AIRBORNE PLATFORM FOR AIRCRAFT WITH ATTITUDE CORRECTION AND TOW HITCH ASSEMBLY
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app pub date -
Aug 25, 2016
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Feb 28, 2014
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Abstract
In a general aspect, a towed device for an aircraft can include a support structure carrying measurement means, the support structure being supple and substantially flat when deployed, a traction pole, means for fastening the support structure to the traction pole, an attachment element for attaching the towed device to a towing cable, and an attitude-correcting structure arranged between the attachment element and the traction pole. The attitude-correcting structure can include an attitude-correcting pole configured to be towed by the aircraft in a vertical position, by means of the attachment element, and traction stays. The traction stays can respectively connect a first end of the attitude-correcting pole to two opposite ends of the traction pole, and a second end of the attitude-correcting pole to the two opposite ends of the traction pole, giving the traction pole a horizontal attitude when the attitude-correcting pole is in the vertical position.
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