Submunition for a spin stabilized carrier projectile
AssigneeRheinmetall GmbH
InventorsKlaus D. Karius, Armin Eskam, Karl-Heinz Vogt
Life of this patent
Estimating the term…
Abstract
A submunition unit for a spin stabilized carrier projectile (1), with the submunition unit including an antenna disposed at the nose of its casing (7), and with the antenna (5) being covered by a protective cover (6). The casing (7) and the protective cover (6) are provided with respective axially overlapping collars (8, 9) which are each provided with respective opposed circumferential grooves (14, 15) to form an annular recess to accommodate an elastic securing ring (16). The securing ring, which is normally positioned within the innermost of the circumferential grooves, expands under the influence of centrifugal forces to connect the casing and protective cover together in a form-locking manner.
Claims11
In a submunition unit for a spin stabilized carrier projectile comprising:
- an outer casing having a first axially extending annular collar at its front end;
- an antenna mounted in said casing at said front end;
- a protective cover for said antenna, said cover having a second axially extending annular collar at its rear end, with said first and second collars axially overlapping and engaging one another and with a radially extending end surface of at least one of said collars engaging a radially extending surface associated with the other of said collars to axially support said cover on said casing;
- and means for securing said protective cover to said casing including a locking element mounted for movement in a direction toward the circumference of said casing to form a form-locking connection between said cover and said casing in response to an appropriate centrifugal force acting on said unit and to release the connection between said cover and said casing when the number of revolutions of said unit, and thus the centrifugal force, drops below a given value;
- the improvement wherein said locking element is a securing ring which expands under the influence of centrifugal forces, and said means further comprises:
- a first circumferential groove on an exterior surface of the radially inward one of said first and second collars, said first circumferential groove having a depth corresponding to the thickness of said securing ring in the radial direction and normally containing said securing ring;
- and a second circumferential groove formed on an interior surface of the radially outer one of said first and second collars opposite said first circumferential groove, with said second circumferential groove having a depth less than said thickness of said securing ring, and both of said grooves having an axial height which includes an amount of play relative to the axial height of said securing ring that is greater than the axial deformation caused by the deformation forces generated at said first and second collars during launching of said unit.
Dependencies are inferred from the claim text.