Parafoil mid-air retrieval

• US 6,824,102 B2
• Filed: 03/10/2003
• Issued: 11/30/2004
• Est. Priority Date: 03/10/2003
• Status: Expired due to Term

• Current Assignee: Airborne Systems Na Inc. (Transdigm Group Incorporated)
• Original Assignee: Roy A. Haggard
• Inventors: Haggard, Roy A.
• Primary Examiner(s): ELDRED, JOHN W
• Application Number:
  US10/383,362
• Publication Number:
  US 20040195458A1
• Time in Patent Office: 631 Days
• Field of Search: 244/110.F, 244/137.1, 244/137.3, 244/137.4, 244/142
• US Class Current: 244/110.00F
• CPC Class Codes: B64D 1/22 Taking-up articles from earth's surface

Abstract

The capture of payloads carried by a descending parafoil is facilitated by the use of a trailing line from the parafoil that is snagged by a hook on a recovery line from a helicopter. The trailing line can be more easily snagged by the use of a drogue at its end to facilitate the extension of the trailing line. The trailing line can take the form of a loop extending from the parafoil canopy. The trailing line can actuate a slider to collapse the parafoil'"'"'s suspension lines and canopy for easier handling by the capturing helicopter. Cutters can be installed on the lines holding the load to cut those lines when the recovery line pulls to hoist the load, thus separating the parafoil from the load as the load is lifted by the helicopter.

Claims

1. A mid-air retrieval system including a payload;

a parafoil;

said parafoil comprising a canopy, multiple suspension lines and multiple payload risers;

said canopy having a leading edge and a trailing edge;

each said suspension line having two ends;

each said payload riser having two ends;

each said first suspension line end being attached to said canopy;

each said second suspension line end being attached to said first payload riser end;

each said second payload riser end being attached to said payload;

a retrieval-line attached to said parafoil;

a helicopter;

a load-line having two ends;

said first load-line end attached to said helicopter at a provided external cargo hook;

said load line second end being attached to an engagement hook;

said helicopter being flown toward said parafoil, said parafoil in gliding flight, supporting said payload and trailing said retrieval-line;

said helicopter then engaging said retrieval line with said engagement hook;

said helicopter then flying forward and upward until said payload is suspended under said helicopter, and said trailing retrieval line can have two ends;

the first said retrieval-line end being attached to the said first ends of said payload risers;

the second said retrieval-line end being attached to a drogue parachute; and

said retrieval line being routed from said first end upward to said leading edge of said canopy, over the top surface of said canopy, and trailing aft, stabilized by said drogue parachute, the invention comprising;

said trailing retrieval line having two ends;

the first said retrieval-line end being attached to said payload risers at locations between said first end and said second end;

cutter devices being attached to each said payload riser above the locations of said retrieval line attachment to said payload risers;

said cutter devices being triggered by increasing tension on said retrieval line;

said cutters severing said payload risers when triggered;

the second said retrieval-line end being attached to a drogue parachute; and

said retrieval line being routed from said first end upward to said leading edge of said canopy, over the top surface of said canopy, and trailing aft, stabilized by said drogue parachute.

2. The mid-air retrieval system of claim 1 in which said engagement hook has multiple tines that are actuated by remote control to facilitate engagement with said retrieval line by clamping firmly to said retrieval line.

3. The mid-air retrieval system of claim 1 in which said parafoil also includes a slider assembly, said slider assembly comprising:

multiple grommets set in a fabric panel reinforced by webbing;

said suspension lines each being routed through one of said grommets;

said slider assembly being located near said second ends of said suspension lines during gliding flight;

said retrieval line attached to said slider;

said slider moving upward as the helicopter pulls upward on said retrieval line;

said upward movement of the slider assembly serving to collapse said canopy and to facilitate smooth load transfer of the payload weight from the parafoil to the helicopter;

said retrieval line proceeding centrally upward through said suspension lines and through a hole in the center of said parafoil.