|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F42B-010/06 F42B-010/26 F42B-010/14 F42B-010/54 F42B-010/64|
|§371/§102 date||20140314 (20140314)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 30|
The invention relates to a rotationally stabilized projectile (1) for launching from a barrel, which projectile (1) comprises a front projectile part (22), a rear projectile part (20) comprising a rotating band (4), and an intermediate projectile part (21) comprising a freely rotatable middle section (2) arranged with guide wings (3) for improving the gliding capability and guidance capability during the gliding phase and end phase of the projectile. The guide wings (3) are arranged extensibly on the freely rotatable middle section (2), and the intermedi...
1. A rotationally stabilized projectile which is to be launched from a barrel, and wherein said projectile comprises a front projectile part,a rear projectile part-comprising a rotating band, andan intermediate projectile part comprising a freely rotatable middle section arranged with at least two radially extendable guide wings,wherein the guide wings are arranged extensibly on the freely rotatable middle section and are located in front of the rotating band, and wherein the intermediate projectile part also comprises a regulator device for regulating t...