Electrical telescopic strut construction

Abstract

Electrical telescopic strut construction, movable between an extended locked position and a retracted unlocked position, comprising: an external cylinder (1); an inner cylinder (2); a screw (3) rotatable disposed within the inner cylinder (2); a drive (4) configured to rotate the screw (3); a nut (5) being movable with respect to the external cylinder (1) responsive to the rotation of the screw (3); at least one segment (6) located in a radial opening of the inner cylinder (2) and movable radially outward and inward in response to the movement of the nut (5) and configured to engage the external cylinder (1) when moved radially outward and not to engage the external cylinder (1) when moved radially inward, a second inner cylinder (7) located external to the first inner cylinder (2) and internal to the external cylinder (1).

Claims

1. An electrical telescopic strut construction, movable between an extended locked position and a retracted unlocked position, comprising: an external cylinder having a connection at an end; a first inner cylinder slidable within the external cylinder and having a second connection at an end; a screw rotatable disposed within the first inner cylinder; a drive configured to rotate the screw; a nut coupled to the screw and connected to the first inner cylinder, being movable with respect to the external cylinder responsive to the rotation of the screw; at least one segment located in a radial opening of the first inner cylinder and movable radially outward and inward in response to the movement of the nut and configured to engage the external cylinder when moved radially outward and not to engage the external cylinder when moved radially inward, the first inner cylinder being lockable to the external cylinder by the segment in an extended position of the strut, wherein the strut further comprises a second inner cylinder located external to the first inner cylinder and internal to the external cylinder when the first inner cylinder is retracted into the external cylinder, the second inner cylinder being joined to the first inner cylinder such that both cylinders are displaceable together and the second inner cylinder being in axial contact with the first inner cylinder.

2. The electrical telescopic strut construction according to claim 1, further comprising a mechanical element extending radially between the first inner cylinder and the second inner cylinder configured to avoid the axial and radial relative movement between both cylinders.

3. The electrical telescopic strut construction according to claim 2, wherein the mechanical element is a pin located in an opening of the first inner cylinder and in an opening of the second inner cylinder.

4. The electrical telescopic strut construction according to claim 1, further comprising a mechanical element extending between the first inner cylinder and the nut configured to avoid the radial relative movement between both elements.

5. The electrical telescopic strut construction according to claim 4, wherein the mechanical element is a pin located in an opening of the first inner cylinder and in an opening of the nut.

6. The electrical telescopic strut construction according to claim 5, wherein the opening of the nut is an axial opening such that there is an axial relative movement between the first inner cylinder and the nut.

7. The electrical telescopic strut construction according to claim 1, wherein the second inner cylinder has a pair of connections at its free end coaxial with the connection of the first inner cylinder.

8. The electrical telescopic strut construction according to claim 1, wherein the external cylinder has a pair of connections at its end coaxial with the connection of the external cylinder that are configured to be in axial contact with the external cylinder and to act in case of failure of the first connection.

9. The electrical telescopic strut construction according to claim 1, wherein the nut comprises a collar located around the nut comprising two surfaces of different external diameter, one leaving the segment in a lower position and therefore not engaging the external cylinder and a second cylindrical surface having a larger diameter and locating the segment engaging the external cylinder.

10. The electrical telescopic strut construction according to claim 9, wherein the sliding surfaces between segment and collar comprise both a zero or negative angle.

Description

DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 shows a sectional longitudinal plan view of the strut construction in a retracted, unlocked position according to a preferred embodiment of the invention.

(2) FIG. 2 shows a sectional longitudinal lateral view of the strut construction of FIG. 2.

(3) FIG. 3 shows a schematic plan view of the load path of an embodiment of the strut construction in an extended position.

(4) FIG. 4 shows a schematic plan view of the load path of an embodiment of the strut construction in an extended position in case of failure on the segment system.

(5) FIG. 5 shows a schematic plan view of the load path of an embodiment of the strut construction in an extended position in case of failure on the lug of the inner cylinder.

(6) FIG. 6 shows a schematic plan view of the load path of an embodiment of the strut construction in an extended position in case of failure on the lug of the external cylinder.

(7) FIG. 7 shows a schematic plan view of the load path of an embodiment of the strut construction in an extended position in case of failure of the inner cylinder.

(8) FIG. 8 shows a sectional longitudinal lateral view of the strut construction of FIG. 2 in a retracted position with compression load.

(9) FIG. 9 shows a sectional longitudinal lateral view of the strut construction of FIG. 2 in a travelling position with compression load.

(10) FIG. 10 shows a sectional longitudinal lateral view of the strut construction of FIG. 2 in a retracted position with traction load.

(11) FIG. 11 shows a sectional longitudinal lateral view of the strut construction of FIG. 2 in a travelling position with traction load.

(12) FIG. 12 shows a sectional longitudinal lateral view of the strut construction of FIG. 2 showing its position before locking the segments.

(13) FIG. 12B shows an enlarged view of FIG. 12.

(14) FIG. 13 shows a sectional longitudinal lateral view of the strut construction of FIG. 2 showing its position the segments locked.

(15) FIG. 13B shows an enlarged view of FIG. 13.

(16) FIG. 14 shows a sectional longitudinal lateral view of the strut construction of FIG. 2 showing the movement of the nut by the motor until it clash with the key.

(17) FIG. 14B shows an enlarged view of FIG. 14.

(18) FIG. 15 shows a sectional longitudinal lateral view of the strut construction of FIG. 2 showing its position with segments unlocked.

(19) FIG. 15B shows an enlarged view of FIG. 15.

(20) FIG. 16 shows a sectional longitudinal lateral view of the strut construction of FIG. 2 showing the beginning of the retraction after locking the segments.

(21) FIG. 16B shows an enlarged view of FIG. 16.

(22) FIG. 17 shows a sectional longitudinal lateral enlarged view of the strut construction of FIG. 2 showing a segment and a nut.

DETAILED DESCRIPTION OF THE INVENTION

(23) An embodiment of the present invention for a strut construction, movable under load from an extended, locked position to a retracted, unlocked position will be described hereinafter.

(24) FIG. 1 shows an embodiment of the collapsible strut construction in the retracted, unlocked position that comprises: an external cylinder (1) having a lug (20) at an end; an inner cylinder (2) slidable within the external cylinder (1) and having a second lug (21) at an end; a screw (3) rotatable disposed within the inner cylinder (2); a drive (4) attached to the external cylinder (1) and configured to rotate the screw (3); a nut (5) coupled to the screw (3) and connected to the inner cylinder (2), being movable with respect to the external cylinder (1) responsive to the rotation of the screw (3); at least one segment (6) located in a radial opening of the inner cylinder (2) and movable radially outward and inward in response to the movement of the nut (5) and configured to engage the external cylinder (1) when moved radially outward and not to engage the external cylinder (1) when moved radially inward, the inner cylinder (2) being lockable to the external cylinder (1) by the segment (6) in an extended position of the strut, the strut further comprises a second inner cylinder (7) located external to the first inner cylinder (2) and internal to the external cylinder (1) when the first inner cylinder (2) is retracted into the external cylinder (1), the second inner cylinder (7) being joined to the first inner cylinder (2) such that both cylinders (2, 7) are displaceable together.

(25) Therefore, both the first (2) and the second (7) inner cylinder are disposed in the external cylinder (1) and are jointly movable longitudinally within external cylinder (1). Both the first (2) and the second (7) internal cylinder are moved outward from the external cylinder (1) and inward into the external cylinder (1).

(26) Typically, the end connection (20) of the external cylinder (1) of the strut is attached to a fixed aircraft structure and the end connection (21) of the internal cylinders (2, 7) are attached to a movable structure, more specifically to a door.

(27) Extension and retraction of the screw (3) is provided by the drive (4) arrangement, including a drive motor assembly, a gear assembly and a brake (36) of the screw (3) which are mounted at the head end of actuator. Drive (4) assembly includes a housing in which is disposed a motor. The drive (4) motor is coupled to the screw (3) located within internal cylinder (1).

(28) Screw (3) assembly includes an elongated screw (3) and a compatible nut (5) riding thereon and coupled thereto by thread engagement, that run in the external helical groove of screw (3), so that rotation of the screw (3) produces translation of the nut (5) on the screw (3).

(29) In the retracted position, both internal cylinders (2, 7) are disposed inside of the external cylinder (1) with the screw (3) inside of the internal cylinder (1) and the nut (5) being drawn substantially to the head end. In this position, actuator is fully retracted and unlocked.

(30) Actuator is driven from the retracted position to the extended position by operating drive (4) motor assembly in a direction to drive the nut (5) in a direction from head end towards internal cylinder (2) end. Similarly, actuator is driven from the extended position to the retracted position by operating electric drive motor assembly to rotate the screw (3) in an opposite direction to drive the nut (5) in a direction from rod end towards head end.

(31) The external cylinder (1) comprises a locking groove or opening (24) configured to house the at least one locking segment (6) in the extended, locked position. Thereat, locking mechanism is unlocked with the plural segment (6) are in a radially inward position. Two lock segments (6) are shown in the figures and they extend radially outward to engage the openings (24) within the external cylinder (1).

(32) When actuating power is not applied a lock spring (25) maintains the nut (5) and therefore the segment (6) in its locked position.

(33) In the locked position of locking mechanism, the inner end of lock segment (6) is adjacent to a cylindrical surface of a collar (26) located around the nut (5) that is of a given diameter selected to so position the lock segment (6) a predetermined radial distance from a central axis of the screw (3) and nut (5). The collar (26) comprises two cylindrical surfaces of different external diameter, one leaving the segment (6) in a lower position and therefore not engaging the recess (24) in the external cylinder (1) and not locking the strut and a second cylindrical surface having a larger diameter and locating the segment (6) into the mentioned recess (24). In the transition between both cylindrical surfaces a sloped surface exists. The combination of these surfaces provides a cam for moving lock segments (6) radially inward and outward for engaging and disengaging lock segments (6) of lock mechanism. When the nut (5) is moving axially lock segments (6) move and radially out of the openings (24).

(34) The position of the collar (26) is additionally secured by an angle (32) designed into sliding surfaces between segment (6) and collar (26). This angle (32) is defined in order to guarantee an irreversible system. Any failure in spring (25) or in a retaining ring (33) of the piece retaining the spring (25) do not allow the inadvertent unlocking operation. This angle (32) is used in both: collar (26) and segment (6) and has to be zero or negative as depicted in FIG. 17 considering that negative angles are those measured in the clockwise direction from the positive horizontal axis.

(35) The nut (5) has also two outwardly extending flange segments (27, 29) at each of its opposite ends. One (29) avoids the collar (26) to step out the nut (5) and the other one (27) retain the spring (25) extending between the collar (26) and the flange (27). Lock spring (25) therein serves to bias the nut (5) towards the locked position, urging the collar (26) to move towards the end of the screw (3). Flange (29) avoiding the collar (26) to step out the nut (5), due to the force exerted by the spring (25), is integrated into the nut (5) avoiding an inadvertent unlocking of the system. In order to allow the assembly of the spring (25), the other flange (27) is separated from the nut (5).

(36) In disengaging the lock mechanism out of the locked position, the screw (3) is rotated in the opposite direction to move the nut (5) towards head end. The distal flange (29) of the nut (5) contacts the collar (26) and urges it (26) towards the base, therefore the segment (6) is displaced to the lower surface of the collar (26) and therefore out of the opening (24) of the external cylinder (1).

(37) As can be seen in FIG. 3 when the actuator is working properly the load path (30) goes from the end connection (21) configured to be coupled to the door, through the inner cylinder (2) until the segment (6) in which the load is transferred to the external cylinder (1) and then to the end connection (20) configured to be coupled to the aircraft structure. In the extended and locked position, a substantial portion of the internal cylinders (2, 7) extend beyond the end of the external cylinder (1).

(38) The locking mechanism locks the internal cylinders (2, 7) in its extended position relative to the external cylinder (1) so that the structural loads are entirely supported by the external (1) and internal cylinder (2) which are structurally locked together by locking mechanism as can be seen in FIG. 3.

(39) In the extended position, the nut (5) is driven into an over-travel position wherein locking mechanism locks the first internal cylinder (2) to external cylinder (1) with the lock segment (6) of locking mechanism having been driven radially outward to engage into an opening (24) in the wall of the external cylinder (1).

(40) The strut comprises a mechanical element extending between the first inner cylinder (2) and the second inner cylinder (7) configured to avoid the axial and radial relative movement between both cylinders (2, 7). Said mechanical element is a pin (10) located in an opening of the first inner cylinder (2) and in an opening of the second inner cylinder (7). As additionally, the second inner cylinder (7) is in axial contact with the first inner cylinder (2), a second load path is achieved. Said axial contact is performed by two corresponding flanges (34, 35) at the end proximate to the segment (6) orifice of the inner cylinder (2).

(41) FIG. 7 discloses the actuator working under condition of failure of the inner cylinder (2). In this particular case the load will be transferred from the lug (21) of the inner cylinder (2) to the second inner cylinder (7) by the pin (10) and due to the axial contact between them (2, 7) to the segment (6) and to the external cylinder (1).

(42) The electrical telescopic strut construction shown in the figures comprises a mechanical element extending between the inner cylinder (2) and the nut (5) configured to avoid the radial relative movement between both elements (2, 7). The mechanical element is a pin (11) located in an opening of the inner cylinder (2) and in an opening of the nut (5) thus restricting the relative radial movement between the nut (5) and the inner cylinder (2). The pin (11) or pins (11) are located in an extension (31) of the nut (5). The opening of the nut (5) is an axial opening (12) such that there is an axial relative movement between the inner cylinder (2) and the nut (5). Said mechanical element allows a second load path as depicted in FIG. 4 in case of failure of the segment (6) being the load transferred from the internal cylinder (2) to the nut (5) and from there to the screw (3). Therefore, the segments (6) with automatic locking are part of the main road and the screw (3) with brake (36) is part of the second loading path as in case of failure of the segments (6) the assembly screw (3)-brake (36) can stand the applied loads in a second load path.

(43) The nut (5) is connected mechanically to cylinder (2) by means the radial pin (11) located in slidable axial gaps (12). The axial gap (12) allows the strut the absorption of traction and compression loads by displacing the nut (5) with respect to the internal cylinder (2) the length of the axial gap (12). From fully extended or retracted position, the first linear movement of nut (5) created by the rotational movement of screw (3), will absorb this axial gap (12) before any linear movement of cylinders (2, 7). This free movement of the nut (5) with respect to the cylinder (2) allows the unlocking of collar (26) and segments (6) by the displacement of the nut (5) towards the collar (26) until the nut (5) reaches said collar (26) and pushes it to achieve the unlocking of the system as can be seen in FIGS. 13 to 15.

(44) During normal operation to extend and retract the strut, in which the segment (6) is not locked, the load path (30) is conducted through the main mechanical parts as screw (3), pins (11) and cylinder (2). Therefore, the external dynamic loads are not applied through segment (6) during extension and retraction allowing a simpler sizing of segment (6), reducing the shear area required. Segment (6) only supports the static external load in fully extended and locked position.

(45) FIG. 4 shows a case in which there is a failure in the segment (6), in that case, and due to a double path of the actuator, the load is transferred from the inner cylinder (2) to the nut (5) thorough pin (11) and afterwards to the screw (3). The screw (3) is locked by the brake (36) and therefore the load is transferred to the brake (36) and to the end connection (20).

(46) The second inner cylinder (7) comprises a second lug (22) at its free end. Additionally, the second inner cylinder (7) is in axial contact with the first inner cylinder (2), the second lug (22) and the axial contact defining an additional load path as depicted in FIG. 5.

(47) FIG. 5 discloses the actuator working under condition of failure of the end connection (21) coupled to the inner cylinder (2). In this particular case the load will be transferred from the end connection (22) coupled with the second internal cylinder (7) to the segment (6) and from there to the external cylinder (1).

(48) The embodiment also shows a second end connection (23) configured to be connected to the aircraft structure and coupled to the armature which is in turn coupled to the external cylinder (1) by an axial contact.

(49) FIG. 6 discloses the actuator working under condition of failure of the end connection (20) coupled to the external cylinder (1). In this particular case the load will be transferred from the external cylinder (1) to the second end connection (23) of the external cylinder (1).