Patent ID: 7871037

Claim:
An emergency landing apparatus comprising: an extraction vehicle for an aircraft, wherein said vehicle comprises of: a chassis; a first adjustable tower and a second adjustable tower; a first gearbox unit wherein said first gearbox unit is mounted on top of said first adjustable tower; a second gearbox unit wherein said second gearbox unit is mounted on the top of said second adjustable tower; a third gearbox unit wherein said third gearbox unit is mounted on lower right side of said chassis; a fourth gearbox unit wherein said fourth gearbox unit is mounted on the lower left side of said chassis; a first rubber restrainer wherein said first rubber restrainer wrapped around said first gearbox unit and extended to said third gearbox unit wherein said rubber restrainer is wrapped around said third gearbox unit; a second rubber restrainer wherein said second rubber restrainer wrapped around said second gearbox unit and extended to said fourth gearbox unit, wherein said second rubber restrainer is wrapped around said fourth gearbox unit; a first moveable wing supporter and a second moveable wing supporter, wherein between said first moveable wing supporter and said second moveable wing supporter a gap is created wherein said gap accommodates space for undercarriage of said aircraft; a plurality of airbags; an adjustable nose supporter unit, wherein said adjustable nose supporter unit covered by rubber and airbag and wherein said adjustable nose supporter unit holds nose of said aircraft, thereby preventing said nose to hit the ground of a runway; a first ramp and a second ramp, wherein said first ramp is installed inside of said apparatus and second ramp is installed at the end of said first ramp; wheels attached to said chassis; brakes; suspension system; and at least two Jet engines to provide a driving force to the apparatus reach a required speed.