Mobile aircraft recovery system
An apparatus for the recovery of an aircraft includes a capture device and first and second pole pairs. The first pole pair includes first top and bottom poles respectively placed near first top and bottom portions of the capture device. The first pole pair is configured to move from a first position, in which the pole pair holds the capture device in an open position to capture the aircraft, to a second position, in which the pole pair holds the capture device in a closed position to contain the captured aircraft after impact of the aircraft on the capture device. The second pole pair includes second top and bottom poles respectively placed near second top and bottom portions of the capture device. The second pole pair is also configured to move from the first position to the second position. Further, energy elements are coupled on one end to a respective top or bottom portion of the capture device and on another end to a respective top or bottom pole. The energy elements are disposed to absorb the force of the impact of the aircraft.
1. A method for the recovery of an aircraft, comprising:
attaching a first pole pair comprising first top and bottom poles respectively to first top and bottom positions of a capture device;
attaching a second pole pair comprising second top and bottom poles respectively to second top and bottom positions of the capture device;
moving each pole pair from a first position, in which the pole pairs hold the capture device in an open position to capture the aircraft, to a second position, in which the top and bottom poles of the first pole pair and the second pole pair pivot about a pivot point with respect to one another and hold the capture device in a closed position to contain the captured aircraft; and
absorbing the force of an impact using energy elements, each coupled on one end to a respective top or bottom position of the capture device and on another end to a respective top or bottom pole.
2. A method for the recovery of an aircraft, comprising:
attaching a first pole pair comprising first top and bottom poles respectively to first top and bottom positions of a capture device;
attaching a second pole pair comprising second top and bottom poles respectively to second top and bottom positions of the capture device;
pivoting the first and second pole pairs forward in the direction of an impact;
moving each pole pair from a first position, in which the pole pairs hold the capture device in an open position to capture the aircraft, to a second position, in which the top and bottom poles of the first pole pair and the second pole pair pivot about a pivot point with respect to one another and hold the capture device in a closed position to contain the captured aircraft; and
absorbing the force of the impact using energy elements, each coupled on one end to a respective top or bottom position of the capture device and on another end to a respective top or bottom pole.
3. The method of claim 1 , further comprising synchronizing the moving of the top and bottom poles, respectively, using synchronization devices coupled to each one of the first and second pole pairs, wherein the synchronization devices provide the pivot point between the to and bottom poles of the first and second pole pairs.
4. The method of claim 1 , further comprising cradling the aircraft after impact on the capture device comprising a ribbon net that forms a basket-like configuration, wherein the top and bottom poles of the first and second pole pairs pivot to the second position and fold the ribbon net around the aircraft.
5. The method of claim 1 , further comprising maintaining the open position prior to the impact of the aircraft on the capture device, using a beam coupled to each one of the first and second pole pairs on ends opposite from the capture device, and shear devices positioned between the first and second bottom poles and each respective beam.
6. The method of claim 1 , further comprising attenuating the speed of the aircraft after impact of the aircraft on the capture device using shock absorption devices each coupled to a respective one of the first and second pole pairs, wherein the shock absorption devices provide the pivot point between the top and bottom poles of the first and second pole pairs.
7. The method of claim 1 , further comprising positioning the top and bottom poles of the first and second pole pairs at a predetermined angle to retain a net in a ready to capture position prior to impact.
8. The method of claim 2 , further comprising synchronizing the movement of the top and bottom poles, respectively, using synchronization devices coupled to each one of the first and second pole pairs, wherein the synchronization devices provide the pivot point between the top and bottom poles of the first and second pole pairs.
9. The method of claim 2 , further comprising cradling the aircraft after impact on the capture device comprising a ribbon net that forms a basket-like configuration.
10. The method of claim 2 , further comprising maintaining the open position prior to the impact of the aircraft on the capture device, using a beam coupled to each one of the first and second pole pairs on ends opposite from the capture device, and shear devices positioned between the first and second bottom poles and each respective beam.
11. The method of claim 2 , further comprising attenuating the speed of the aircraft after impact of the aircraft on the capture device using shock absorption devices each coupled to a respective one of the first and second pole pairs, wherein the shock absorption devices provide the pivot point between the top and bottom poles of the first and second pole pairs.
12. The method of claim 2 , further comprising positioning the top and bottom poles of the first and second pole pairs at a predetermined angle to retain a net in a ready to capture position prior to impact.
13. The method of claim 4 , further comprising focusing the impact of the capture device on a wing of the aircraft adjacent to a fuselage.