US3363567A

US3363567A - Rotationally activated fuze

Info

Publication number: US3363567A
Application number: US113965A
Authority: US
Inventors: Lewis C Dixon
Original assignee: Army Usa
Current assignee: US Department of Army
Priority date: 1961-05-31
Filing date: 1961-05-31
Publication date: 1968-01-16
Anticipated expiration: 1985-01-16

Description

Jan. 16, 1968 1 c. DIXON 3,363,567

HOTATIONALLY ACTIVATED FUZE Filed May 3l, 1961 Figa INVENTOR Lewis C. Dixon BY M MLM- ATTORNEY United States Patent C 3,363,567 ROTATIONALLY ACTIVATED FUZE Lewis C. Dixon, Mount Airy, Md., assigner to the United States of America as represented by the Secretary of the Army Filed May 31, 1961, Ser. No. 113,965 4 Claims. (Cl. 10279) The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment to me of any royalty thereon This invention relates to a rotationally activated fuze. More specifically, it relates to a fuze that arms by rotation albout a principal axis of the f'uze. After arming, the fuze tires by a sudden deceleration of the rotation.

In the drawings, FIG. 1 shows a section through the unarmed fuze. FIG. 2 shows a section through the fuze after the retaining detents have been moved out by centrifugal force. FIG. 3 shows a section through the fully armed fuze. FIG. 4 shows a section through the fuze at moment of ring.

More particularly, the fuze consists of stator casing 4 which is shaped to contain the several pivoted rotating elements therein. Of these, 6 and 8 are firing pins which consist of pivoted Weights having

integral pins

26, 26.

Perforations

24, 24 are drilled cavities which assist in creating the desired unbalance in the weights. Elements 10 and 12 are detents, pivoted about pins 14 and 16 and biased by springs 18 and 20 respectively. These springs bear against the detents on one side and pins 20` and 22 on the other side. The detents are thus biased inwardly against the pivoted firing pins as shown in FIG. 1 with the result that tiring

pins

6 and 8 are not free to rotate until detents 10 and 12 are moved out of the way by centrifugal force as shown in FIG. 2. The bias on these detents is such that they move outwardly prior to or simultaneously with the movement of the rotary tiring pins. As the rotational velocity increases, the rotary firing pins, due to their unbalance, begin to turn and ultimately assume the position shown in FIG. 3. As they reach this position, rounded

lugs

25, 25 on each ring pin encounter opposite sides of pivoted primer holder 28. As the primer holder rotates into the position shown in FIG. 3, the primers 30, 32 positioned in each end of holder line up with the iring pins after which the fuze is armed.

In order to lire, it is necessary that there be a sudden deceleration of the rotation at which time the rotary tiring pins will reverse their rotation with respect to the body of the fuze, and impinge on the primers as shown in FIG. 4. Primer holder 28 is center bored as shown at 34 and this bore is vented through a transverse Ibore through the pivot at 36. Thus when the fuze tires, ignition of the munition of which the fuze is a part takes place through pivot 36 at right angles to the fuze. This makes 3,363,567 Patented Jan. 16, 1968 ICC the fuze especially adaptable to spherical free falling munitions that are rotated about a horizontal axis during their free fall.

There are several advantages inherent in a fuze of this structure. It is symmetrical and balanced in weight about its axis. By proper unbalancing of the tiring pins, it can -be made to arm at any desired rotational velocity. Having armed, it is tired by a sudden reduction in rotational velocity such as might be occasioned -by striking the ground Due to the symmetrical structure of the fuze, it is armed Iby rotation about its principal axis which is the axis of the primer holder. The fuze can therefore occupy a central position in the munition so that the rotational axis of the munition and of the fuze coincide.

I claim:

1. A fuze comprising a hollow fuze body, a centrally positioned and symmetrically pivoted primer holder within said fuze body, said primer holder having primers diametrically positioned in each end thereof, two rotary tiring pins pivotally mounted one at each end in said fuze body and adjacent each end of said primer holder and in mechanical cooperation with said primer holder, the pivotal axis of said primer holder and of said firing pins being parallel and in a common plane, said rotary tiring .pins having impact and balancing portions on opposite sides of the pivotal axis of said tiring pins and Ibeing unbalanced about said pivotal axis with the impact portion being heavier than the balancing portion.

2. A fuze in accordance with claim 1 wherein two pivoted detents are positioned one beside each rotary tiring pin, said detents being centrifugally actuated and serving to hold the rotary tiring pins in unarmed position until the rotation of the fuze reaches a predetermined velocity.

3. A fuze in accordance with claim 1 wherein the rotary tiring pins pivot in the same direction under centrifugal force.

4. A `fuze in accordance with claim 1 wherein the primer holder contains a primer in each end and is bored out to carry the ignition out through a hollow pivot of the pivoted primer.

References Cited UNITED STATES PATENTS 2,458,474 1/1949 Jordan 1oz-702x FOREIGN PATENTS 1,230,402 4/1960 France.

BENJAMIN A. BORCHELT, Primary Examiner.

SAMEUL FEINBERG, ARTHUR M. HORTON,

Examiners.

L. L. HALLACHER, G. H. GLANZMAN,

Assistant Examiners.

Claims

1. A FUZE COMPRISING A HOLLOW FUZE BODY, A CENTRALLY POSITIONED AND SYMMETRICALLY PIVOTED PRIMER HOLDER WITHIN SAID FUZE BODY, SAID PRIMER HOLDER HAVING PRIMERS DIAMETRICALLY POSITIONED IN EACH END THEREOF, TWO ROTARY FIRING PINS PIVOTALLY MOUNTED ONE AT EACH END IN SAID FUZE BODY AND ADJACENT EACH END OF SAID PRIMER HOLDER AND IN MECHANICAL COOPERATION WITH SAID PRIMER HOLDER, THE PIVOTAL AXIS OF SAID PRIMER HOLDER AND OF SAID FIRING PINS BEING PARALLEL AND IN A COMMON PLANE, SAID ROTARY FIRING PINS HAVING IMPACT AND BALANCING PORTIONS ON OPPOSITE SIDES OF THE PIVOTAL AXIS OF SAID FIRING PINS AND BEING UNBALANCED ABOUT SAID PIVOTAL AXIS WITH THE IMPACT PORTION BEING HEAVIER THAN THE BALANCING PORTION.