IP Library Granted Patent US 10,865,736
Granted Patent B2
US 10,865,736 · App. 16/156,547 · Granted Dec 15, 2020

Cascade segment for thrust reverser with repeating modular units, and method of manufacturing same

Inventors: Mark Anthony Wadsworth (Sedan, KS); Alexander Jon Carr (Wichita, KS)
Assignee: Spirit AeroSystems, Inc.
F02K1/64F01D25/28F01D25/285F02K1/72F05D2230/60F05D2240/129
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Quick Facts
Patent No.
US 10,865,736
App. No.
16/156,547
Granted
Dec 15, 2020
Kind
B2
Abstract

A cascade segment for a thrust reverser, and a method of manufacturing it. The segment includes individual vane elements, modular units, and a frame. Each element includes a vane and two flanges arranged in a generally “U” shape. Each flange diverges from being perpendicular to the vane by an amount equal to a thickness of the flange over a desired spacing distance, such that when one element is inserted into another the desired spacing distance is established between their respective vanes. The units include first modular units, each of which includes a first column of the elements oriented in a first direction, and second modular units, each of which includes a second column of the elements oriented in a second direction. In the assembled segment, the first units are positioned adjacent to and alternating with the second units. The frame extends at least partly around and secures the units.

Claims (50)

1. A cascade segment, the cascade segment comprising: a plurality of individual vane elements, with each individual vane element of the plurality of individual vane elements including—

a vane having a first vane end and a second vane end,

a first flange extending angularly from the first vane end to a first flange end, and

a second flange extending angularly from the second vane end to a second flange end in approximately the same direction as the first flange, such that the individual vane element is generally U-shaped,

wherein each of the first and the second flanges diverge from being perpendicular to the vane by an amount equal to a thickness of the respective first or the respective second flange over a desired vane spacing distance, such that when one of the individual vane elements is inserted into another of the individual vane elements the desired vane spacing distance is established between their respective vanes;

a first modular unit including a first column of the individual vane elements oriented in a first direction; and

a second modular unit including a second column of the individual vane elements oriented in a second direction which is opposite the first direction,

wherein the first modular unit is positioned adjacent to the second modular unit in the cascade segment.

2. The cascade segment of claim 1 , wherein each vane of the first modular unit has a concave cross-section, and each vane of the second modular unit has a convex cross-section.

3. The cascade segment of claim 1 , wherein the first and the second flanges have flat cross-sections.

4. The cascade segment of claim 1 , wherein the first and the second flanges have curved cross-sections.

5. The cascade segment of claim 1 , wherein the first flange ends of the individual vane elements of the first modular unit abut the second flange ends of the individual vane elements of the second modular unit.

6. The cascade segment of claim 1 , wherein the first and the second flange ends are tapered, and the first flange ends of the individual vane elements of the first modular unit form scarf joints with the second flange ends of the individual vane elements of the second modular unit.

7. The cascade segment of claim 1 , wherein the individual vane elements are constructed of a thermoplastic material.

8. The cascade segment of claim 1 , wherein the first modular unit is one of a plurality of first modular units;

wherein the second modular unit is one of a plurality of second modular units,

wherein the first modular units are positioned adjacent to and alternating with the second modular units in the cascade segment; and

a frame extending at least partly around and securing the pluralities of the first and the second modular units together.

9. A cascade segment for a thrust reverser, the cascade segment comprising: a plurality of individual vane elements, with each individual vane element of the plurality of individual vane elements including—

a vane having a first vane end and a second vane end,

a first flange extending angularly from the first vane end to a first flange end, and

a second flange extending angularly from the second vane end to a second flange end in approximately the same direction as the first flange, such that the individual vane element is generally U-shaped,

wherein each of the first and the second flanges diverge from being perpendicular to the vane by an amount equal to a thickness of the respective first or the respective second flange over a desired vane spacing distance, such that when one of the individual vane elements is inserted into another of the individual vane elements the desired vane spacing distance is established between their respective vanes;

a plurality of first modular units, with each first modular unit including a first column of the individual vane elements oriented in a first direction, with each of the vanes having a concave cross-section;

a plurality of second modular units, with each second modular unit including a second column of the individual vane elements oriented in a second direction which is opposite the first direction, with each of the vanes having a convex cross-section;

wherein the first modular units are positioned alternatingly with and adjacent to the second modular units in the cascade segment; and

a frame extending at least partly around and securing the pluralities of the first and the second modular units together.

10. The cascade segment of claim 9 , wherein the first flange ends of the individual vane elements of the first modular units abut the second flange ends of the individual vane elements the second modular units.

11. The cascade segment of claim 9 , wherein the first and the second flange ends are tapered, and the first flange ends of the individual vane elements of the first modular units form scarf joints with the second flange ends of the individual vane elements of the second modular units.

12. The cascade segment of claim 9 , wherein the individual vane elements are constructed of a thermoplastic material.

13. A method of manufacturing a cascade segment, the method comprising: forming a plurality of individual vane elements, with each individual vane element of the plurality of individual vane elements including—

a vane having a first vane end and a second vane end,

a first flange extending angularly from the first vane end to a first flange end, and

a second flange extending angularly from the second vane end to a second flange end in approximately the same direction as the first flange, such that the individual vane element is generally U-shaped,

wherein each of the first and the second flanges diverge from being perpendicular to the vane by an amount equal to a thickness of the respective first or the respective second flange over a desired vane spacing distance, such that when one of the individual vane elements is inserted into another of the individual vane elements the desired vane spacing distance is established between their respective vanes;

assembling the plurality of individual vane elements to form—

a first modular unit including a first column of the individual vane elements oriented in a first direction, and

a second modular unit including a second column of the individual vane elements oriented in a second direction which is opposite the first direction; and

positioning the first modular unit adjacent to the second modular unit in the cascade segment.

14. The method of claim 13 , wherein each vane of the first modular unit has a concave cross-section, and each vane of the second modular unit has a convex cross-section.

15. The method of claim 13 , wherein the first and the second flanges have flat cross-sections.

16. The method of claim 13 , wherein the first and the second flanges have curved cross-sections.

17. The method of claim 13 , wherein the first flange ends of the individual vane elements of the first modular unit abut the second flange ends of the individual vane elements of the second modular unit.

18. The method of claim 13 , wherein the first and the second flange ends are tapered, and the first flange ends of the individual vane elements of the first modular unit form scarf joints with the second flange ends of the individual vane elements of the second modular unit.

19. The method of claim 13 , wherein the individual vane elements are constructed of a thermoplastic material.

20. The method of claim 13 , wherein the first modular unit is one of a plurality of first modular units and wherein the second modular unit is one of a plurality of second modular units, the method further including assembling the plurality of individual vane elements to form—

the plurality of the first modular units, and

the plurality of the second modular units;

positioning the first modular units alternatingly with and adjacent to the second modular units in the cascade segment; and

securing the pluralities of the first and the second modular units together with a frame extending at least partly around the pluralities of the first and the second modular units.

Assignments (15)
RELEASE OF SECURITY INTEREST Recorded Dec 11, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073932/0669 →
RELEASE OF SECURITY INTEREST Recorded Dec 10, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073900/0356 →
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 →
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 065772/0456 →
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 →
RELEASE OF SECURITY INTEREST Recorded Nov 23, 2022
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 061995/0281 →
RELEASE OF SECURITY INTEREST Recorded Oct 28, 2020
From: BANK OF AMERICA, N.A.
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 054230/0578 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 053993/0569 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 053993/0505 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 053983/0350 →
SECURITY INTEREST Recorded Apr 17, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 052433/0843 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Feb 24, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 052004/0929 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 10, 2018
From: WADSWORTH, MARK ANTHONY; CARR, ALEXANDER JON
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 047124/0472 →