Cascade system and apparatus

Patent metadata

Field	Value
Publication number	US-10502161-B2
Application number	US-201514954570-A
Country	US
Kind code	B2
Filing date	Nov 30, 2015
Priority date	Apr 11, 2014
Publication date	Dec 10, 2019
Grant date	Dec 10, 2019

Abstract

A thrust reverser system may comprise a cascade radially positioned about a centerline of an engine or a nacelle centerline. Various cascade features may be positioned at a constant radius from the centerline while other features vary according to station and/or circumferential position.

First claim

What is claimed is:

1. A thrust reverser system formed around an engine centerline, comprising:
a torque box;
an aft cascade ring disposed aft of the torque box;
a cascade having a first vane set and a second vane set,
the first vane set having a fore end connected to the torque box, an aft end disposed aft of the fore end at an axial position and a radial position with respect to the engine centerline, and a first axial length extending between the fore end and the aft end of the first vane set, the first vane set positioned at a constant radius from the engine centerline along the first axial length and
the second vane set having an aft end connected to the aft cascade ring, a fore end disposed at the axial position and the radial position of the aft end of the first vane set, and a second axial length extending between the fore end and the aft end of the second vane set, the second vane set positioned at a variable radius, from the engine centerline to a radially inward side of the second vane set, along the second axial length and varies about a circumferential position relative to the engine centerline, the variable radius decreasing in value from the fore end of the second vane set to the aft end of the second vane set.

2. The thrust reverser system of claim 1 , further comprising a translating sleeve comprising a non-uniform annularly shaped pocket, wherein the cascade is receivable within the non-uniform annularly shaped pocket in response to the translating sleeve assuming a stowed position.

3. The thrust reverser system of claim 1 , wherein the torque box has a substantially constant radius relative to the engine centerline.

4. The thrust reverser system of claim 1 , wherein the aft cascade ring has a variable radius relative to the engine centerline.

Assignees

• Rohr Inc

Inventors

• Crawford Sara C

Classifications

• F02K1/64

  Reversing fan flow · CPC title

• F02K1/70

  using thrust reverser flaps or doors mounted on the fan housing · CPC title

• F05D2250/37

  circumferential · 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