Thrust reversers and methods to provide reverse thrust

Patent metadata

Field	Value
Publication number	US-10590885-B2
Application number	US-201615350217-A
Country	US
Kind code	B2
Filing date	Nov 14, 2016
Priority date	Oct 31, 2012
Publication date	Mar 17, 2020
Grant date	Mar 17, 2020

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 for an engine comprising:
an air extractor pump to extract a portion of air from an interior portion of the engine, the air in the interior portion of the engine to generate reverse thrust with respect to a direction of travel of the engine; and
an air ejector pump, the air extractor pump and the air ejector pump defining (a) a first fluid flow path for the portion of the air, the portion of the air to be ejected from a location on an exterior surface of the engine via the first fluid flow path and (b) a second fluid flow path for the portion of the air, the portion of the air to be ejected via the second fluid flow path to a location in the interior portion of the engine different from a location in the interior portion in which the portion of the air was extracted.

2. The thrust reverser of claim 1 , wherein the interior portion of the engine includes a first door to direct the air to form the reverse thrust and wherein at least a portion of the exterior surface of the engine includes a second door to direct the reverse thrust in a forward direction relative to the direction of travel.

3. The thrust reverser of claim 2 , wherein the location on the exterior surface is forward of the second door relative to the direction of travel.

4. The thrust reverser of claim 2 , wherein the portion of the air to be ejected via the second fluid flow path is to be ejected behind the first door.

5. The thrust reverser of claim 1 , wherein the air ejector pump is to increase a pressure of the portion of the air extracted by the air extractor pump.

6. The thrust reverser of claim 1 , wherein the air extractor pump is disposed proximate to a diverter fairing of a nacelle of the engine.

7. The thrust reverser of claim 6 , the air extractor pump is to extract the portion of the air via an opening formed in the diverter fairing.

8. An engine comprising:
a thrust reverser to generate reverse thrust by directing air from an interior volume of the engine to an exterior of the engine;
first pumping means to extract a portion of the air from the interior volume; and
second pumping means to eject the portion of the air, the first pumping means and the second pumping means defining (a) a first fluid flow path for the portion of the air, the portion of the air to be ejected from the interior volume to a location on an exterior surface of the engine via the first fluid flow path and (b) a second fluid flow path for the portion of the air, the portion of the air to be ejected via the second fluid flow path to a location in the interior volume of the engine different from a location in the interior volume in which the portion of the air was extracted.

9. The engine of claim 8 , further including a diverter fairing, the first pumping means to extract the portion of the air via an opening formed in the diverter fairing.

10. The engine of claim 8 , wherein the thrust reverser further includes means for directing the reverse thrust relative to a direction of travel of the engine.

11. The engine of claim 10 , wherein the means for directing the reverse thrust includes a first door.

12. The engine of claim 11 , further including a second door disposed in the interior volume of the engine, wherein the portion of the air to be ejected via the second fluid flow path is to be ejected behind the second door.

13. The engine of claim 10 , wherein the means for directing the reverse thrust is disposed at the exterior surface of the engine.

14. The engine of claim 10 , wherein the location on the exterior surface of the engine is disposed ahead of the means for directing the reverse thrust relative to the direction of travel of the engine.

15. The engine of claim 8 , wherein the second pumping means is to increase a pressure of the portion of the air extracted by the first pumping means, the second pumping means to eject the portion of the air at an ejection speed to overcome external air pressure.

Assignees

• Boeing Co

Inventors

• Acheson Kurt Erik
• Chuck Chen

Classifications

• F02K1/766

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

• 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

• 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