Apparatus and methods for removably securing payloads in an aircraft
Apparatus and methods for removably securing payloads are disclosed. In one embodiment, a method includes coupling the payload to a body of a locking assembly, engaging an insertion portion of the body into the channel, translating the insertion portion of the body along the track from a first position to a second position, the body being substantially constrained from movement away from the track in the second position, and actuating at least one engagement member from an unsecured position to a secured position, a portion of the track being clampably engaged by the at least one engagement member and the insertion portion of the body when the at least one engagement member is positioned in the secured position such that the body is substantially constrained from movement along the track by the at least one engagement member.
1. A system for securing a payload to a support structure within an aircraft, comprising:
a locking assembly body coupled to the payload;
an insertion portion engaged in a channel of a track, the support structure comprising the track, the insertion portion configured to translate along the track and within the channel from a first position on the track to a second position on the track, and the insertion portion further configured to transition between an unsecured position and a secured position, the insertion portion configured to move in an inward direction relative to the locking assembly body to reach the secured position, the insertion portion configured to engage a portion of the track when the insertion portion is positioned in the secured position such that the locking assembly body is substantially constrained from movement along the track and away from the track by the insertion portion;
an actuation member, the actuation member moveably coupled to the body, the actuation member configured to transition the insertion portion from the unsecured position to the secured position; and
a biasing member configured to maintain a biasing force against the actuation member, the biasing force biasing the actuation member into an unsecured position.
2. The system of claim 1 , wherein the insertion portion comprises a stud coupled to the actuation member through a connector shaft.
3. The system of claim 1 , further comprising:
a locking device configured to lock the actuation member into a secured position.
4. The system of claim 1 , further comprising:
a self-alignment feature coupled to the locking assembly body.
5. The system of claim 3 , wherein the locking device comprises a locking aperture present in the actuation member.
6. The system of claim 5 , wherein the locking device further comprises a locking pin.
7. The system of claim 1 , wherein the actuation member comprises a pedal.
8. The system of claim 7 , wherein the pedal is configured to engage an upper surface of the track when the actuation member is in the secured position.
9. The system of claim 1 , wherein the actuation member is configured to engage an upper surface of a support member when the actuation member is in the secured position.