Equation (2) may be written thus--

R r_x - Rr

t_x = T -------- . ---------- (3)

R + r0 (r_x)²

Substituting successively r_x = r0 and r_x = R, we obtain

expressions for the stresses on the external and internal radii--

R - r0 R R - r0

t_R = T -------- and t_r0 = -T ---- --------

R + r0 r0 R + r0

Therefore, in a homogeneous hollow cylinder, in which the internal

stresses are theoretically most advantageous, the layer situated next to

the bore must be in a state of compression, and the amount of

compression relative to the tension in the external layer is measured by

the inverse ratio of the radii of these layers. It is further evident

that the internal stresses will obey a definite but very simple law,

namely, there will be in the hollow cylinder a layer whose radius is

sqrt(R r0), in which the stress is _nil_; from this layer the

stresses increase toward the external and the internal radii of the

cylinder, where they attain a maximum, being in compression in the

internal layers and in tension in the external ones.

The internal pressures corresponding to these stresses may be found by

means of very simple calculations. The expression for this purpose,

reduced to its most convenient form, is as follows:

R / R \ / r0 \

p_x = T -------- ( --- - 1 ) ( 1 - ----- ) (4)

R + r0 \ r_x / \ r_x /

In order to represent more clearly the distribution of stresses and

pressures in the metal of a homogeneous ideally perfect hollow cylinder,

let us take, as an example, the barrel of a 6 in. gun--153 mm. Let us

suppose T = 3,000 atmospheres; therefore, under the most favorable

conditions, P0 = 1.41 T, or 4,230 atmospheres. From Equation (1) we

determine R = 184.36 mm. With these data were calculated the internal

stresses and the pressures from which the curve represented in Fig. 1 is

constructed. The stresses developed under fire with a pressure in the

bore of 4,230 atmospheres are represented by a line parallel to the axis

of the abscissæ, since their value is the same throughout all the layers

of metal and equal to the elastic limit, 3,000 atmospheres. If, previous

to firing, the metal of the tube were free from any internal stresses,

then the resistance of the tube would be

R² - r²_0

P0 = U ----------- ,

R² + r²_0

or 2,115 atmospheres--that is, one-half that in the ideally perfect

cylinder. From this we perceive the great advantage of developing useful

initial stresses in the metal and of regulating the conditions of

manufacture accordingly. Unless due attention be paid to such

precautions, and injurious stresses be permitted to develop themselves

in the metal, then the resistance of the cylinder will always be less

than 2,115 atmospheres; besides which, when the initial stresses exceed

a certain intensity, the elastic limit will be exceeded, even without

the action of external pressures, so that the bore of the gun will not

be in a condition to withstand any pressure because the tensile stress

due to such pressure, and which acts tangentially to the circumference,

will increase the stress, already excessive, in the layers of the

cylinder; and this will occur, notwithstanding the circumstance that the

metal, according to the indications of test pieces taken from the bore,

possessed the high elastic limit of 3,000 atmospheres.

[Illustration: Fig. 1]

In order to understand more thoroughly the difference of the law of

distribution of useful internal stresses as applied to homogeneous or to

built-up cylinders, let us imagine the latter having the external and

internal radii of the same length as in the first case, but as being

composed of two layers--that is to say, made up of a tube with one hoop

shrunk on under the most favorable conditions--when the internal radius

of the hoop = sqrt(R v0) or 118.7 mm., Fig. 2, has been traced,

after calculating, by means of the usual well known formulæ, the amount

of pressure exerted by the hoop on the tube, as well as the stresses and

pressures inside the tube and the hoop, before and after firing. A

comparison of these curves with those on Fig. 1 will show the difference

between the internal stresses in a homogeneous and in a built-up

cylinder. In the case of the hooped gun, the stresses in the layers

before firing, both in the tube and in the hoop, diminish in intensity

from the inside of the bore outward; but this decrease is comparatively

small. In the first place, the layer in which the stresses are = 0 when

the gun is in a state of rest does not exist. Secondly, under the

pressure produced by the discharge, all the layers do not acquire

simultaneously a strain equal to the elastic limit. Only two of them,

situated on the internal radii of the tube and hoop, reach such a

stress; whence it follows that a cylinder so constructed possesses less

resistance than one which is homogeneous and at the same time endowed

with ideally perfect useful initial stresses. The work done by the

forces acting on a homogeneous cylinder is represented by the area _a b

c d_, and in a built-up cylinder by the two areas _a' b' c' d'_ and _a"

b" c" d"_. Calculation shows also that the resistance of the built-up

cylinder is only 3,262 atmospheres, or 72 per cent. of the resistance of

a homogeneous cylinder. By increasing the number of layers or rows of

hoops shrunk on, while the total thickness of metal and the caliber of

the gun remains the same, we also increase the number of layers

participating equally in the total resistance to the pressure in the

bore, and taking up strains which are not only equal throughout, but are

also the greatest possible. We see an endeavor to realize this idea in

the systems advocated by Longridge, Schultz, and others, either by

enveloping the inner tubes in numerous coils of wire, or, as in the

later imitations of this system, by constructing guns with a greater

number of thin hoops shrunk on in the customary manner. But in wire

guns, as well as in those with a larger number of hoops--from four to

six rows and more--the increase in strength anticipated is acknowledged

to be obtained in spite of a departure from one of the fundamental

principles of the theory of hooping, since in the majority of guns of

this type the initial compression of the metal at the surface of the

bore exceeds its elastic limit.[3] We have these examples of departure

from first principles, coupled with the assumption that initial stresses

do not exist in any form in the metal of the inner tube previous to the

hoops having been shrunk on; but if the tube happen to be under the

influence of the most advantageous initial stresses, and we proceed

either to hoop it or to envelope it with wire, according to the

principles at present in vogue, then, without doubt, we shall injure the

metal of the tube; its powers of resistance will be diminished instead

of increased, because the metal at the surface of the bore would be

compressed to an amount exceeding twice its elastic limit. An example of

injury inflicted in this way is to be found in the method adopted for

hooping cast iron tubes cast by Rodman's process. If we take into

consideration the undoubted fact of the existence to a considerable

extent of useful initial stresses in these tubes, then the hoops should

be put on them either with very little shrinkage or none at all, whereas

ordnance authorities everywhere have applied to this case methods which

are only correct for tubes which are free from initial stresses.

[Footnote 3: In certain cases this, of course, may be an

advantage, as, for instance, when the inner tube is under

injurious initial stresses; but then, in order to be able to

apply the necessary shrinkage, we must know the magnitude of

these stresses.]

[Illustration: Fig. 2]

During the process of hooping guns it is very important to know how to

take into account the value and mode of distribution of the prejudicial

stresses in the inner tube, should such exist. Knowing these stresses,

it is possible, by regulating the tension of the hoops, to reduce the

compression of the metal at the surface of the bore to the proper

extent, thus doing away with the previously existing tension, and by

that means removing a source of weakness in the tube. In precisely the

same way in the shrinkage of gun hoops attention must be paid to the

character and value of the stresses which arise in the course of their

manufacture; otherwise it will be impossible to hoop the barrel

throughout in a proper manner. If prejudicial stresses exist in the

metal of a hoop before it is put in its place, then, when the gun is

fired, if it had been shrunk on with the degree of tension usually

allowed, the layer situated in the internal radius will be extended

beyond admissible limits, thereby causing the resistance of the gun to

be less than that prescribed.[4]

[Footnote 4: When the inner tube is strengthened by means of

wire, the initial or natural stresses in the latter may be

neglected on account of its thinness; but when the thickness of

the hoops is reduced, and the number of layers thereby increased,

then the value of the initial stresses in these hoops is a very

important factor with respect to the decrease or increase Of the

powers of resistance of the gun.]

It is evident, from what has been said, that in order to determine

precisely the resistance of hollow cylinders to internal pressures, and

to make the correct calculations for hooping tubes, it is absolutely

necessary to know whether internal initial stresses exist in the tube

and in the hoops, and to ascertain what their nature and intensity may

be--that is to say, whether they are useful or detrimental; yet it is

incontestable that in the construction of modern ordnance no attention

has been paid to the investigations indicated. If it be possible to

ignore these considerations in the manufacture of guns of small caliber,

and where the thickness of metal is not sufficiently great to admit of

strongly developed internal stresses, such is by no means the case with

the colossal and costly weapons of the present day. In these the

thickness of metal in the tube and hoops is very great; hence the

extreme probability of very considerable internal stresses developing

themselves. That the strength of large guns is often far below that

anticipated is demonstrated, year by year, by the repeated cases of

failure. Consciousness as to the want of strength in such guns is made

evident by the precautionary measures as to their use everywhere

adopted. The heavy artillery produced in the gun factories of Europe is

constructed with all the skill, science, and experience which engineers

and artillerists can command, and therefore it would seem that instances

of defective strength should not arise. Such cases, however, do occur

everywhere, and irresistibly give rise to the suspicion that not only is

the system of construction of guns of large caliber faulty, but also

that the conditions of their manufacture must be considered as

defective. Bearing in mind the enormous sums of money expended by every

nation in order to secure an armament of completely trustworthy guns,

this question demands speedy and searching investigation. The first step

in this direction is the study of the internal stresses inherent in the

metal; because, if such exist, and are capable of attaining, under

certain conditions, considerable magnitudes, then it is absolutely

necessary to take advantage of them in order to increase the resistance

of the metal, instead of allowing them to act to its detriment.

The study of natural internal stresses is of importance, not only with

reference to gun making, but also in respect of other structures where

great resistance is required. All have heard of the sudden failure of

crank shafts and piston rods, of the bursting of boiler shells and

tubes, of the breaking of tires, etc. In the majority of cases the

investigations into the causes of such sudden failures have not led to

any definite results. It has usually been found that the metal possessed

a satisfactory elastic resistance, and satisfied all the conditions set

down in the specifications. Had attention been paid during these

investigations to the state of the internal stresses in the metal, the

cause of unlooked-for accidents might have been explained, and steps

would consequently have been taken to avoid them in future.

We are also familiar with the development of considerable internal

stresses in various kinds of steel articles which are subjected to

hardening and tempering; for example, as dies, tools of various

description, sword blades, and thin plates rolled at a low temperature

or subjected to cold hammering. In the foundry the appearance of

internal stresses is of still more frequent occurrence. The neglect of

certain practical rules in casting, and during the subsequent cooling,

leads to the spontaneous breakage of castings after a few hours or days,

although taken out of the sand apparently perfectly sound. Projectiles

for penetrating armor plate, and made of cast steel, as well as shells

which have been forged and hardened, and in which the metal possessed an

ultimate resistance of over twelve thousand (12,000) atmospheres, with

an elastic limit of more than six or seven thousand atmospheres, will

crack to a serious extent, and even break up in the lathe, while the

recess for the copper ring is being turned out. In shell of this nature,

as well as in chilled cast iron shell, the heads are apt to fly off

spontaneously either while they are lying in store or during transport.

Such phenomena, it seems to me, demonstrate the existence of internal

stresses of considerable magnitude in the metal of the projectiles, and

it is highly probable that the manufacture of many articles would have

approached nearer to perfection had more attention been bestowed upon

the study of the internal stresses which they were liable to. Having

thus explained the nature and importance of the subject, I will proceed

to describe the experiments which I have made with a view to its

illustration.--_London Engineer._

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Scientific American Supplement, No. 633, February 18, 1888 · 第 10 / 49 题