DRIVE SCREW ASSEMBLY AND LANDING GEAR ASSEMBLY WITH SAME

• US 20130299631A1
• Filed: 09/11/2012
• Published: 11/14/2013
• Est. Priority Date: 05/10/2012
• Status: Abandoned Application

• Current Assignee: Triumph Actuation Systems - UK, Ltd. (Triumph Group, Inc.)
• Original Assignee: GE Aviation Systems Limited (GE Aerospace)
• Inventors: Tucker, Miles
• Application Number:
  US13/609,860
• Publication Number:
  US 20130299631A1
• Time in Patent Office: Days
• US Class Current: 244/102.R
• CPC Class Codes: B64C 25/14 fore-and-aft
• CPC Class Codes: B64C 25/26 Control or locking systems therefor
• CPC Class Codes: Y10T 74/19702 Screw and nut

Abstract

A landing gear assembly includes a leg that may be rotated between retracted and extended positions, a link assembly, and a drive screw assembly. The drive screw assembly includes a casing, a piston slidably coupled to the casing for reciprocation relative to the casing and a portion mounted to the link assembly and where the drive screw assembly is capable of locking and unlocking.

Claims

1. A landing gear assembly for an aircraft comprising:

a leg having a first end rotatably coupled to the aircraft for rotating between retracted and extended positions;

a link assembly comprising multiple rotatably coupled links, with one of the links rotatably coupled to the aircraft and another of the links rotatably coupled to the leg; and

a drive screw assembly comprising;

a casing coupled to the aircraft and having an interior with an open end and having at least one detent;

a piston having at least a portion received within the interior and slidably coupled to the casing for reciprocation relative to the casing and another portion mounted to the link assembly;

a drive screw provided within the casing and extending into the piston;

a nut assembly threadably coupled on the drive screw and having at least one moveable segment receivable within the detent and a cam operably coupled to the at least one moveable segment to move the segment into the detent, and the cam having a key; and

a screw cap rotationally mounting an end of the drive screw proximate the open end and having a keyway for receiving the key;

wherein upon the rotation of the drive screw, the nut assembly traverses the drive screw where it contacts the piston to move the leg from the retracted position to the extended position and when the key engages the keyway, the cam moves the moveable segment into the detent, which locks the piston relative to the casing to fix the leg in the extended position.

2. The landing gear assembly of claim 1 wherein the nut assembly further comprises a biasing element biasing the cam axially along the drive screw toward the screw cap.

3. The landing gear assembly of claim 1 wherein the cam comprises a cam surface abutting an end of the moveable segment.

4. The landing gear assembly of claim 3 wherein the cam surface has an increasing radius such that rotation of the cam radially extends the moveable segment.

5. The landing gear assembly of claim 4 wherein the cam surface terminates in a stop that abuts the moveable segment after a predetermined amount of rotation.

6. The landing gear assembly of claim 1 wherein the detent and the moveable segment have complementary surfaces.

7. The landing gear assembly of claim 6 wherein the complementary surfaces are at an angle relative to a rotational axis of the drive screw.

8. The landing gear assembly of claim 1 wherein the key and the keyway have complementary chamfers preventing immediate locking of the key in the keyway upon initial contact between the key and the keyway.

9. The landing gear assembly of claim 8 wherein the nut assembly further comprises a biasing element biasing the cam axially along the drive screw toward the screw cap.

10. The landing gear assembly of claim 8 wherein the key and the keyway have complementary driving surfaces, which abut when the key is received within the keyway.

11. The landing gear assembly of claim 10 wherein the complementary driving surfaces are between 45 and 70 degrees.

12. A drive screw assembly comprising:

a casing having one end for coupling to a structure and having an interior with an open end and having at least one detent;

a piston having at least a portion received within the interior and slidably coupled to the casing for reciprocation relative to the casing and another portion for coupling to a moveable portion;

a drive screw provided within the casing and extending into the piston;

a nut assembly threadably coupled on the drive screw and having at least one moveable segment receivable within the detent and a cam operably coupled to the at least one moveable segment to move the at least one moveable segment into the detent, and the cam having a key; and

a screw cap rotationally mounting an end of the drive screw proximate the open end and having a keyway for receiving the key;

wherein upon rotation of the drive screw, the nut assembly traverses the drive screw to move the piston out of the casing ultimately causing the key to engage the keyway, which causes the cam to move the moveable segment into the detent, which locks the piston relative to the casing.

13. The drive screw assembly of claim 12 wherein the cam comprises a cam surface abutting an end of the moveable segment.

14. The drive screw assembly of claim 13 wherein the cam surface has an increasing radius such that rotation of the cam radially extends the moveable segment.

15. The drive screw assembly of claim 14 wherein the cam surface terminates in a stop that abuts the moveable segment after a predetermined amount of rotation.

16. The drive screw assembly of claim 12 wherein the detent and the moveable segment have complementary surfaces.

17. The drive screw assembly of claim 12 wherein the key and the keyway have complementary chamfers preventing immediate locking of the key in the keyway upon initial contact between the key and the keyway.

18. The drive screw assembly of claim 17 wherein the nut assembly further comprises a biasing element biasing the cam axially along the drive screw toward the screw cap.

19. The drive screw assembly of claim 17 wherein the key and the keyway have complementary driving surfaces, which abut when the key is received within the keyway.

20. The drive screw assembly of claim 19 wherein the complementary surfaces are between 45 and 70 degrees.