AIRBORNE PLATFORM FOR AIRCRAFT WITH ATTITUDE CORRECTION AND TOW HITCH ASSEMBLY
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United States of America Patent
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app pub date -
Oct 6, 2016
filing date -
Feb 28, 2014
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Abstract
In a general aspect, a device for attaching a towed device to an aircraft in flight can include an attachment cable secured to the towed device. The attachment cable can have one end forming a closed loop and including a loop head. The device can also include a first attachment element secured to the loop head of the attachment cable, The first attachment element can include first electrical connectors. The device can further include a towing cable attached to the aircraft and a second attachment element attached to one end of the towing cable. The second attachment element can be configured to cooperate mechanically and electrically with the first attachment element. The second attachment element can include second electrical connectors configured to cooperate with the first electrical connectors. The device can still further include fasteners or guides configured to hold the loop head of the attachment cable off the ground.
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