing for enclosing the plenum; and a standpipe installed on the housing. The outside air enters the plenum via the inlet and plenum, housing, and standpipe interact to impact the outside air entering the plenum to cause the particles to be released from the outside air.

First claim

What is claimed is:

1. A rotorcraft comprising:
a first fairing; and
a passive particle separation system installed on the first fairing, the passive particle separation system comprising:
a plenum;
an inlet for feeding outside air into the plenum, wherein the outside air has particles entrained therewith;
a housing for enclosing the plenum; and
a standpipe installed on the housing;

wherein the outside air enters the plenum via the inlet; and
wherein the plenum, housing, and standpipe interact to impact the outside air entering the plenum to cause the particles to be released from the outside air;
wherein the plenum comprises an area adjacent the inlet that has a cross-sectional area greater than that of the inlet such that the outside air entering the inlet expends into a larger volume;
wherein the plenum is arranged such that the outside air must change direction as it flows from the are toward the standpipe;
wherein the housing comprises a cylindrical area around the standpipe arranged such that the outside air continues to flow into the cylindrical area where it encounters additional direction changes such that rotation is imparted to the outside air flow; and
wherein the first fairing is pivotably attached to a fixed fairing for articulation relative to the fixed fairing between a closed position and an open position.

2. The rotorcraft of claim 1 , wherein the passive particle separation system further comprises a filter through which the outside air is drawn into the standpipe.

3. The rotorcraft of claim 1 , wherein the passive particle separation system further comprises a trash trap disposed at the base of the housing around the standpipe for accumulating particles released from the outside air.

4. The rotorcraft of claim 1 wherein the standpipe is removable.

5. The rotorcraft of claim 1 , wherein the passive particle separation system further comprises a consumer system inlet duct through which the outside air from which particles have been separated exits the passive particle separation system.

6. The rotorcraft of claim 1 further comprising a drain disposed at a bottom of the plenum proximate the standpipe.

7. The rotorcraft of claim 1 further comprising a seal disposed at a base of the standpipe.

8. The rotorcraft of claim 1 , wherein the inlet comprises a National Advisory Council on Aeronautics (“NACA”) type flush low-pressure inlet.

9. A rotorcraft comprising:
a fairing assembly comprising:
a first fairing affixed to an airframe of the rotorcraft;
a second fairing hinged on the first fairing for articulation relative to the first fairing between a closed position and an open position;

a passive particle separation system installed on the first fairing, the passive particle separation system comprising:
a plenum;
an inlet for feeding outside air into the plenum, wherein the outside air has particles entrained therewith;
a housing for enclosing the plenum; and
a standpipe installed on the housing;

wherein the outside air enters the plenum via the inlet; and
wherein the plenum, housing, and standpipe interact to impact the outside air entering the plenum to cause the particles to be released from the outside air;
wherein the plenum comprises an area adjacent the inlet that has a cross-sectional area greater than that of the inlet such that the outside air entering the inlet expends into a larger volume;
wherein the plenum is arranged such that the outside air must change direction as it flows from the are toward the standpipe; and
wherein the housing comprises a cylindrical area around the standpipe arranged such that the outside air continues to flow into the cylindrical area where it encounters additional direction changes such that rotation is imparted to the outside air flow.

10. The rotorcraft of claim 9 , wherein the passive particle separation system further comprises:
a filter through which the outside air is drawn into the standpipe; and
a trash trap disposed at the base of the housing around the standpipe for accumulating particles released from the outside air.

11. The rotorcraft of claim 9 , wherein the standpipe is removable.

12. The rotorcraft of claim 9 , wherein the passive particle separation system further comprises a consumer system inlet duct through which the outside air from which particles have been separated exits the passive particle separation system.

13. The rotorcraft of claim 9 , wherein the passive particle separation system further comprises a drain disposed at a bottom of the plenum proximate the standpipe.

14. The rotorcraft of claim 9 , wherein the passive particle separation system further comprises a seal disposed at a base of the standpipe.

15. The rotorcraft of claim 9 , wherein the inlet comprises a National Advisory Council on Aeronautics (“NACA”) type flush low-pressure inlet.

Assignees

• Bell Helicopter Textron Inc
• Textron Innovations Inc

Inventors

• Edler Joshua Allan
• Scannell Brent
• Mast Thomas
• Villanueva Sarah R
• Tiedeman David Michael
• Pedersen Keith C

Classifications

• B64C27/06

  with single rotor · CPC title

• B64D2013/0651

  comprising filters, e.g. dust filters · CPC title

• B64D2033/0246

  comprising particle separators · CPC title

• B60J5/108

  for load transporting vehicles or public transport, e.g. lorries, trucks, buses · CPC title

• B64C27/04

  Helicopters · CPC title