| 摘要 |
The present invention relates to a support arrangement (10) for an aircraft seat (2). The support arrangement (10) relates to a support leg that is arranged to support a seat (2) above the floor (20) of an aircraft. The support arrangement (10) comprises a first part (14) having a first anchoring point arranged to be anchored to the floor (20) of an aircraft and a second part (16) having a second anchoring point arranged to be secured to an aircraft seat (2). The second part (16) is operatively engaged with the first part (14), wherein the first part (14) is deployable downwardly away from the second part (16) from a retracted to an extended configuration to limit variance in the height of an aircraft seat (2) in the event of the first anchoring point being pulled downwardly by the floor (20) of an aircraft, and a retraction impeding arrangement (34) for impeding retraction of the first part (14) from the extended configuration subsequent to deployment. |
