Arrestment system

• US 4,311,290 A
• Filed: 11/01/1979
• Issued: 01/19/1982
• Est. Priority Date: 11/01/1979
• Status: Expired due to Term

• Current Assignee: the united states of america as represented by the secretary of the navy
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Koper, Kenneth T.
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US06/090,205
• Time in Patent Office: 810 Days
• Field of Search: 244/110 R, 244/110 F, 244/63, 244/114 R, 244/115, 244/116, 244/137 R, 258/1.2, 258/1.8, 258/11-26, 114/261
• US Class Current: 244/110.00R
• CPC Class Codes: B64F 1/0299 characterized by the use of multiple devices
• CPC Class Codes: B64U 10/50 Glider-type UAVs, e.g. with parachute, parasail or kite for landing B64U70/83
• CPC Class Codes: B64U 70/30 for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
• CPC Class Codes: B64U 70/83 using parachutes, balloons or the like

Abstract

Apparatus and method for recovering and arresting an aircraft or other vele. A boom is swivelly connected to a support structure via braking mechanism. The boom is pivotally connected to the brake mechanism such that it can also pivot in a second, different plane intersecting the plane of rotation of the brake mechanism. A shear pin prevents pivoting of the boom in the second plane until the boom has experienced a predetermined load in that plane. The distal end of the boom distant from the brake mechanism is provided with structure for engaging the aircraft. When the aircraft is flown at and captured by the boom, the weight and motion of the aircraft breaks the shear pin, causing the boom to move in the second plane until engaged by a stop. This rapid change in position of the engaging end of the boom in the second plane prevents the aircraft from pendulating about the boom. Forward motion of the aircraft also causes movement within the brake mechanism in the first plane which absorbs the kinetic energy of the aircraft as the boom swivels against the brake mechanism, so that the aircraft is slowed and arrested.

Claims

1. Apparatus for arrestment on a vessel of an aircraft in flight having a parafoil connected to it by shroud lines from the body of the aircraft, comprising:

support means formed to be uprightly mounted on the vessel;

engaging means pivotally connected to said support means and radially extending therefrom for pivoting downwardly and about said support means upon capturing the shroud lines; and

adjustable braking means operatively connected between said support means and said engaging means for providing a constant force for stopping the aircraft within a predetermined sector of pivoting of said engaging means about said support means.

2. Apparatus as recited in claim 1 wherein said engaging means further comprises:

boom means pivotally connected to said support means;

releasing means releasably connecting said boom means and said braking means for preventing until capture of the aircraft downward movement and pendulation of the aircraft about said boom means; and

limiting means connecting to said braking means for limiting downward movement of said boom means to the plane of motion of the aircraft.

3. Apparatus as recited in claim 1 wherein said braking means further comprises:

disc means connected to said engaging means for rotation therewith and rotatably connected to said support means; and

caliper means mounted on said support means about said disc means for stopping the rotation of said disc means about said support means.

4. Apparatus as recited in claim 3 wherein said braking means further comprises:

power means operatively connected to said caliper means for providing a predetermined brake force to delete the aircraft'"'"'s kinetic energy within said predetermined sector of pivoting.

5. Apparatus as recited in claim 2 wherein said releasing means comprises:

shearing means releasably connecting said boom means and said braking means for preventing until capture of the aircraft downward movement and pendulation of the aircraft about said boom means.

7. Apparatus as recited in claim 5 wherein said engaging means further comprises:

a shear pin releasably connecting said boom and to said brake for preventing until capture of the aircraft downward movement and pendulation of the aircraft about said boom; and

a pad connected to said brake for limiting downward movement of said boom to the line of flight of the aircraft.

6. Apparatus for arrestment on a vessel of an aircraft in flight having a parafoil connected to it by shroud lines from the body of the aircraft, comprising:

an upright support formed to be mounted on the stern deck of the vessel;

an adjustable boom pivotally connected at one end to said support and laterally extending therefrom for pivoting downwardly and about said support upon capturing the shroud lines; and

a brake operatively connected between said support and said boom for stopping the aircraft within a 90 degree sector of pivoting of said boom about said support.

8. Apparatus as recited in claim 6 wherein said brake further comprises:

a disc connected to said boom for rotation therewith and rotatably connected to said support means; and

calipers mounted on said support about said disc for stopping the rotation of said disc about said support.

9. Apparatus as recited in claim 8 wherein said brake further comprises:

a pressure source operatively connected to said calipers for providing a predetermined brake pressure to deplete the aircraft'"'"'s kinetic energy within said 90 degree sector of pivoting.