Projectile Equipped With Deployable Parachute

The invention relates to a projectile equipped with a deployable parachute. More particularly, the present invention relates to such a projectile which is composed of at least two sections arranged axially in tandem and connected with one another by means of radially extending bolts, and with one of the sections accommodating the parachute.

One possibility of recovering projectiles undamaged after firing is to decelerate the flying velocity of the projectile or of its components to acceptable ground impact values with the aid of a parachute. A parachute can also be employed to cause the projectile tip to penetrate into the ground.

To cause the parachute to become effective, it must be ejected on the trajectory or the projectile must be separated in such a way that the parachute is able to automatically deploy as a result of the streaming air.

It is an object of the invention to provide a projectile having a deployable parachute, with such a projectile being of the type mentioned above with two axially tandem sections connected by radial bolts and having a simple structure and permitting reliable separation for deployment of the parachute.

This object is accomplished according to the invention by a projectile of the above described type wherein the radial bolts are radially chargeable by the gas pressure so as to separate the two sections, with the pyrotechnic charge being burnt off or ignited by way of a fuse.

Further features of the invention are to be found in the description below and in the dependent claims.

The invention will be described below in greater detail with reference to embodiments that are illustrated in the attached drawing figures.

FIG. 1 is a longitudinal sectional view of a projectile equipped with one embodiment of a separating device.

FIG. 2 is a cross-sectional view of the separating device along line II--II of FIG. 1.

FIG. 3 is a longitudinal sectional view along line III--III of FIG. 2.

FIG. 4 is a cross-sectional view along line IV--IV of FIG. 3.

FIG. 5 is a longitudinal sectional view along line V--V of FIG. 4.

FIG. 6 is a partial cross-sectional rear view of a further embodiment of a separating device.

FIG. 7 is a longitudinal sectional view along line VII--VII of FIG. 6.

FIGS. 8 to 11 are sectional views corresponding to lines VIII--VIII to XI--XI of FIGS. 6, 7, 8 and 9.

FIG. 12 is a longitudinal sectional view of an additional embodiment of a separating device.

FIG. 13 is a sectional view along line XIII--XIII of FIG. 12.

In the embodiment shown in FIGS. 1 to 5, a projectile 1 is composed of a nose section 2, a center section 3 and a tail section 4, with tail section 4 being equipped with fins 5 and accommodating two parachutes 6, 6'. Also provided is a propelling cage 7 which extends essentially over the center section 3 and part of the tail section 4 and is discarded upon firing after it has left the gun barrel.

Center section 3 is provided at its rear with a coaxial cylindrical recess 8 at whose bottom two delayed-action fuses 9 are disposed which are covered by means of a plate 10. Recess 8 is closed by an insert 11 which simultaneously accommodates plate 10 and is connected with center section 3 by means of screws 12 extending in the axial direction. On its circumference, insert 11 is sealed against center section 3 by circumferential seals 13 between which there is disposed an annular, circumferential channel 14.

In corresponding blind bores in insert 11, a pyrotechnic charge 15 and a flame capsule 16 are inserted from the side facing plate 10 in two diametrally oppositely disposed positions, the flame capsule 16 being connected by way of conduits 17 extending through plate 10 with the associated delayed-action fuses 9 so that flame capsules 16 can be ignited by delayed-action fuses 9. Gas conducting channels 18 extend from the region of the blind bores accommodating the pyrotechnic charge 15 to the annular channel 14.

Moreover, three bolts 19 are provided which are equipped with pistons 20 at their rear sides and are received in radial bores 21 in insert 11 which are distributed equidistantly over the circumference of insert 11 in the region between the two seals 13. In the region of insert 11, the outer diameter of center section 3 is reduced while tail section 4 has a correspondingly enlarged inner diameter to be able to receive the end of center section 3. In the telescoped state of center section 3 and tail section 4, both sections are provided with bores which are coaxial in the overlapping region and through which bolts 19 extend up to the outer circumference of tail section 4 so as to connect center section 3 and tail section 4 with one another, while a gas pressure chamber 22 exists between the interior of center section 3 and the oppositely disposed side of piston 20, which is disposed in the region of channel 14.

Piston 20 may be provided with a circumferential seal 23 while bolt 19 may be provided with an axial bore 24 which permits easy positioning of bolts 19 during assembly.

Additionally, insert 11 is provided with a recess 25 to accommodate a bearing 26 whose inner ring is connected with an eye 27 which is thus movable and receives a loop 28 of parachute 6. Bearing 26 is secured in insert 11 by a spring ring 29.

If, after firing of projectile 1, parachute 6 is to be deployed, flame capsules 16 are ignited by delayed-action fuses 9 thus causing the pyrotechnic charges 15 to burn off. The gases developed thereby travel through gas conducting channels 18 into annular channel 14 and thus charge the pistons 20 of bolts 19 from the circumferential side by way of gas pressure chamber 22. This causes pistons 20 and thus bolts 19 to be pressed radially inwardly so that they go out of engagement with respect to tail section 4 and the latter is separated from center section 3. Thus parachute 6 which is fastened to center section 3 is released by way of insert 11 and is able to be deployed. Tail section 4 is decelerated by the second parachute 6' whose deployment is also effected by the separation.

In the embodiment shown in FIGS. 6 to 11, center section 3' and tail section 4' are connected with one another by means of clamps 30. Clamps 30 are screwed to bolts 19' which, in turn, are held in insert 11' by axial shear pins 31. Gas conducting channels 18' open into gas pressure chamber 22' between the bottom of bore 21' and the interior of bolt 19' so that the gases generated by the pyrotechnic charges 15 charge bolts 19' from the inside and press them outwardly thus causing shear pins 31 to be sheared off and clamps 30 to be thrown off so that center section 3' and tail section 4' are separated.

Adjacent gas pressure chamber 22', bolts 19' may be provided with a circumferential seal 23'. Delayed-action fuses 9 may be held by means of pins 32 between insert 11' and center section 3'.

In principle bolts 19' which, according to the second embodiment, are secured by shear pins and can be pressed outwardly, can also be used in the first embodiment.

In the embodiment shown in FIGS. 12 and 13, shear pins 31 are replaced by shear discs 33 which are held by a two-part bolt 19". Bores 21" are designed as threaded bores and receive a threaded ring 34 which supports shear disc 33 toward the exterior and surrounds bolt 19". Between shear disc 33 and the bottom of bore 21", a ring 35 is inserted which surrounds bolt 19" so that the gases released by pyrotechnic charges 15 act only on the interior frontal faces of bolts 19".

An annular channel 14" is here provided at the interior of recess 15" and is closed toward the outside by bearing 26. Channel 14" is in communication with bores 21" and with the bores accommodating pyrotechnic charges 15 so that the inner frontal faces of bolts 19" are charged directly by the gas pressure from the combustion of pyrotechnic charges 15 through channel 14".