초록 ▼

A payload is housed in a deliverable body of a device, such as in a projectile, and this device is delivered as close as possible to a target. At the landing point, a drive system of the body is activated to take the payload directly to the target. The target is described by target coordinates, for

A payload is housed in a deliverable body of a device, such as in a projectile, and this device is delivered as close as possible to a target. At the landing point, a drive system of the body is activated to take the payload directly to the target. The target is described by target coordinates, for example, which are programmed into the device before it is launched. The device itself can be steered or unsteered. The drive system installed on the body or formed by the body is variable and should occupy a minimum of space.

대표청구항 ▼

The invention claimed is: 1. A device, comprising: a body adapted for independent travel through air with aid of a separate launch device to a landing site a distance from a target, the body being divided into cylindrical, coaxial segments, which are connected to each other; a payload arranged in t

The invention claimed is: 1. A device, comprising: a body adapted for independent travel through air with aid of a separate launch device to a landing site a distance from a target, the body being divided into cylindrical, coaxial segments, which are connected to each other; a payload arranged in the body and operative to trigger open or concealed mines and explosive charges on or in land; a computer arranged in the body for controlling sequences of operations and navigation; a programming module and a navigation system arranged in the body and electrically connected to the computer; and an integrated land drive system installed on or formed by the body, and configured to take the body holding the payload to the target by mechanically self crawling on the surface of the ground immediately after the body has landed at the landing site, the drive system including a first drive motor for a front segment and a second drive motor for a rear segment, the drive motors being provided in a middle segment, wherein helical flights are mounted on the front and rear segments, the flights on the front segment and the rear segment having a common orientation and a common pitch, wherein a flight is mounted on the middle segment and has an opposite orientation but a common pitch as the flights on the front and rear segments, the flight of the middle segment being substantially twice a length of one of the other flights. 2. The device according to claim 1, and further comprising a device for determining direction and a device for determining distance traveled, both devices being integrated into the body. 3. The device according to claim 1, and further comprising a brake system provided on the body so as to activate about 5 m above the landing site. 4. The device according to claim 3, wherein the brake system is an airbag that detaches when the body comes to rest. 5. The device according to claim 4, wherein small explosive charges are arranged on the airbag for detaching the airbag from the body. 6. The device according to claim 1, and further comprising a device for determining direction and a device for determining distance traveled. 7. The device according to claim 6, wherein the device for determining direction operates in the earth coordinate system and is constructed as a magnetic sensor.