IP Library › Granted Patent US 10,502,161
Granted Patent B2
US 10,502,161 · App. 14/954,570 · Granted Dec 10, 2019

Cascade system and apparatus

Inventor: Sara C. Crawford (San Diego, CA)
Assignee: ROHR, INC.
F02K1/72F02K1/64F02K1/70F05D2250/37
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Quick Facts
Patent No.
US 10,502,161
App. No.
14/954,570
Granted
Dec 10, 2019
Kind
B2
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.

Claims (9)

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.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 30, 2015
From: CRAWFORD, SARA C.
To: ROHR, INC.
Reel/Frame 037169/0978 →
Continuity (3)
Continuation In Part PCTUS2015025418 · Apr 10, 2015
Provisional Application 61978616 · Apr 11, 2014
Related Publication 20160146156A1 · May 26, 2016