IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0363383
(2001-09-03)
|
우선권정보 |
SE-0003107 (2000-09-04) |
국제출원번호 |
PCT//SE01/01867
(2003-07-02)
|
§371/§102 date |
20030702
(20030702)
|
국제공개번호 |
WO02//21070
(2002-03-14)
|
발명자
/ 주소 |
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
2 인용 특허 :
9 |
초록
▼
The present invention relates to a method for attacking a target by means of a missile (1) with at least one shaped charge, the direction of action of which differs from the direction of flight of the missile, and to a missile (1) comprising at least one shape charge (2) arranged to act in a directi
The present invention relates to a method for attacking a target by means of a missile (1) with at least one shaped charge, the direction of action of which differs from the direction of flight of the missile, and to a missile (1) comprising at least one shape charge (2) arranged to act in a direction (4) that differs from the direction of flight (5) of the missile. The shaped charge jet is corrected for the speed of the missile (1). According to the invention, the correction of the shaped charge jet is adjustable, whereby the lethality of the missile can be achieved within a wide range of speeds of the missile.
대표청구항
▼
1. A method for attacking a target by means of a missile with at least one shaped charge, a direction of action of which differs from a direction of flight of the missile, in which a jet of the shaped charge is corrected for a speed of the missile, the method comprising:adjusting the shaped charge j
1. A method for attacking a target by means of a missile with at least one shaped charge, a direction of action of which differs from a direction of flight of the missile, in which a jet of the shaped charge is corrected for a speed of the missile, the method comprising:adjusting the shaped charge jet relative to the shaped charge; measuring a speed of the missile during flight of the missile towards the target; and carrying out the correction of the shaped charge jet based on the measured speed of the missile. 2. A method for attacking a target by means of a missile with at least one shaped charge, a direction of action of which differs from a direction of flight of the missile, in which a jet of the shaped charge is corrected for a speed of the missile, the method comprising:adjusting the shaped charge jet relative to the shaped charge; and measuring the speed of the missile by measuring its acceleration and integrating. 3. A method for attacking a target by means of a missile with at least one shaped charge, a direction of action of which differs from a direction of flight of the missile, in which a jet of the shaped charge is corrected for a speed of the missile, the method comprising:adjusting the shaped charge jet relative to the shaped charge; and carrying out the correction for the speed of the missile in one or more steps during the flight of the missile. 4. A method for attacking a target by means of a missile with at least one shaped charge, a direction of action of which differs from a direction of flight of the missile, in which a jet of the shaped charge is corrected for a speed of the missile, the method comprising:adjusting the shaped charge jet relative to the shaped charge; and carrying out the correction for the speed of the missile continuously during the fight of the missile. 5. A method for attacking a target by means of a missile with at least one shaped charge, a direction of action of which differs from a direction of flight of the missile, in which a jet of the shaped charge is corrected for a speed of the missile, the method comprising:carrying out the correction in a launcher of the missile before the missile is launched, based on information about a distance to the target; and adjusting the shaped charge jet relative to the shaped charge. 6. The method according to claim 5, the correction is also based on at least one of the following: information about the speed of the target, temperature in the missile or launcher, wind conditions or characteristics of the weapon.7. A missile, comprising:at least one shaped charge arranged to act in a direction that differs from a direction of flight of the missile, the shaped charge comprising a correction device for correcting a jet of the shaped charge based on different directions of movement of the missile and the shaped charge jet, wherein the correction device is operative to adjust the correction of the shaped charge jet relative to the shaped charge; and one or more electric motors operative to achieve movements of the correction device. 8. The missile according to claim 7, wherein the one or more electric motors comprise stepping motors.9. A missile, comprising:at least one shaped charge arranged to act in a direction that differs from a direction of flight of the missile, the shaped charge comprising a correction device for correcting a jet of the shaped charge based on different directions of movement of the missile and the shaped charge jet, wherein the correction device is operative to adjust the correction of the shaped charge jet relative to the shaped charge; and one or more magnets operative to achieve movements of the correction device. 10. A missile, comprising:at least one shaped charge arranged to act in a direction that differs from a direction of flight of the missile, the shaped charge comprising a correction device for correcting a jet of the shaped charge based on different directions of movement of the missile and the shaped charge jet, wherein the correction device is operative to adjust the correction of the shaped charge jet relative to the shaped charge; and pneumatic or hydraulic systems operative to achieve movements of the correction device. 11. A missile, comprising:at least one shaped charge arranged to act in a direction that differs from a direction of flight of the missile, the shaped charge comprising a correction device for correcting a jet of the shaped charge based on different directions of movement of the missile and the shaped charge jet, wherein the correction device is operative to adjust the correction of the shaped charge jet relative to the shaped charge; and a speed-measuring device arranged in the missile to measure a speed of the missile during flight. 12. The missile according to claim 11, wherein the correction device comprises an initiation point for the shaped charge, wherein the initiation point is movable to adjust the correction of the shaped charge jet.13. The missile according to claim 11, further comprising a propulsive element operative to achieve the movements of the correction device.14. A missile, comprising:at least one shaped charge arranged to act in a direction that differs from a direction of flight of the missile, the shaped charge comprising a correction device for correcting a jet of the shaped charge based on different directions of movement of the missile and the shaped charge jet, wherein the correction device is operative to adjust the correction of the shaped charge jet relative to the shaped charge; and a range-finding device arranged to measure a distance to a target before launching, wherein the correction device pre-sets a correction of the shaped charge jet based at least on the distance. 15. The missile according to claim 14, wherein the correction device comprises an initiation point for the shaped charge, wherein the initiation point is movable to adjust the correction of the shaped charge jet.16. The missile according to claim 14, further comprising a propulsive element operative to achieve the movements of the correction device.17. A missile, comprising:at least one shaped charge arranged to act in a direction that differs from a direction of flight of the missile, the shaped charge comprising a correction device for correcting a jet of the shaped charge based on different directions of movement of the missile and the shaped charge jet, wherein the correction device is operative to adjust the correction of the shaped charge jet relative to the shaped charge; and a propulsive element operative to achieve the movements of the correction device, wherein the propulsive element comprises gunpowder.
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