Ballistic element
The ballistic element is made with a main body of non-metallic material, such as, from filaments of glass, aramid, carbon and basaltic fibers. The ballistic element also has heads of metal at opposite ends of the main body. A tubular liner of plastic may be disposed with the main body about an axial cavity for a detonating charge. The main body may also have one or more inserts for receiving one of an anchor bolt and a suspension component of an aircraft for use of the element as an aircraft bomb.
1. A ballistic element comprising
a main body made completely in a composite non-metallic material having a lateral wall of tubular configuration developed around a longitudinal main axis of said main body and defining an axial cavity delimiting a housing area for receiving an internal charge, at least one strengthening rib on said lateral wall extending substantially longitudinally of said axis and two terminal sections, each said terminal section being disposed at a respective extremity of said lateral wall; and
a pair of heads, each said head being fastened directly to a respective terminal section of said main body.
2. A ballistic element according to claim 1
wherein said at least one rib extends parallel to said axis.
3. A ballistic element
comprising a main body made completely in a composite non-metallic material having a lateral wall of tubular configuration developed around a longitudinal main axis of said main body and defining an axial cavity delimiting a housing area for receiving an internal charge, a plurality of strengthening ribs on said lateral wall uniformly distributed around said axis, and two terminal sections, each said terminal section being disposed at a respective extremity of said lateral wall; and
a pair of heads, each said head being fastened directly to a respective terminal section of said main body.
4. A ballistic element comprising
a main body made completely in a composite non-metallic material having a lateral wall of tubular configuration defining an axial cavity delimiting a housing area for receiving an internal charge, at least one strengthening rib on said lateral wall and two terminal sections, each said terminal section being disposed at a respective extremity of said lateral wall; and
a pair of heads, each said head being fastened directly to a respective terminal section of said main body
wherein each said head has a recess and each said terminal section has a protruding section engaged within said recess of a respective head.
5. A ballistic element according to claim 4 wherein said recess in at least one of said pair of heads is an annular recess and said protruding section of a respective terminal section is of annular shape.
6. A ballistic element according to claim 1 wherein at least one of said heads is made of metal.
7. A ballistic element comprising
a main body made completely in a composite non-metallic material having a lateral wall of tubular configuration defining an axial cavity delimiting a housing area for receiving an internal charge, at least one strengthening rib on said lateral wall and two terminal sections, each said terminal section being disposed at a respective extremity of said lateral wall;
a tubular liner within said main body and circumferentially about said axial cavity; and
a pair of heads, each said head being attached to a respective terminal section of said main body.
8. A ballistic element according to claim 1 further comprising at least one insert in an outer surface of said main body having an anchoring area for receiving one of an anchor bolt and a suspension component of an aircraft.
9. A ballistic element according to claim 8 wherein said lateral wall entirely enfolds said at least one of said insert except for said anchoring area thereof.
10. A ballistic element according to claim 8 wherein an end of said at least one strengthening rib abuts said at least one insert.
11. A ballistic element comprising
a main body made completely in a composite non-metallic material having a lateral wall of tubular configuration defining an axial cavity delimiting a housing area for receiving an internal charge, at least one strengthening rib on said lateral wall and two terminal sections, each said terminal section being disposed at a respective extremity of said lateral wall;
a pair of heads, each said head being fastened directly to a respective terminal section of said main body, and
at least one insert in an outer surface of said main body having an anchoring area for receiving one of an anchor bolt and a suspension component of an aircraft, wherein said lateral wall entirely enfolds said at least one insert except for said anchoring area thereof.