Linear telescopic actuator

Patent metadata

Field	Value
Publication number	US-9976542-B2
Application number	US-201615245386-A
Country	US
Kind code	B2
Filing date	Aug 24, 2016
Priority date	Aug 27, 2015
Publication date	May 22, 2018
Grant date	May 22, 2018

Abstract

A linear telescopic actuator ( 1 ) that comprises a cylinder ( 2 ), a sliding part ( 3 ), a spring seat ( 4 ) and a first compression spring ( 5 ) capable of resiliently opposing the sliding part ( 3 ) approaching the spring seat ( 4 ). The spring seat ( 4 ) presents an outer annular groove ( 6 ) and the cylinder ( 2 ) includes an inner annular groove ( 7 ). The actuator ( 1 ) also presents a blocking part ( 8 ), the actuator ( 1 ) being adapted to adopt selectively an assembled configuration and a disassembled configuration. The blocking part ( 8 ) in the assembled configuration is engaged inside the inner and outer annular grooves ( 6, 7 ). The blocking part ( 8 ) in the disassembled configuration being disengaged from one of the grooves so as to allow spring seat ( 4 ) to slide in the cylinder ( 2 ).

First claim

The invention claimed is:

1. A linear telescopic actuator ( 1 ) comprising:
a cylinder ( 2 );
a sliding part ( 3 ) extending at least in part inside the cylinder ( 2 ) in order to slide therein along a sliding axis (X-X′);
a spring seat ( 4 ) that is arranged at least in part inside the cylinder ( 2 ); and
at least a first compression spring ( 5 ) arranged inside the cylinder ( 2 ) between said sliding part ( 3 ) and the spring seat ( 4 ) in order to be capable of resiliently opposing the sliding part ( 3 ) approaching the spring seat ( 4 ), the actuator being characterized in that:

the spring seat ( 4 ) presents an outer annular groove ( 6 ) and the cylinder ( 2 ) includes an inner annular groove ( 7 ), the actuator ( 1 ) further presenting a blocking part ( 8 ), the actuator ( 1 ) being adapted to adopt selectively an assembled configuration and a disassembled configuration, the blocking part ( 8 ) in the assembled configuration being engaged inside the inner and outer annular grooves ( 6 , 7 ) and forming an obstacle opposing sliding of the spring seat ( 4 ) relative to the cylinder ( 2 ), and the blocking part ( 8 ) in the disassembled configuration being disengaged from at least one of the inner and outer annular grooves ( 7 , 6 ) in order to allow the spring seat ( 4 ) to slide relative to the cylinder ( 2 ), the blocking part ( 8 ) and the inner and outer annular grooves ( 7 , 6 ) being adapted:
A) to allow the actuator to pass from its assembled configuration to its disassembled configuration when a first force (F 1 ) is exerted on the spring seat ( 4 ) along said sliding axis (X-X) in a first direction (S 1 ) going from the spring seat ( 4 ) towards the spring ( 5 ), this first force (F 1 ) presenting a first magnitude greater than a predetermined minimum threshold; and
B) to prevent the actuator from passing from its assembled configuration to its disassembled configuration:
when a force is exerted on the spring seat ( 4 ) in said first direction (S 1 ) with a magnitude less than or equal to the predetermined minimum threshold; or
when a force (F 2 ) is exerted on the spring seat ( 4 ) in a second direction (S 2 ) opposite to said first direction (S 1 ).

2. The actuator according to claim 1 , wherein the blocking part ( 8 ) is an open resilient ring adapted under the action of said first force (F 1 ) to disengage from the outer annular groove ( 6 ) of the spring seat by moving towards the inside of the inner annular groove ( 7 ) of the cylinder ( 2 ) in such a manner as to allow the spring seat ( 4 ) to move relative to said cylinder ( 2 ) in said first direction (S 1 ).

3. The actuator according to claim 2 , wherein the outer annular groove ( 6 ) of the spring seat ( 4 ) presents first and second shoulders ( 9 , 10 ) arranged to be on either side of the blocking part ( 8 ) when the actuator ( 1 ) is in the assembled configuration, the first shoulder ( 9 ) being arranged to oppose any movement of the spring seat ( 4 ) relative to the cylinder ( 2 ) in the first direction (S 1 ), and the second shoulder ( 10 ) being arranged to oppose any movement of the spring seat ( 4 ) relative to the cylinder ( 2 ) in the second direction (S 2 ), the outer annular groove ( 6 ) of the spring seat ( 4 ) presenting:
a first outer radius of length R 1 measured at its first shoulder; and
a minimum outer radius of length Rmin measured between the first and second shoulders ( 9 , 10 );
the inner annular groove ( 7 ) of the cylinder ( 2 ), the outer annular groove ( 6 ) of the spring seat ( 4 ), and the blocking part ( 8 ) being dimensioned so that then the actuator ( 1 ) is in the assembled configuration, the blocking part ( 8 ) is spaced apart from the bottom of the inner annular groove ( 7 ) of the cylinder by a distance Dx greater than the difference R 1 −Rmin.

4. The actuator according to claim 3 , wherein the blocking part ( 8 ) is in the form of an open ring that is circular in section when observed in a radial section plane, the circular section being uniform over a major portion of the length of the open ring and presenting a radius R 3 , the outer annular groove ( 6 ) of the spring seat ( 4 ) presenting a second outer radius of length R 2 measured at its second shoulder ( 10 ), the radius R 3 being less than or equal to the difference R 2 −Rmin.

5. The actuator according to claim 4 , wherein the blocking part ( 8 ) in the form of an open ring is resilient so as to exert a resilient force against the outer annular groove ( 6 ) of the spring seat ( 4 ) opposing any passage of the actuator ( 1 ) from its assembled configuration to its disassembled configuration.

6. The actuator according to claim 5 , wherein a first end of the spring seat ( 4 ) presents an annular chamfer ( 13 ) designed to guide the blocking part ( 8 ) in the form of an open ring around the spring seat ( 4 ) while said spring seat ( 4 ) is displaced so as to bring the blocking part ( 8 ) closer to the outer annular groove ( 6 ) of the spring seat ( 4 ) while the blocking part ( 8 ) is in contact with the annular chamfer ( 13 ).

7. The actuator according to claim 6 , wherein, said annular chamfer ( 13 ) and said blocking part ( 8 ) are designed so that the displacement of the spring seat ( 4 ) so as to bring the blocking part ( 8 ) closer to the outer annular groove ( 6 ) of the spring seat ( 4 ) can be achieved by applying an axial displacement force (F 0 ) on the spring seat ( 4 ) which is inferior to 200 Newton.

8. The actuator according to claim 6 , wherein a side of the annular grove ( 6 ) adjacent to the first annular chamfer ( 13 ) is formed by a second annular chamfer ( 14 ), said second annular chamfer ( 14 ) being designed to guide the blocking part ( 8 ) in the form of an open ring around the spring seat ( 4 ) while said spring seat ( 4 ) is displaced so as to move the blocking part ( 8 ) away from the outer annular groove ( 6 ) of the spring seat ( 4 ) while the blocking part ( 8 ) is in contact with said second annular chamfer ( 14 ).

9. The actuator according to claim 8 , wherein, said second annular chamfer ( 14 ) a said blocking part ( 8 ) are designed so that the displacement of the spring seat ( 4 ) so as to move the blocking part ( 8 ) away from the outer annular groove ( 6 ) of the spring seat ( 4 ) can be achieved by exerting said first force (F 1 ) on the spring seat ( 4 ) along said sliding axis (X-X) in a first direction (S 1 ).

10. An aircraft, characterized in that it includes an actuator according to claim 1 .

Assignees

• Safran Landing Systems Canada Inc

Inventors

• Ataman Gary

Classifications

• F15B15/1438

  Cylinder to end cap assemblies · CPC title

• F16F2226/041

  Clipping · CPC title

• F16F9/3242

  of cylinder ends, e.g. caps · CPC title

• F16F2226/044

  Snapping · CPC title

• F15B15/1442

  End cap sealings · CPC title