Retention systems for light weight actuator glands

Patent metadata

Field	Value
Publication number	US-11085465-B2
Application number	US-201916298928-A
Country	US
Kind code	B2
Filing date	Mar 11, 2019
Priority date	Mar 11, 2019
Publication date	Aug 10, 2021
Grant date	Aug 10, 2021

Abstract

Retention systems for retaining a gland is provided. A hydraulic actuator may comprise a cylinder closed at an end by a gland, wherein the gland comprises a gland body having a bearing flange disposed within an interior volume of the cylinder, a lock ring retainer disposed between the gland body and the cylinder and contacted with the bearing flange, and a lock ring coupled between the lock ring retainer and a lock ring channel of the cylinder.

First claim

What is claimed is:

1. A hydraulic actuator, comprising:
a cylinder closed at an end by a gland,
wherein the gland comprises a gland body having a bearing flange disposed within an interior volume of the cylinder;
a lock ring retainer disposed between the gland body and the cylinder and contacted with the bearing flange;
a lock ring coupled between the lock ring retainer and a lock ring channel of the cylinder; and
a spacer disposed between the gland body and the cylinder, the spacer in contact with the lock ring.

2. The hydraulic actuator of claim 1 , further comprising a piston disposed within the interior volume of the cylinder and coupled to a piston rod,
wherein the gland body comprise an annular cylindrical structure, wherein the piston rod extends from a piston end of the gland body through an annulus of the gland body out a rod end of the gland body.

3. The hydraulic actuator of claim 2 , wherein the piston rod is supported by a piston bearing fitted into the annulus of the gland body.

4. The hydraulic actuator of claim 3 , wherein the gland body comprises one of aluminum, aluminum alloy, titanium, titanium alloy, lithium alloy, magnesium alloy, composite material, or plastic.

5. The hydraulic actuator of claim 1 , wherein the cylinder comprises composite material.

6. The hydraulic actuator of claim 1 , wherein the gland body further comprises a supply port, wherein the spacer is fixed from translating axially with respect to the gland body by an interference between the spacer and the supply port or between the spacer and a supply port fitting disposed within the supply port.

7. The hydraulic actuator of claim 1 , wherein the lock ring retainer comprises one of nickel, nickel alloy, bronze, bronze alloy, aluminum, aluminum alloy, aluminum-nickel-bronze alloy, or bearing metal.

8. The hydraulic actuator of claim 1 , wherein each of the lock ring, the lock ring retainer, and the spacer comprise two or more arcuate segments.

9. A landing gear system, comprising:
a shock strut coupled to an axle;
a wheel coupled to the axle; and
a hydraulic actuator coupled to the shock strut comprising:
a cylinder closed at an end by a gland,
wherein the gland comprises a gland body having a bearing flange disposed within an interior volume of the cylinder;
a lock ring retainer disposed between the gland body and the cylinder and contacted with the bearing flange;
a lock ring coupled between the lock ring retainer and a lock ring channel of the cylinder; and
a spacer disposed between the gland body and the cylinder, the spacer in contact with the lock ring.

10. The landing gear system of claim 9 , further comprising a piston disposed within the interior volume of the cylinder and coupled to a piston rod,
wherein the gland body comprise an annular cylindrical structure, wherein the piston rod extends from a piston end of the gland body through an annulus of the gland body out a rod end of the gland body.

11. The landing gear system of claim 10 , wherein the piston rod is supported by a piston bearing fitted into the annulus of the gland body.

12. The landing gear system of claim 11 , wherein the gland body comprises one of aluminum, aluminum alloy, titanium, titanium alloy, lithium alloy, magnesium alloy, composite material, or plastic.

13. The landing gear system of claim 9 , wherein the cylinder comprises composite material.

14. The landing gear system of claim 9 , further comprising a spacer disposed between the gland body and the cylinder and contacted with the lock ring.

15. The landing gear system of claim 14 , wherein the gland body further comprises a supply port, wherein the spacer is fixed from translating axially with respect to the gland body by an interference between the spacer and the supply port or between the spacer and a supply port fitting disposed within the supply port.

16. The landing gear system of claim 9 , wherein the lock ring retainer comprises one of nickel, nickel alloy, bronze, bronze alloy, aluminum, aluminum alloy, aluminum-nickel-bronze alloy, or bearing metal.

17. The landing gear system of claim 14 , wherein each of the lock ring, the lock ring retainer, and the spacer comprise two or more arcuate segments.

18. A method of retaining a gland, comprising:
inserting a piston end of a gland body of the gland into a cylinder and further inserting a bearing flange of the gland body beyond a lock ring channel of the cylinder;
inserting a lock ring retainer between the gland body and the cylinder and beyond the lock ring channel into contact with the bearing flange;
inserting a lock ring between the gland body and the cylinder and beyond the lock ring channel to contact the lock ring retainer;
partially withdrawing the piston end of the gland from the cylinder and, in response, seating the lock ring in the lock ring channel; and
inserting a spacer disposed between the gland body and the cylinder into contact with the lock ring.

Assignees

• Goodrich Corp

Inventors

• Goldring Eric
• Ganis Rony Giovanni

Classifications

• B64C25/62

  Spring shock-absorbers; Springs · CPC title

• F15B15/1428

  Cylinders (F15B15/1438 takes precedence) · CPC title

• F15B15/1442

  End cap sealings · CPC title

• F15B15/1438 Primary

  Cylinder to end cap assemblies · CPC title

• F15B2215/305

  characterised by the use of special materials · CPC title