US35611A - Improvement in concussion-fuse for explosive shells - Google Patents

Improvement in concussion-fuse for explosive shells Download PDF

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US35611A
US35611A US35611DA US35611A US 35611 A US35611 A US 35611A US 35611D A US35611D A US 35611DA US 35611 A US35611 A US 35611A
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shell
wire
plug
plunger
fuse
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/24Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by inertia means

Description

B. B. HOTCHKISS.
Shell-Fuse.
Patnted Jime 17, 1862.
UriiTnio STaTes PATENT @rrrcn.
I3. 13. IIOTCHKISS, OF SHARON, CONNECTICUT.
Specification forming part of Letters Patent No. 35,5512, dated June 17, l8ll2.
lb all whom it may concern:
Be it known that I, B. B. Ho'rcrriuss, of Sharon, in the county of Litchlield, in the State of Connecticut, have invented certain new and important Improvements in the Fercussive Mechanism of Explosive Shells; and I do hereby declare that the following is a full and exact description of the same, prepared with a View to the obtaining of Letters Patent therefor.
My improvement is intended for use in councction with rifled ordnance, or with some other means of throwing the shell in such manner that the point which will strike the object first can be determined. Its purpose is to cause the shell to explode with certainty at the instant of striking any object, and to avoid all danger of explosion at other periods.
The accompanying drawings form a part of this specification, and similar letters refer to like parts in. all the figures.
Figure l is a longitudinal section of mypercnssive mechanism as inserted in a shell ready for use. Fig. 2 is a similar section ofthe same as it exists after the shell in which it is introd need is discharged from the cannon, and while all the parts are flying with equal velocity through the air; and Fig. 3 is a similarsection of the same as it exists after the shell has struck an object or while it is in theact of striking and before it has exploded.
Fig. 1, it will be observed, represents, in addition to my percussive mechanism, a section of aportion of a conical rifled-cannon projectile in which it is supposed to be used. Iprefor to use it in such a projectile; but the latter forms no part of my present invention.
My invention is applicable to any and all characters of explosive missiles which can be made to strike with any given point or side against the object to be destroyed.
To enable others skilled in theart to make and use my invention, I will proceed to describe its construction and aid of the drawings.
A is a case or barrel of the form represented. Its shoulder a rests, through the intervention of a soft ring, '13, upon a corresponding shoulder in the fusecavity in the shell 0, as repre sented. It is inserted in the cavity and secured by the screwDin the manner whichis obvious, and may be introduced and so secured either operation by the immediatelybefore the act of loading the can a non or a long time earlier, as may beinost convenient. In the base of the barrel A is a conical hole provided with a coni i211 plug, 113, as represented. In the interior of the case A is a heavy plunger of any suitable material and of the form represented by F. Its upper end is fitted with a cone or nipple, G, as represented, and its interior is filled with powder II. The cone G is provided with a common percussioir cap, and the lower end of the powder-cavity in F is closed by sealing it slightly with shellac varnish. In the base of the case A is laid a washer of soft material, I, as represented. A
wire, J, is so introduced between the plug E y and its seat as to hold it with sufficient force to resist the concussions occasioned by ordinary handling, or by dropping it from the hands or from a wagon upon the ground. The other end of this wire is secured to the plunger F, and so long as the plug E remains in the position shown in Fig. 1 the plunger is held by this wire in the position indicated, so that the nipple G cannot strike its cap against the top plate of the case to effect its discharge, except under the action of a force sufficient to violentlypull out the wire from its hold on one or the other )art. 1 WVhen the shell 0 is fired from the cannon, the violence with which it is suddenly urged forward by the discharge causes all the loose parts to tend backward within the shell with great force by their inertia. The tapering form of the plug E renders it extremely liable to yield to this force by its own inertia, and the inertia of the whole of the heavy plunger F, pressing against its point, makes it certain thus to yield and to escape backward from the cav ity in A, while the plunger F follows it so far as it is allowed by the structure of the parts.
Fig. 2 shows the position of the parts at this period, and shows the plug E slightly turned around, as it is very likely to move after it has become entirely free from A. After the shell '0, with its contents, has been discharged and the parts E F, &c. have acquired the same ve locity as the shell, no tendency to change their relative positions exists until the instant of striking. In the act of stopping the shell,the resistance being felt by the outside first, the tendency of all the loose parts is to'move forward within the shelLwith a violence pro portioned to the suddenness with which the motion is stopped. This tends to induce the parts to assume the position shown in Fig. 3, unless the plugE is so far disturbed in its axial position that its point fails to enter again in the hole from which it escaped, and in'either case the heavy plunger A is projected by its entire inertia, minus the friction, if any, on the wire J, and is thrown against the front with 7 are not represented, but may .beof any character desired-that is to say, may be powder alone, loose or solid, or may be powder arranged in any manner desired relatively to shot or other destructive or offensive material.
The several parts of my apparatus or mechanism may be ofvarious forms and proportions; but I have tried the forms and sizes indicated and found them highly successful. I prefer for some reasons to make the ease Aof wrought or cast iron, the plunger F of like material, and the ring B, washer I, and plug E of lead or some soft and heavy alloy, while the wire J may be of copper or any other desired material. I can unite my wire J to the plunger F by soldering or otherwise, if desired; but I have found it suffieient to simply compress it tightly between the screw-threads of the nipple G and the interior of the plunger. It is thus so slightlyheld'that if by any chance the other extremity of the wire should be entangled or nipped so firmly as to positively retain it, the connection of the wire to the plunger would then yield and release the latter,so as to allow the same action as before described.
The junction of the rear end of the wire J with the base of the tube A, or with the plug E, may be made strong or slight by a simple adjustment before putting the case A and its contents within the shell (3. The adjustment may be made in many ways,which will readily occur to any skilled mechanic, as the end of the wire and the plug are both freely accessible; but one of the simplest methods is by allowing the wire'to remain straight and pan tially loosening the plug to make the shell explode easily, and by cutting off the point of the plug and driving it verytight, and then bending the end of the wire either over upon the plug across its rear end or over upon the base of A, to make the shell explode only on striking a very hard object or a very severe resistance. The latter end may be often desirable in firing ricochet shots, either on land or water, and by shortening the inner or front end of E, and bending the wire across its base,so as to partially tie it, the plug may be made to stand with its point in the hole during the flight of the shell, and to be pretty certain to again seat itself and hold the wire with con-' siderable force, so as not to allow the nipple to meet the front of the case during the ricochets, but only on the impact against the object desired. 7
Excepting for the chance of liberating the plunger by the means described, it is not important that the wire be attached to F by pressure between it and the nipple, or that it be any other than an extension of the plunger F itself.
It is also not essential that it possess any rigidity.
My invention maybe operated with success if the part J be a wire, a strip of metal, or even a flexible cord of silk or other material.
The plug E, in addition to its'holding the wire J or its equivalent, performs a very important function by excluding the powder or other contents of the shell from theinterior of In my invention it will be obthe case A. served the interior of the case A is never open to the interior-of the shell 0 until after the shell has commenced its flight or is in the act of commencing it.
The wire J, in addition to its sustaining the plunger while handling the shell and in ricochets, also prevents the premature explosion of the shell by the elastic rebound of the parts which occurs when the shell starts on its flight.
The soft ring B prevents the friction or percussion of A within 0 from striking fire, and reduces the elasticity of the parts.
Having now fully described my invention, what I claim as new therein, and desire to secure by Letters Patent, is
The plug E and wire J, or their respective equivalents, arranged to operate in the percussive mechanism of explosive projectiles, substantially as herein set forth.
B. B. IIOTCIIKISS.
Yv'itn esses THOMAS D. Srnfrsoiv, H. M. CoLLYnn.
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060064403A1 (en) * 2004-09-17 2006-03-23 Rechterman Barbara J Web page customization based on expertise level of a user
US20060064637A1 (en) * 2004-09-17 2006-03-23 Rechterman Barbara J Web page customization based on search engine search term
DE102007061407B4 (en) 2006-12-13 2021-03-04 General Electric Co. Waterjet stripping and recontouring of gas turbine guide vanes and blades

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060064403A1 (en) * 2004-09-17 2006-03-23 Rechterman Barbara J Web page customization based on expertise level of a user
US20060064637A1 (en) * 2004-09-17 2006-03-23 Rechterman Barbara J Web page customization based on search engine search term
DE102007061407B4 (en) 2006-12-13 2021-03-04 General Electric Co. Waterjet stripping and recontouring of gas turbine guide vanes and blades

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