System for protection in particular of large flying platforms against infrared and/or radar-guided threats
A protection system ( 10 ) is proposed which comprises a storage container ( 1 ), a transport unit ( 2 ), an activation unit ( 3 ), an ejection unit ( 4 ), a monitoring/control unit ( 5 ) and a user unit/interface ( 6 ), as well as at least one effect body ( 7 ). This system ( 10 ) is integrated at the front in a flying carrier ( 11 ), and a modular system ( 10 ), with the object of positioning spoof measures in a defined manner, in this case by means of the effect body ( 7 ). The various effect bodies ( 7 ) are preferably activated and initiated in a controlled manner without any physical contact, in the same way as pneumatic or mechanical ejection of these effect bodies ( 7 ). The effect bodies ( 7 ) are packets without any munitions, and are responsible for the actual effect of the system ( 10 ) outside the carrier ( 11 ).
1. A protection system, comprising:
at least one storage container;
an activation unit;
a monitoring and control unit for monitoring and controlling individual components of the system;
a user unit;
a plurality of active bodies arranged in the storage container;
at least one transport unit capable of fast and sequential transport of the active bodies to the activation unit for activation; and
an ejection unit operative to eject the active bodies, wherein the storage container supplies the active bodies, the activation unit activates the active bodies and is operative to ensure that the various active bodies are activated or initiated in a controlled manner with or without any physical contact, wherein the system is integrated in a carrier and the active bodies are munition-free packets responsible for an actual effect of the system outside the carrier, wherein the storage container is mechanically, releasably and exchangeably connected to the carrier so as to be reusable.
2. The protection system in accordance with claim 1 , wherein the storage container is a reusable, fire resistant, sealed case or container for supplying the active body, whereby the container is exchangeable for another container.
3. The protection system in accordance with claim 1 , wherein the transport unit is a conveyor belt system.
4. The protection system in accordance with claim 1 , wherein the transport unit is a pneumatic tube conveyance system.
5. The protection system in accordance with claim 1 , wherein various active bodies are provided, the activation unit being operative to activate the various active bodies with contact.
6. The protection system in accordance with claim 1 , wherein the ejection unit has a pneumatic or mechanical system that allows pneumatic or mechanical ejection of the active body.
7. The protection system in accordance with claim 6 , wherein the ejection unit includes fast, electrically switching valves or springs.
8. The protection system in accordance with claim 1 , wherein the monitoring and control unit has a stored-program control system.
9. The protection system in accordance with claim 1 , wherein the monitoring and control unit has an interface with the carrier.
10. The protection system in accordance with claim 1 , wherein the active bodies provide an infrared and radar effect.
11. The protection system in accordance with claim 1 , wherein the system is integrated in a flying carrier.
12. The protection system in accordance with claim 10 , wherein the active bodies are red phosphorus or chaff.
13. The protection system in accordance with claim 1 , wherein the monitoring and control unit provides computer-assisted controllability for setting action, duration of action, and intensity of action of the active bodies by deployment of variable portions and numbers of the active bodies.
14. The protection system in accordance with claim 1 , wherein an unfolding effect of the active bodies is controlled by well-defined activation and separation during well-defined ejection.
15. The protection system in accordance with claim 1 , wherein the active bodies have different geometries.