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Publication numberUS3425354 A
Publication typeGrant
Publication dateFeb 4, 1969
Filing dateOct 30, 1967
Priority dateOct 30, 1967
Also published asDE1805427A1
Publication numberUS 3425354 A, US 3425354A, US-A-3425354, US3425354 A, US3425354A
InventorsCarlson Donovan
Original AssigneeHoneywell Inc
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Centrifugally armed fuze
US 3425354 A
Abstract  available in
Previous page
Next page
Claims  available in
Description  (OCR text may contain errors)

Feb. 4, 1969 o. CARLSON 3,425,354

GENTRIFUGALLY ARMED FUZ E Filed Oct. 30, 1967 I NVENTOR. DONOVAN CARLSON AT TORNE Y 3,425,354 CENTRIFUGALLY ARMED FUZE Donovan Carlson, Minneapolis, Minn., assignor to Honeywell Inc., Minneapolis, Minn., a corporation of Delaware Filed Oct. 30, 1967, Ser. No. 678,910 US. Cl. 10279 Int. Cl. F42c 9/06, 15/26 4 Claims ABSTRACT OF THE DISCLOSURE Background of the invention Field of the invention.Percussive or electric fuzes wherein the fuze is armed by inovement of a member which responds centrifugally to rotation of the shell (CL 102-79).

Description of the prior art.Centrifugal arming is quite well-known in the prior art. Most centrifugal arming arrangements, however, comprised of mechanical locks and weights. Fluid is utilized in some cases for the purpose of delaying the operation of the fuze. Examples of the prior art are Patents 2,641,186 to Apotheloz and 3,118,379 to Jasse. The applicant is not, however, aware of any prior art wherein fluid is used as a positive force in the arming sequence of a centrifugally armed fuze.

Summary of the invention The present invention provides for an arming and time delay mechanism for spin operated fuzes. Its unique feature is that it employs a buoyant slider member mounted in a fluid-filled housing. In the unarmed condition the slider member is held away from the axis of rotation by a spring and by centrifugal looks or other suitable safing mechanisms. The space around the slider member is filled with a fluid having long-term stability and a relatively uniform viscosity over a broad temperature range. The fluid has adequate density to float the slider assembly.

The fuze is spin actuated. The centrifugal locks are are released under spin environment, releasing the slider member. Under the spin conditions, the fluid is displaced outwardly, away from the axis of rotation, and the buoyant slider is forced by the fluid inwardly toward the axis of rotation. The slider member carries an explosive detonator, which upon actuation is carried by the slider member into a position in line with a firing pin and a pyrotechnic chain.

It is therefore an object of the present invention to provide an improved centrifugally armed fuze. A further object of the present invention is to provide a centrifugally armed fuze wherein a fluid is used to provide a positive force in the arming sequence. These and further objects will become apparent to those skilled in the art upon examination of the following specification, claims, and the drawing.

A brief description of the drawing FIGURE 1 is a cross-sectional view of a typical embodiment of the fuze according to the present invention, looking along the spin axis from the top of the fuze;

States Patent 3,425,354 Patented Feb. 4, 1969 FIGURE 2 is a simplified schematic representation of the embodiment of FIGURE 1;

FIGURE 3 is a sectional side view taken along line 3-3 of FIGURE 1;

FIGURE 4 is a simplified schematic. representation of the sectional side view of FIGURE 3; and

FIGURE 5 is a similar sectional side view, but with the fuze in the armed position.

Detailed description Referring now to FIGURE 1, a cross-sectional view of the fuze is shown out along a plane perpendicular to the axis of rotation. The fuze has an outside fuze housing 10. Within fuze housing 10 is mounted a delay housing 12. Delay housing 12 defines a cylindrical cavity -13 whose axis intersects the axis of rotation and lies in a plane substantially perpendicular to the axis of rotation. Cavity 13 extends from one side of housing 10 across the center of housing 10, a certain distance beyond the axis of rotation. Within cavity 13 is mounted a buoyant slider piston 14. Slider piston 14 is biased towards the end of cavity 13 which is nearest the outside wall of housing 10. The biasing is accomplished by a light spring 15 located between slider piston 14 and a closure member 16 which defines the inner end of delay housing 12.

Slider piston 14 carries a detonator 18 at a position which is away from the axis of rotation while the slider piston is in its normal position adjacent to the outside wall of housing 10. The entire internal cavity of delay housing 12 is filled with a fluid 20. Fluid 20 is chosen for a long-term stability and a relatively uniform viscosity over a broad temperature range. The relative density of fluid 20 to slider piston 14 is such that slider piston 14 will float. To give slider piston 14 sufiicient buoyancy, the slider piston can be provided with a hollow cavity 21, such as shown in FIGURE 1. Cavity 21 is shown being sealed by a cover 22.

At the inner most end of slider piston 14, a seal 17 is placed around the periphery of slider'member 14, adjacent to the internal walls of delay housing 20. The purpose of seal 17 is to prevent uncontrolled flow of fluid 20 from one side to the other side of slider piston 14. A metering orifice 19 is, however, provided to allow the flow of fluid 20 from one side to the other side of slider piston 14 at a controlled rate.

A pair of centrifugal locks 24 and 25 are mounted Within delay housing 12 and are adapted to engage with slider piston 14 to prevent the motion of piston 14 prior to a predetermined threshold of angular rotation about the fuze axis of rotation.

A more clear understanding of the apparatus of FIG- URE 1 will be achieved by referring to FIGURE 3. FIG- URE 3 shows a cross-section of a side view cut along lines 3-3 of FIGURE 1. Delay housing 12 is shown held between a forward housing member 28 and a rear housing member 29. Formed in the rear housing member 29, concentric with the axis of rotation, is an opening 30 within which is located a lead cup or booster charge 31. An opening 32 is formed in forward housing member 28, opening 32 being centrally located and coaxial with opening 30 on rear housing member 29. Mounted within opening 32 is a firing pin 34. Firing pin 34 has a first flange 35 formed adjacent the pointed end thereof, to prevent the firing pin 18 from being forced out of opening 17. A second flange 36 is connected to the opposite end of firing pin 34 by a screw 37. Mounted between flange 36 and forward housing member 28 is a coiled spring 38 which tends to hold firing pin 34 in the position shown in FIGURE 3.

The simplified schematics of views 2, 4, and 5 will be helpful in understanding the operation of the invention.

Operation In the unarmed condition, buoyant slider piston 14, carrying detonator 18, is held away from the axis of rotation by centrifugal locks 24 and 25. If redundancy is desired for additional safety, setback locks can also be added although they are not shown in the embodiments of FIGURES 1 and 2. The space surrounding slider piston 14 is filled with a fluid such as Dow Corning Silicone 200, which has a long-term stability, has a relatively uniform viscosity over a broad temperature range, and is of adequate density to float slider piston 14. The displacement away from the axis of rotation of lock weights of centrifugal locks 24 and 25 under the spin environment releases slider piston 14. Under spin conditions the fluid is displaced outwardly through orifice 19 at a rate de pending on rotational velocity and orifice size. The resulting buoyant force acting on the slider member moves it toward the in-line position against a light return spring 15.

Delay time will depend on the viscosity of the fluid and hence on temperature. The use of a very short orifice causes the flow rate to follow the Bernoulli equation, and minimizes the flow restriction due to the viscous shearforces, thus yielding a delay that is inversely proportional to the spin rate and relatively insensitive to temperature. The delay time can be controlled by varying the spring biasing and varying viscosity of the fluid.

Although centrifugal locks are shown in FIGURE 1 for holding the slider prior to the operation of the fuze, these may not be necessary because of the force-time integrating features of the dash-pot system. A setback lock pin may be more appropriate.

A unique feature of the present invention, as compared to prior art fluid delays, is that in case of loss of fluid from the system, the fuze will remain in a fail-safe condition. This is an advantage of great importance, as will be obvious to those who are familiar with the safety hazards in the area of fuzing art.

The following functioning sequence places the fuze from a unarmed to an armed position. Centrifugal locks 24 and 25 are released by centrifugal forces above a safety threshold. Fluid 20 is displaced radially through metering orifice 19 by a centrifugal force at a rate dependent upon projectile spin and orifice size. The slider floats toward armed position, snapping in line when seal 17 passes over arming grooves 40 and 41, thus permitting a sudden increase in fluid flow rate.

Obvious advantages of the present invention are that it is extremely simple in operation and is therefore highly reliable. It has the unique safety feature that it is impossible to prematurely arm and has high resistance to rough handling environments.

From the above description it will be apparent that I have invented a munition fuzing concept having new and more effective means for utilizing the centrifugal force developed by a rotation munition for arming purposes and providing safety in handling.

I claim:

1. An arming and time delay mechanism for spin operated fuzes comprising:

a fuze housing defining a hermetically sealed chamber filled with a relatively high density fluid;

a buoyant slider positioned in said fluid within said chamber, said slider having a freedom of motion along a line substantially perpendicular to the spin axis of the fuze;

an explosive detonator mounted on said slider; and

locking means mounted in said housing for holding said slider away from the axis of rotation when said fuze is in an unarmed condition, and to release said slider for motion toward the axis of rotation in response to fluid pressure exerted on said slider, in line with a firing pin and pyrotechnic chain, after the fuze is subjected to an angular rotation.

2. An arming and time delay mechanism for a spin operated munition fuze comprising:

a fuze housing having an axis of rotation;

a firing pin and an explosive lead cup mounted in said housing centered on said axis of rotation;

a delay housing mounted within said fuze housing, said delay housing defining a hollow hermetically sealed chamber of generally cylindrical shape with its axis substantially perpendicular to said axis of rotation;

a slideable piston member mounted within said delay housing, said piston member subdividing the sealed chamber of said delay housing into a first chamber toward said axis of rotation and a second chamber away from said axis of rotation, said piston member further having a fluid passage to allow fluid transfer between said two chambers;

a fluid filling said sealed chamber of said delay housing, said fluid having suflicicnt density to float said piston member;

a detonator mounted on said piston member; and

safing means mounted in said delay housing for holding said piston member away from the axis of rotation when said fuze is in an unarmed state, and to allow said piston member to move toward the axis of rotation when said fuze is caused to spin about its axis of rotation in response to fluid flow from said first chamber to said second chamber to arm the fuze by bringing said detonator in line with said firing pin and said explosive lead cup.

3. Apparatus according to claim 2 wherein said safing means includes a spring for biasing said piston member away from the axis of rotation.

4. Apparatus according to claim 3, wherein said safing means further includes centrifugal locking means for maintaining said slideable piston locked in a safe position until said fuze is caused to spin about its axis of rotation in excess of a predetermined angular rate.

References Cited UNITED STATES PATENTS 527,250 10/ 1894 Smith 102-82 3,118,379 1/1964 Jasse 102-79 3,264,995 8/1966 Libby et al 102-79 3,296,969 1/ 1967 Mueller et a1. 102-82 FOREIGN PATENTS I 129,041 7/ 1919 Great Britain.

BENJAMIN A. BORCHELT, Primary Examiner. GERALD H. GLANZMAN, Assistant Examiner.

US. Cl. X.R. 102-82

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US527250 *Oct 24, 1893Oct 9, 1894Charles STime-fuse for projectiles
US3118379 *Nov 10, 1961Jan 21, 1964 Fuze for a gyratory projectile
US3264995 *May 11, 1964Aug 9, 1966Avco CorpMechanical fuze operable on grazing impact
US3296969 *Oct 14, 1964Jan 10, 1967Thiokol Chemical CorpTime delay initiator
GB129041A * Title not available
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3633511 *Nov 12, 1969Jan 11, 1972Lacroix ERocket fuse with delayed-action arming
US3640225 *Jun 20, 1969Feb 8, 1972Honeywell IncFuze apparatus
US3721195 *Jun 1, 1971Mar 20, 1973Honeywell IncLiquid revolution counter for fuze arming
US3732824 *Apr 28, 1971May 15, 1973Us ArmyMeans for converting impulse linear acceleration to rotational inertia
US3750589 *Dec 13, 1971Aug 7, 1973Honeywell IncCentrifugally driven spin device
US4018164 *Jun 12, 1975Apr 19, 1977Breed CorporationProjectile fuze containing a floating body
US4078497 *Aug 6, 1973Mar 14, 1978Breed CorporationLiquid timing device having a floating mass
US4098192 *Jun 23, 1976Jul 4, 1978Breed David SBall rotor safety and arming delay device
US4213395 *Mar 3, 1978Jul 22, 1980Breed David SBall rotor safety and arming delay device
US7530312Jun 14, 2006May 12, 2009Sandia CorporationInertial sensing microelectromechanical (MEM) safe-arm device
U.S. Classification102/238, 102/277, 102/245
International ClassificationF42C15/00, F42C15/285, F42C15/184
Cooperative ClassificationF42C15/285, F42C15/184
European ClassificationF42C15/184, F42C15/285