Thrust reversers and methods to provide reverse thrust

Patent metadata

Field	Value
Publication number	US-9670875-B2
Application number	US-201213665596-A
Country	US
Kind code	B2
Filing date	Oct 31, 2012
Priority date	Oct 31, 2012
Publication date	Jun 6, 2017
Grant date	Jun 6, 2017

Abstract

Thrust reversers and methods to provide reverse thrust are disclosed. An example thrust reverser includes a cascade to direct air from an interior volume of an engine nacelle to generate reverse thrust with respect to a direction of travel, and an air extractor to extract a portion of air approaching the cascade from within the interior volume.

First claim

What is claimed is:

1. A thrust reverser, comprising:
a cascade to direct air from an interior volume of an engine nacelle to generate reverse thrust with respect to a direction of travel;
an air extractor to extract a portion of air approaching the cascade from within the interior volume; and
an air ejector to eject the portion of the air to a location on an exterior surface of the engine nacelle, the location being on an exterior of the engine and forward of the cascade in the direction of travel.

2. A thrust reverser as defined in claim 1 , wherein the thrust reverser further comprises a diverter fairing, the air extractor to extract the portion of the air from a volume adjacent the diverter fairing.

3. A thrust reverser as defined in claim 1 , wherein the cascade comprises a plurality of vanes to direct the air to generate the reverse thrust.

4. A thrust reverser as defined in claim 1 , wherein the air extractor comprises a pump.

5. A thrust reverser as defined in claim 4 , wherein the air ejector comprises a pump.

6. A thrust reverser as defined in claim 1 , wherein the air ejector comprises a pump.

7. A thrust reverser as defined in claim 1 , wherein the air ejector is to increase an air pressure of the portion of the air extracted by the air extractor to eject the air from the location at an ejection speed to overcome external air pressure.

8. A thrust reverser for an engine, comprising:
a cascade;
an air extractor to extract a portion of an air intake flow approaching the cascade; and
an air ejector to eject the portion of the air intake flow to a location on an exterior surface of an engine nacelle of the engine, the location being on an exterior of the engine including the cascade and forward of the cascade in a direction of travel of the engine.

9. A thrust reverser as defined in claim 8 , wherein the air extractor comprises a pump and the air ejector comprises another pump.

10. A thrust reverser as defined in claim 8 , wherein the air ejector is to increase an air pressure of the portion of the air extracted by the air extractor to eject the air from the location at an ejection speed to overcome external air pressure.

11. A method, comprising:
exposing a thrust reverser to generate reverse thrust by directing air from an interior volume of an engine nacelle of an engine through the thrust reverser;
extracting a portion of the air approaching the thrust reverser from the interior volume; and
ejecting the portion of the air to a location on an exterior surface of the engine nacelle of the engine, the location being on an exterior of the engine and forward of the thrust reverser in a direction of travel of the engine.

12. A method as defined in claim 11 , wherein extracting the portion of the air comprises extracting the portion of the air from a volume adjacent a diverter fairing.

13. A method as defined in claim 11 , wherein the thrust reverser comprises a cascade type thrust reverser.

14. A method as defined in claim 11 , further comprising increasing an air pressure of the portion of the air to an increased air pressure, the ejecting of the portion of the air including ejecting the portion of the air at the increased air pressure.

15. An engine comprising:
a nacelle;
a thrust reverser to generate reverse thrust by directing air from an interior of the nacelle to an exterior of the nacelle;
an air extractor to extract a portion of air approaching the thrust reverser from within the interior of the nacelle; and
an air ejector to eject the portion of the air to a location on an exterior surface of the nacelle, the location being on the exterior of the engine and forward of the thrust reverser in a direction of travel of the engine.

16. An engine as defined in claim 15 , wherein the thrust reverser is a cascade type thrust reverser.

17. An engine as defined in claim 15 , wherein the air ejector is to increase an air pressure of the portion of the air extracted by the air extractor to eject the air from the location at an ejection speed to overcome external air pressure.

18. An engine as defined in claim 15 , wherein the air extractor comprises a pump and the air ejector comprises another pump.

Assignees

• Boeing Co

Inventors

• Acheson Kurt Erik
• Chuck Chen

Classifications

• F02K1/72 Primary

  the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow · CPC title

• F02K1/766

  with blocking systems or locking devices; Arrangement of locking devices for thrust reversers · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• Y02T50/671

  Cross-Sectional Technologies · mapped topic

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title