IP Library Granted Patent US 11,459,979
Granted Patent B2
US 11,459,979 · App. 17/165,433 · Granted Oct 4, 2022

Textile cascade assembly

Inventor: Randall Ray West (Wichita, KS)
Assignee: SPIRIT AEROSYSTEMS, INC.
F02K1/72F05D2240/129F05D2300/601
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Quick Facts
Patent No.
US 11,459,979
App. No.
17/165,433
Granted
Oct 4, 2022
Kind
B2
Abstract

A cascade assembly for a thrust reverser of an aircraft engine. The cascade broadly comprises a number of vanes formed of a pliable material and shiftable between a collapsed position when the thrust reverser is in a stowed configuration and a distended position when the thrust reverser is in a deployed configuration to redirect fan duct flow in a reverse thrust flow opening created by the thrust reverser.

Claims (19)

1. A cascade assembly for a thrust reverser, the cascade assembly comprising:

a plurality of pliable textile vanes including a plurality of longitudinal panels and a plurality of lateral panels cooperatively forming a plurality of channels, the plurality of pliable textile vanes being shiftable between a collapsed position when the thrust reverser is in a stowed configuration and a distended position when the thrust reverser is in a deployed configuration to redirect fan duct flow,

the plurality of longitudinal panels and the plurality of lateral panels being configured to pliably distend via the fan duct flow passing through the plurality of channels when the thrust reverser is actuated from the stowed configuration to the deployed configuration so that the plurality of lateral panels achieve a fan duct flow redirecting curvature in transitioning to the distended position and pliably collapse when the thrust reverser is actuated from the deployed configuration to the stowed configuration so that the plurality of lateral panels lose the fan duct flow redirecting curvature in transitioning to the collapsed position,

the plurality of pliable textile vanes having at least two different depths when the plurality of pliable textile vanes are in the distended position.

2. The cascade assembly of claim 1 , the pliable textile vanes being made of ripstop material.

3. The cascade assembly of claim 1 , the cascade assembly further comprising a plurality of battens configured to reinforce a shape of the plurality of pliable textile vanes when the plurality of pliable textile vanes are distended.

4. The cascade assembly of claim 1 , the plurality of pliable textile vanes including directional reinforcement stitching.

5. The cascade assembly of claim 1 , the plurality of pliable textile vanes including semi-rigid or rigid portions.

6. A cascade assembly for a thrust reverser, the cascade assembly comprising:

a plurality of pliable textile vanes including a plurality of longitudinal panels and a plurality of lateral panels cooperatively forming a plurality of channels, the plurality of pliable textile vanes being shiftable between a collapsed position when the thrust reverser is in a stowed configuration and a distended position when the thrust reverser is in a deployed configuration to redirect fan duct flow,

the plurality of longitudinal panels and the plurality of lateral panels being configured to pliably distend via the fan duct flow passing through the plurality of channels when the thrust reverser is actuated from the stowed configuration to the deployed configuration so that the plurality of lateral panels achieve a fan duct flow redirecting curvature in transitioning to the distended position and pliably collapse when the thrust reverser is actuated from the deployed configuration to the stowed configuration so that the plurality of lateral panels lose the fan duct flow redirecting curvature in transitioning to the collapsed position,

the plurality of pliable textile vanes having at least two different depths when the plurality of pliable textile vanes are in the distended position and a maximum collapsed depth smaller than the at least two different depths when the plurality of pliable textile vanes are in the collapsed position.

7. A cascade assembly for a thrust reverser including a forward structure and a sleeve having an open-ended chamber, the cascade assembly comprising:

a plurality of pliable textile vanes including a plurality of substantially straight longitudinal panels and a plurality of lateral panels cooperatively forming a plurality of channels, the plurality of pliable textile vanes being shiftable between a collapsed position when the thrust reverser is in a stowed configuration and a distended position when the thrust reverser is in a deployed configuration to redirect fan duct flow,

the plurality of longitudinal panels and the plurality of lateral panels being configured to pliably distend via the fan duct flow passing through the plurality of channels when the thrust reverser is actuated from the stowed configuration to the deployed configuration so that the plurality of lateral panels achieve a fan duct flow redirecting curvature in transitioning to the distended position and pliably collapse when the thrust reverser is actuated from the deployed configuration to the stowed configuration so that the plurality of lateral panels lose the fan duct flow redirecting curvature in transitioning to the collapsed position,

the plurality of pliable textile vanes having at least two different depths when the plurality of pliable textile vanes are in the distended position and a maximum collapsed depth smaller than the at least two different depths when the plurality of pliable textile vanes are in the collapsed position;

a forward connection point configured to connect the plurality of pliable textile vanes to the forward structure;

a rear support member configured to be positioned in the open-ended chamber; and

an aft connection point opposite the forward connection point and configured to connect the plurality of pliable textile vanes to the rear support member.

Assignments (9)
RELEASE OF SECURITY INTEREST Recorded Dec 9, 2025
From: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073916/0346 →
RELEASE OF SECURITY INTEREST Recorded Dec 9, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073900/0653 →
SECURITY AGREEMENT Recorded Jul 8, 2024
From: SPIRIT AEROSYSTEMS, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC.
Reel/Frame 068217/0456 →
RELEASE OF SECURITY INTEREST Recorded Dec 4, 2023
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
To: SPIRIT AEROSYSTEMS, INC.; SPIRIT AEROSYSTEMS HOLDINGS, INC.; SPIRIT AEROSYSTEMS NORTH CAROLINA, INC.
Reel/Frame 065757/0004 →
SECURITY AGREEMENT (SECOND LIEN NOTES) Recorded Nov 21, 2023
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
Reel/Frame 065659/0585 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Nov 23, 2022
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 061993/0847 →
SECURITY INTEREST Recorded Nov 23, 2022
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
Reel/Frame 061869/0241 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Nov 23, 2022
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 061993/0236 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 2, 2021
From: WEST, RANDALL RAY
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 055115/0844 →
Continuity (1)
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