IP Library Granted Patent US 10,151,333
Granted Patent B2
US 10,151,333 · App. 14/767,556 · Granted Dec 11, 2018

Modular actuator with snubbing arrangement

Inventors: Marin Besliu (Mississauga, CA); Chris Bryant (Pickering, CA); Howard Smith (Niagara Falls, CA)
Assignee: Safran Landing Systems Canada Inc./ Safran Systèmes d'Atterrissage Canada Inc.
F15B15/222F15B15/1438F15B15/1447F15B15/1457F16F9/3242F16J1/12F16B3/04
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Quick Facts
Patent No.
US 10,151,333
App. No.
14/767,556
Granted
Dec 11, 2018
Kind
B2
Abstract

Described is a modular linear actuator for use in an aerospace application, comprising: a piston housing having a closed end and an open end; a piston rod slideable within an interior of the piston housing between an extended position and a compressed position, the piston rod having a first end proximal to the closed end of the piston housing and a second end distal to the closed end of the piston housing; an attachment mechanism for removably attaching a lug end to the closed end of the piston housing, the lug end for attaching the actuator to a first component; an attachment mechanism for removably attaching a rod end to the second end of the piston rod, the rod end for attaching the piston rod to a second component; and, a piston head removably attached to the first end of the piston rod, the piston head for providing a snubbing engagement with the closed end of the piston housing.

Claims (22)

1. A modular linear actuator, comprising:

a piston housing having a closed end and an open end, the open end including a gland having a passageway to an interior of the piston housing;

a piston rod slideable within the interior of the piston housing between an extended position and a compressed position, the piston rod having a first end oriented towards the closed end of the piston housing and a second end oriented away from the closed end of the piston housing;

a retention wire removably attaching a lug end to the closed end of the piston housing, the lug end defining a cavity fluidly connected to a flow passage extending out of the lug end and engaging the gland passageway; and

a piston head removably attached to the first end of the piston rod using a piston retention wire, the piston head comprising a spear configured to slidably and sealably engage the cavity, the spear having an axial channel and a transverse passage that fluidly connects the axial channel with the interior of the piston housing, wherein the piston head is configured to provide a snubbing engagement with the lug end;

wherein the piston head and the closed end of the piston housing define a first chamber for holding hydraulic fluid therebetween and the piston head and the open end of the piston housing define a second chamber for holding hydraulic fluid therebetween, the piston head comprises a flow control device in the axial channel of the spear to provide the snubbing engagement with the lug end by controlling the rate of flow of hydraulic fluid from the first chamber to control pressure in the first chamber relative to pressure in the second chamber.

2. The modular linear actuator of claim 1 , wherein a first circumferential notch on an inner surface of the lug end aligns with a second circumferential notch on an outer surface of the closed end of the piston housing to receive the retention wire.

3. The modular linear actuator of claim 2 , wherein the lug end defines a tangential slot connecting an outer surface of the lug end to the first circumferential notch of the lug end, the tangential slot for inserting and removing the retention wire to attach or detach the lug end to the closed end of the piston housing.

4. The modular linear actuator of claim 3 , wherein the retention wire further comprises a hook to latch onto the outer surface of the closed end of the piston housing.

5. The modular linear actuator of claim 1 , wherein the lug end is removably attached to the piston housing using a second retention wire.

6. The modular linear actuator of claim 5 wherein the second retention wire either: is shaped as a helix to provide an axial force in the direction of the longitudinal axis of the piston rod for compensating for free play between the piston rod and the piston head; or comprises at least one wave for providing a force between the piston rod and the piston head for compensating for free play between the piston rod and the piston head.

7. The modular linear actuator of claim 1 wherein the retention wire either: is shaped as a helix to provide an axial force in the direction of the longitudinal axis of the piston housing for compensating for free play between the piston housing and the lug end; or comprises at least one wave for providing a force between the lug end and the piston housing for compensating for free play between the lug end and the piston housing.

8. The module linear actuator of claim 1 , wherein the spear further comprises a contact seal that dynamically re-engages the cavity.

9. The modular linear actuator of claim 8 wherein the spear is attached to the piston head using a retention plate.

10. The modular linear actuator of claim 1 wherein the gland is removably attached to the open end of the piston housing, the gland defining a gland cavity opening into the second chamber, the piston head further comprising a piston head extension that sealingly engages the gland cavity in the extended position, the gland further comprising a second flow control device coupled to the gland cavity to provide the snubbing engagement in the extended position by controlling the rate of flow of hydraulic fluid from the gland cavity.

11. The modular linear actuator of claim 10 , wherein the piston head extension further comprises a contact seal that dynamically re-engages the gland cavity.

12. The modular linear actuator of claim 10 further comprising a hydraulic fitting attached near the open end of the piston housing and coupled to the gland cavity.

13. The modular linear actuator of claim 10 wherein the gland is removably attached to the open end of the piston housing by a second retention wire.

14. The modular linear actuator according to claim 1 , wherein the retention wire comprises an elongate flexible wire having two free ends, the elongate flexible wire forming a substantially circular shape in a first plane and comprising one or more waves spaced along the elongate flexible wire, the waves extending in a second plane.

15. The retention wire of claim 14 , wherein the one or more waves form a sinusoidal pattern along the wire.

16. The retention wire of claim 14 , wherein the free ends are offset from each other.

17. The retention wire of claim 14 , wherein the waves form a helical pattern in the second plane.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 7, 2017
From: BESLIU, MARIN; BRYANT, CHRIS; SMITH, HOWARD
To: MESSIER-DOWTY INC.
Reel/Frame 043776/0993 →
CHANGE OF NAME Recorded Aug 25, 2016
From: MESSIER-DOWTY INC.
To: SAFRAN LANDING SYSTEMS CANADA INC./SAFRAN SYSTEMES D'ATTERRISSAGE CANADA INC.
Reel/Frame 039810/0027 →
Continuity (2)
Provisional Application 61764292 · Feb 13, 2013
Related Publication 20150377262A1 · Dec 31, 2015
Cited By (2)
US 12,276,289 US 12,534,878