Linear actuator
A linear actuator includes a housing, a piston rod having a longitudinal axis (A-A) and at least one locking arrangement. The piston rod is axially moveable in a first direction (D 1 ) relative to the housing to extend the piston rod and is axially moveable in a second direction (D 2 ) relative to the housing to retract the piston rod. The piston rod is rotatable about the longitudinal axis relative to the housing between an operational state and a locking state. Each locking arrangement includes a piston rod flange extending from the piston rod and a housing flange extending from the housing. When the piston rod is in the operational state, the or each housing flange does not overlap with the or each piston rod flange so as to allow axial movement of the piston rod in the first and second directions.
1 . A linear actuator comprising:
a housing comprising a hollow cylindrical body having an outer wall;
a piston rod having a longitudinal axis; and
at least one locking arrangement comprising an arm extending parallel to an radially from the outer wall,
wherein the piston rod is axially moveable in a first direction relative to the housing to extend the piston rod,
wherein the piston rod is axially moveable in a second direction relative to the housing to retract the piston rod,
wherein the piston rod is rotatable about the longitudinal axis relative to the housing between an operational state and a locking state,
wherein each locking arrangement comprises a piston rod flange extending from the piston rod and a housing flange extending from the arm of the locking arrangement,
wherein when the piston rod is in the operational state, each housing flange does not overlap with each piston rod flange so as to allow axial movement of the piston rod in the first and second directions,
wherein when the piston rod is in the locking state and the housing flange is positioned beyond the piston rod flange in the first direction, the housing flange of each locking arrangement at least partially overlaps with the piston rod flange of that locking arrangement so as to limit axial movement of the piston rod in the first direction.
2 . The linear actuator as claimed in claim 1 , comprising a plurality of locking arrangements.
3 . The linear actuator as claimed in claim 1 , comprising three or a multiple of three locking arrangements.
4 . The linear actuator as claimed in claim 2 , wherein the locking arrangements are evenly circumferentially spaced on the linear actuator.
5 . The linear actuator as claimed in claim 1 , wherein each locking arrangement is configured to also limit axial movement of the piston rod in the second direction when the piston rod is in the locking state and the housing flange is positioned beyond the piston rod flange in the first direction.
6 . The linear actuator as claimed in claim 5 , wherein each locking arrangement comprises either:
an engagement surface on the housing, circumferentially aligned with and axially spaced from the housing flange so as to form a recess between the engagement surface and the housing flange; or
an engagement surface on the piston rod, circumferentially aligned with and axially spaced from the piston rod flange so as to form a recess between the engagement surface and the piston rod flange.
7 . The linear actuator as claimed in claim 6 , wherein the or each locking arrangement comprises a piston part extending axially outwardly from the piston rod in the second direction and radially inwardly of an outer wall of the housing, wherein the part forms the recess, the engagement surface on a first axial side of the recess and the piston rod flange on a second, opposite side thereof.
8 . The linear actuator as claimed in claim 1 ,
wherein each piston rod flange extends outwardly from the piston rod and the or each housing flange extends inwardly from the housing; or
wherein each piston rod flange extends inwardly from the piston rod and the or each housing flange extends outwardly from the housing.
9 . The linear actuator as claimed in claim 1 , wherein each piston rod flange the or each housing flange and/or the or each engagement surface extend approximately in a radial direction.
10 . The linear actuator as claimed in claim 1 , comprising an indicator for indicating whether the piston rod is in the operational state or the locking state.
11 . The linear actuator as claimed in claim 1 , wherein the linear actuator is a flight control actuator, and/or
wherein the linear actuator is a hydraulic actuator.
12 . The linear actuator as claimed in claim 1 , comprising:
a rod end attached to the piston rod by a threaded connection; and
a mechanism for adjusting the rotational alignment of the rod end on the piston rod to allow the rod end to accurately rotate the piston rod between the operational condition and the locking condition as required.
13 . An aircraft comprising:
at least one flight control surface; and
a linear actuator as claimed in claim 1 ;
wherein the piston rod is connected to the flight control surface.
14 . A method of locking a flight control surface of an aircraft as claimed in claim 13 , the method comprising:
rotating the piston rod of the linear actuator from the operational state to the locking state; and
prior to rotating the piston rod, retracting the piston rod until the housing flange is positioned beyond the piston rod flange in the first direction.