Forward extraction force transfer coupling
An extraction force transfer coupling device is particularly adapted for use with certain cargo aircraft systems for aerial delivery of a load. The extraction force transfer coupling device employs a drop arm which prevents inadvertent actuation of the actuator arm. Prior to aerial delivery, the actuator arm is obstructed by the drop arm. When the platform is forwardly extracted from the aircraft, the drop arm slides along and eventually disengages from the aircraft floor which eventually results in actuation of the cable release to provide for opening of a suspension parachute.
1. A forward extraction force transfer coupling comprising:
a housing mountable to a forward edge portion of a platform;
a cylinder with a control rod mounted in said housing;
a cable received by said housing;
a crank pivotally connected to said control rod and connected to said cable;
an actuator arm rotatably mounted for rotation at the exterior of said housing and rotatably connected to the crank;
said crank and said cable being displaceable in response to rotation of said actuator arm; and
a drop arm mounted to said base for preventing rotation of the actuator arm in a first position and pivotable from said first position to allow rotation of said actuator arm.
2. The forward extraction force transfer coupling of claim 1 wherein said drop arm and said actuator arm pivot about axes which are orthogonal to each other.
3. The forward extraction force transfer coupling of claim 1 wherein said drop arm includes a transversely extending rod and an inclined toe.
4. The forward extraction force transfer coupling of claim 1 wherein said drop arm comprises an angled member which connects with an extension having an enlarged portion.
5. The forward extraction force transfer coupling of claim 1 and further comprising a platform with a forward portion, said forward extraction force transfer coupling is mounted to said forward portion.