초록 ▼

At least a first rescue device for receiving rescue is configured on a bottom side of an aircraft and at least a second rescue device for providing rescue is configured on a bottom side of the aircraft. The first and second rescue devices can be optionally configured. For a small aircraft, only the

At least a first rescue device for receiving rescue is configured on a bottom side of an aircraft and at least a second rescue device for providing rescue is configured on a bottom side of the aircraft. The first and second rescue devices can be optionally configured. For a small aircraft, only the first rescue device for receiving rescue can be configured. For a large aircraft, both the first and second rescue devices for providing and receiving rescue can be simultaneously or optionally configured. When an aircraft with the first rescue device for receiving rescue suffers loss of power, insufficient power, or control difficulty, another aircraft with the second rescue device for providing rescue can fly on top of the former and their first and second rescue devices can be linked together so that the troubled aircraft can be pulled away to land in a safe place.

대표청구항 ▼

1. An aircraft rescue device, comprising: a first aircraft; anda first rigid rescue device in the form of a ring attached to a top side of said first aircraft;wherein said first rescue device extends from said top side of said aircraft and is attached via a rail;a second aircraft comprising a detach

1. An aircraft rescue device, comprising: a first aircraft; anda first rigid rescue device in the form of a ring attached to a top side of said first aircraft;wherein said first rescue device extends from said top side of said aircraft and is attached via a rail;a second aircraft comprising a detachable and extensible second rescue device attached to a bottom side of said second aircraft and configured to connect with said first rescue device during a rescue operation. 2. The aircraft rescue device according to claim 1 wherein said second rescue device is flexible. 3. The aircraft rescue device according to claim 1 wherein said second rescue device has a mechanical arm. 4. The aircraft rescue device according to claim 1 wherein said second rescue device has a jointed hook at one end.