IP Library Granted Patent US 11,661,178
Granted Patent B2
US 11,661,178 · App. 17/336,185 · Granted May 30, 2023

Tail rotor gearbox support assemblies for helicopters

Inventors: James Everett Kooiman (Fort Worth, TX); Jeffrey Matthew Williams (Hudson Oaks, TX); Clegg Benjamin Brian Smith (Keller, TX); Michael Edwin Rinehart (Euless, TX)
Assignee: Textron Innovations Inc.
B64C27/82B64C2027/8254B64C2027/8272
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Quick Facts
Patent No.
US 11,661,178
App. No.
17/336,185
Granted
May 30, 2023
Kind
B2
Abstract

A tail rotor assembly coupled to a tailboom of a helicopter includes a tail rotor gearbox having top, bottom and aft sides and a shroud surrounding the tail rotor gearbox. The shroud includes a shroud airframe having top and bottom portions. The tail rotor assembly includes a tail rotor gearbox support assembly configured to support the tail rotor gearbox within the shroud. The tail rotor gearbox support assembly includes a support column coupling the aft side of the tail rotor gearbox between the top and bottom portions of the shroud airframe, an upper support crossbar coupling the top side of the tail rotor gearbox between the support column and the tailboom airframe and a lower support crossbar coupling the bottom side of the tail rotor gearbox between the support column and the tailboom airframe.

Claims (42)

1. A tail rotor assembly configured to be coupled to a tailboom of a helicopter, the tailboom having an aft end and a tailboom airframe, the tail rotor assembly comprising:

a tail rotor gearbox having top, bottom and aft sides;

a shroud including a shroud airframe having top and bottom portions configured to be coupled to the aft end of the tailboom, the shroud surrounding the tail rotor gearbox; and

a tail rotor gearbox support assembly configured to support the tail rotor gearbox within the shroud, the tail rotor gearbox support assembly comprising:

a support column coupled to the aft side of the tail rotor gearbox, the support column having a top end coupled to the top portion of the shroud airframe and a bottom end coupled to the bottom portion of the shroud airframe;

a substantially horizontal upper support crossbar coupled to the top side of the tail rotor gearbox, the upper support crossbar having a forward end configured to be coupled to the tailboom airframe and an aft end coupled to the support column; and

a substantially horizontal lower support crossbar coupled to the bottom side of the tail rotor gearbox, the lower support crossbar having a forward end configured to be coupled to the tailboom airframe and an aft end coupled to the support column;

wherein, the aft side of the tail rotor gearbox is coupled to a middle portion of the support column.

2. The tail rotor assembly as recited in claim 1 wherein each of the upper and lower support crossbars is perpendicular to the support column.

3. The tail rotor assembly as recited in claim 1 wherein each of the upper and lower support crossbars is nonperpendicular to the support column.

4. The tail rotor assembly as recited in claim 1 wherein the upper and lower support crossbars are substantially parallel.

5. The tail rotor assembly as recited in claim 1 wherein the support column is nonvertical.

6. The tail rotor assembly as recited in claim 1 wherein the support column is a tubular support column; and

wherein, the upper and lower support crossbars are tubular support crossbars.

7. The tail rotor assembly as recited in claim 1 wherein the tail rotor gearbox experiences torque and thrust loads during tail rotor operation and wherein the tail rotor gearbox support assembly transfers the torque and thrust loads to the tailboom.

8. The tail rotor assembly as recited in claim 1 wherein the tail rotor gearbox support assembly further comprises first and second tee connectors, the first tee connector coupling the aft end of the upper support crossbar to the support column and the second tee connector coupling the aft end of the lower support crossbar to the support column.

9. The tail rotor assembly as recited in claim 1 wherein the tail rotor gearbox support assembly further comprises:

a column pin joint assembly coupling the support column to the aft side of the tail rotor gearbox;

an upper crossbar pin joint assembly coupling the upper support crossbar to the top side of the tail rotor gearbox; and

a lower crossbar pin joint assembly coupling the lower support crossbar to the bottom side of the tail rotor gearbox.

10. A tail rotor assembly configured to be coupled to a tailboom of a helicopter, the tailboom having an aft end and a tailboom airframe, the tail rotor assembly comprising:

a tail rotor gearbox having top, bottom and aft sides;

a shroud including a shroud airframe having top and bottom portions configured to be coupled to the aft end of the tailboom, the shroud surrounding the tail rotor gearbox; and

a tail rotor gearbox support assembly configured to support the tail rotor gearbox within the shroud, the tail rotor gearbox support assembly comprising:

a support column coupled to the aft side of the tail rotor gearbox, the support column having a top end coupled to the top portion of the shroud airframe and a bottom end coupled to the bottom portion of the shroud airframe;

an upper support crossbar coupled to the top side of the tail rotor gearbox, the upper support crossbar having a forward end configured to be coupled to the tailboom airframe and an aft end coupled to the support column; and

a lower support crossbar coupled to the bottom side of the tail rotor gearbox, the lower support crossbar having a forward end configured to be coupled to the tailboom airframe and an aft end coupled to the support column;

wherein, the upper and lower support crossbar are nonparallel with each other; and

wherein, the aft side of the tail rotor gearbox is coupled to a middle portion of the support column.

11. The tail rotor assembly as recited in claim 10 wherein the lower support crossbar is nonperpendicular to the support column.

12. The tail rotor assembly as recited in claim 10 wherein the upper support crossbar is nonperpendicular to the support column.

13. The tail rotor assembly as recited in claim 10 wherein each of the upper and lower support crossbars is nonperpendicular to the support column.

14. The tail rotor assembly as recited in claim 10 wherein the lower support crossbar is nonhorizontal.

15. The tail rotor assembly as recited in claim 10 wherein the upper support crossbar is nonhorizontal.

16. The tail rotor assembly as recited in claim 10 wherein each of the upper and lower support crossbars is nonhorizontal.

17. The tail rotor assembly as recited in claim 10 wherein the support column is nonvertical.

18. The tail rotor assembly as recited in claim 10 wherein the tail rotor gearbox experiences torque and thrust loads during tail rotor operation and wherein the tail rotor gearbox support assembly transfers the torque and thrust loads to the tailboom.

19. The tail rotor assembly as recited in claim 10 wherein the tail rotor gearbox support assembly further comprises first and second tee connectors, the first tee connector coupling the aft end of the upper support crossbar to the support column and the second tee connector coupling the aft end of the lower support crossbar to the support column.

20. The tail rotor assembly as recited in claim 10 wherein the tail rotor gearbox support assembly further comprises:

a column pin joint assembly coupling the support column to the aft side of the tail rotor gearbox;

an upper crossbar pin joint assembly coupling the upper support crossbar to the top side of the tail rotor gearbox; and

a lower crossbar pin joint assembly coupling the lower support crossbar to the bottom side of the tail rotor gearbox.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 9, 2021
From: BELL TEXTRON INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 056485/0861 →
CHANGE OF NAME Recorded Jun 3, 2021
From: BELL HELICOPTER TEXTRON INC.
To: BELL TEXTRON INC.
Reel/Frame 056467/0483 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 1, 2021
From: KOOIMAN, JAMES EVERETT; WILLIAMS, JEFFREY MATTHEW; SMITH, CLEGG BENJAMIN BRIAN; RINEHART, MICHAEL EDWIN
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 056406/0575 →
Continuity (2)
Continuation 16290797 · Mar 1, 2019
Related Publication 20210339852A1 · Nov 4, 2021