U.S. patent number 3,646,792 [Application Number 04/889,587] was granted by the patent office on 1972-03-07 for apparatus for shock-deformation of workpieces.
This patent grant is currently assigned to SAID Hertel, by said Ruppin. Invention is credited to Heinrich Hertel, Dietrich Ruppin.
United States Patent |
3,646,792 |
Hertel , et al. |
March 7, 1972 |
APPARATUS FOR SHOCK-DEFORMATION OF WORKPIECES
Abstract
A die is located in a receptacle and has an exposed surface of
predetermined contour which it is desired to impart to a workpiece.
Support means is provided for supporting a workpiece proximal to
the exposed surface in such position relative to the latter as to
be deformable into conformance with the exposed surface. A shock
energy transmitting medium is accommodated in the receptacle
surrounding the die and the workpiece. Shock-energy producing means
is provided for producing shock-energy in the medium. Shock-energy
transfer means is interposed between the medium and the workpiece
for receiving shock energy from the former and for transmitting on
optimum amount of the shock energy to the latter.
Inventors: |
Hertel; Heinrich (Berlin,
DT), Ruppin; Dietrich (Berlin, DT) |
Assignee: |
SAID Hertel, by said Ruppin
(N/A)
|
Family
ID: |
5713791 |
Appl.
No.: |
04/889,587 |
Filed: |
December 31, 1969 |
Foreign Application Priority Data
|
|
|
|
|
Nov 15, 1968 [DT] |
|
|
P 18 09 866.3 |
|
Current U.S.
Class: |
72/56;
29/421.2 |
Current CPC
Class: |
B23H
1/04 (20130101); Y10T 29/49806 (20150115) |
Current International
Class: |
B23H
1/04 (20060101); B23H 1/00 (20060101); B21d
026/08 () |
Field of
Search: |
;72/56 ;29/421 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Herbst; Richard J.
Claims
We claim:
1. An apparatus for shock-deformation of workpieces, comprising a
receptacle; a die located in said receptacle and having an exposed
surface having predetermined contours which it is desired to impart
to a workpiece; support means for supporting a workpiece proximal
to said exposed surface in such position relative to the latter as
to be deformable into conformance with said exposed surface, and at
a spacing from said surface which is smaller than a given distance
through which said workpiece must yield to absorb an optimum amount
of deformation energy; a shock-energy transmitting medium in said
receptacle surrounding said die and said workpiece; shock-energy
producing means for producing shock-energy in said medium; and
shock-energy transfer means interposed between said medium and said
workpiece being spaced from the latter by at least substantially
said given distance and operative for receiving shock-energy from
said medium and for transmitting an optimum amount of such
shock-energy to said workpiece.
2. An apparatus as defined in claim 1, said workpiece having an
outer side and an inner side with the latter facing and being
spaced from said exposed surface by said distance; and wherein said
transfer means comprises a transfer element at least in part
juxtaposed with but spaced from said outer side of said workpiece
by a distance greater than said distance.
3. An apparatus as defined in claim 2, wherein said workpiece and
said transfer element both are of self-supporting deformable sheet
material.
4. An apparatus as defined in claim 3, wherein said sheet material
is sheet metal.
5. An apparatus as defined in claim 2, wherein said transfer
element defines with said outer side of said workpiece an evacuated
space.
6. An apparatus as defined in claim 2, wherein said transfer
element defines with said outer side of said workpiece a space;
further comprising a body of gas confined in said space and subject
to rapid heating in response to compression resulting from
transmission of shock energy to said transfer element; and
auxiliary energy producing means confined in said space and
operative for producing auxiliary energy for transmission to said
workpiece, in response to heating of said gas to a predetermined
temperature.
7. An apparatus as defined in claim 6, wherein said auxiliary
energy producing means is a combustible oil capable of flash
combustion in response to rise of the temperature of said gas to a
predetermined level.
8. An apparatus as defined in claim 7, wherein said combustible oil
is a predetermined quantity of petroleum, and wherein said gas
consists at least in part of oxygen in an amount smaller than that
required for supporting combustion of the entire predetermined
quantity of petroleum, so that some of said petroleum remains
uncombusted and constitutes an auxiliary shock-energy transmitting
medium.
9. An apparatus as defined in claim 6, wherein said auxiliary
energy producing means is a nonexplosive chemical substance.
10. An apparatus as defined in claim 2, wherein said transfer
element comprises an annular first portion peripherally surrounding
said workpiece, and a transverse second portion extending
transversely of said first portion juxtaposed with said outer side
of said workpiece and spaced from the same axially of said first
portion.
11. An apparatus as defined in claim 10, wherein said first and
second portions are of one piece.
12. An apparatus as defined in claim 11, wherein said portions
consist at least in part of elastomeric material.
13. An apparatus as defined in claim 12, wherein said transfer
element is of inverted cup shape.
14. An apparatus as defined in claim 2, wherein said transfer
element comprises an interior side; and further comprising a
protective foil releasably secured to and covering said interior
side.
15. An apparatus as defined in claim 14, wherein said foil is
self-adhesive.
16. An apparatus as defined in claim 10, wherein said second
portion consists at least predominantly of elastomeric material;
and further comprising connecting means connecting said second
portion with said first portion.
17. An apparatus as defined in claim 6, wherein said auxiliary
energy producing means comprises a solid fuel capable of rapid
combustion for thereby producing said auxiliary energy.
18. An apparatus as defined in claim 6, wherein said auxiliary
energy producing means comprises a solid fuel containing oxygen in
chemically combined form and capable of rapid combustion for
thereby producing said auxiliary energy.
19. An apparatus as defined in claim 18, wherein said solid fuel is
a cellulose-based compound in sheet-material form.
20. An apparatus as define in claim 6, said auxiliary energy
producing means being combustible; further comprising a body of
auxiliary shock-energy transmitting medium in space in contact with
said workpiece; and wherein said auxiliary energy producing means
is spaced from said body for preventing possible interference of
the latter with combustion of said auxiliary energy producing
means.
21. An apparatus as defined in claim 1, said workpiece having an
outer side and an inner side with the latter facing and being
spaced from said exposed surface; and wherein said transfer means
comprises a plurality of transfer element means spaced from one
another and from said outer side of said workpiece, and being
arranged for serially transferring shock energy to the latter.
22. An apparatus as defined in claim 21, said transfer element
means comprising a plurality of differently sized transfer elements
arranged serially in pyramidal form and ascending in order of size
in direction towards said outer side of said workpiece; and a
plurality of spacing rings each arranged between two successive
ones of said transfer elements.
23. An apparatus as defined in claim 1, wherein said transfer means
comprises amplifying means for cascade-amplification of shock
energy in direction towards said workpiece.
24. An apparatus as defined in claim 23, said amplifying means
comprising an initial and a terminal auxiliary shock-energy
producing means, and the first-mentioned shock-energy producing
means being operative for triggering production of shock energy by
said initial auxiliary shock energy producing means.
Description
CROSS-REFERENCE TO RELATED APPLICATION
A related application was filed on Sept. 24, 1969 in the name of
Heinrich Hertel et al. under the title of "Device for
Shock-Deformation of Workpieces," it is copending under Ser. No.
860,752.
BACKGROUND OF THE INVENTION
The present invention relates generally to the deformation of
workpieces by shock pressure energy, and more particularly to an
apparatus for effecting the shock-deformation of such
workpieces.
The concept of deforming workpieces into conformance with the
surface contours of a die by subjecting them to shock originating
from setting off of explosives, or other means, is already known.
Processes for carrying out such deformation are known in the art
under various names, for instance explosive forming and the
so-called "Hydrospark" process. The workpiece, which may be a sheet
material member or a semifinished blank, is superimposed with
spacing on an exposed surface of a die, the exposed surface having
been given the configuration which it is intended to reproduce on
the workpiece itself. The die and the workpiece are accommodated in
a suitable receptacle containing a pressure-transmitting medium,
preferably a liquid medium. Now shock energy is produced in the
medium, for instance by detonating an explosive or in one of the
other ways already known from the art, and this shock energy is
transmitted through the medium in form of kinetic energy to the
workpiece to be deformed, effecting deformation of the workpiece
into close conformance with the exposed surface of the die.
All of this requires only a brief period of time, but nevertheless
the transmission and deformation process is not instantaneous and
the period of time required for it is finite. It follows from this
that in order to absorb the optimum amount of kinetic energy which
carries out the deformation process, the workpiece requires a
certain starting or acceleration distance which, depending upon the
particular deformation problem and the particular deformation
method used, may vary but is generally on the order between
approximately 2 and approximately 10 cm. In other words, taking the
lower limit, if the workpiece moves into contact with the exposed
surface of the die before it has been deflected through a distance
of approximately 2 cm. (or more as pointed out above) it has not
yet absorbed the optimum quantity of kinetic energy from the energy
transmitting medium.
This means that wherever the necessary distance range mentioned
above is not present between the workpiece and the exposed surface
of the die into conformance with which it is to be deformed, the
energy available for the deformation is not fully utilized.
This is true, not exclusively but in particular, in deformation
methods having a limited energy availability, for instance in the
aforementioned "Hydrospark" method or where apparatus is used of
the type disclosed in our aforementioned copending application. The
problem exists in particular where a preformed semifinished blank
is to be deformed, that is a blank which has been preformed to
approximate roughly the contours of the exposed surface of the die
so that is deformation into contact with this exposed surface is
required only to provide sharper and more precise contours of the
workpiece. Under these circumstances the juxtaposed surfaces of the
die and of the workpiece must be closely adjacent prior to
initiation of the deformation process because of the
high-dimensional accuracy which is desired to be obtained in the
finished product, that is in the deformed workpiece. For this
reason there is under these circumstances almost never any
possibility of providing the necessary acceleration distance
mentioned above. This is evidently a disadvantage, which is further
coupled with the fact that residual air remaining in the space
between the juxtaposed surfaces of the die and the workpiece
undergoes high compression when the deformation occurs and thus may
lead to flaws in the finished workpiece.
SUMMARY OF THE INVENTION
It is, accordingly, an object of the present invention to provide
an apparatus for shock-deformation of workpieces which is not
possessed of the aforementioned disadvantages.
More particularly it is an object of the present invention to
provide such an apparatus which is capable of supplying an optimum
quantity of deformation energy to the workpiece even though an
inadequate acceleration distance exists between the workpiece and
the surface of the die.
In pursuance of the above objects, and others which will become
apparent hereafter, one feature of our invention resides in an
apparatus of the type mentioned above, which briefly stated
comprises a receptacle and a die located in this receptacle and
having an exposed surface of predetermined contour which it is
desired to impart to a workpiece. Support means is provided for
supporting a workpiece proximal to the exposed surface of the die
in such position relative to the exposed surface as to be
deformable to conformance with the same. A shock-energy
transmitting medium is provided in the receptacle surrounding the
die and the workpiece and shock-energy producing means is present
for producing shock-energy in the medium. Finally, shock-energy
transfer means is interposed between the medium and the workpiece
for receiving shock-energy from the former and for transmitting an
optimum amount of such shock-energy to the latter.
In accordance with one embodiment of the invention the shock-energy
transfer means may be in form of a transfer element which is
arranged in juxtaposition with the workpiece, being spaced from the
same by the necessary acceleration distance so that it is the
transfer element which undergoes acceleration by the shock energy
transmitted through the transmitting medium before it in turn
transmits its energy to the workpiece, so that the transmission of
energy from the transfer element to the workpiece takes place under
optimum conditions with a resulting optimum transmission of energy.
The transmission may take place directly or by interposing a
pressure transmitting medium, preferably of liquid type. It is
particularly advantageous to evacuate the space between the
transfer element and the workpiece or, if a pressure transmitting
medium is utilized, the space between the pressure transmitting
medium and the transfer element. This makes it possible for the
transfer element to move without encountering any resistance while
it traverses the aforementioned acceleration distance.
However, while this is an advantageous concept it is not necessary
in every instance. Tests have shown that if the aforementioned
space is not evacuated and air is allowed to remain in it, the
energy exchange between the transfer element and the workpiece is
not disadvantageously influenced by the included air which, it will
be appreciated, is subjected to significant compression and
consequent to rapid heating. It was observed that the degree of
effectiveness was approximately on the same order whether or not
the space between the transfer element and the workpiece was
evacuated.
In fact, if air is allowed to remain in the space and thus
undergoes compression and heating as the shock deformation takes
place, this fact may be utilized for providing an additional energy
input into the deformation process. Under the conditions which are
encountered in the space between the transfer element and the
workpiece when this space is not evacuated, that is under the
pressure and temperature conditions which take place as the
transfer element is caused to move towards the workpiece under the
influence of explosively released shock energy, such ordinary fuel
as petroleum may be instantaneously combusted with the oxygen
contained in the air in accordance with the Diesel effect, and the
same is true of fuel containing oxygen in chemically combined form
and which under normal circumstances combust only slowly.
Therefore, such fuels may be accommodated in the aforementioned
space and their combustion and instantaneous energy release may be
triggered when the air in the space reaches a predetermined
temperature as a result of its compression by the transfer element
which advances towards the workpiece under the influence of shock
energy transmitted from the shock energy producing means through
the shock energy transmitting means. In fact, the fuels themselves
may constitute a secondary pressure transmitting medium. For
instance, if the fuel selected is petroleum the quantity of fuel
accommodated in this case may be so chosen as to larger than the
quantity which can be combusted with the available oxygen in the
space. Thus, after combustion a certain quantity of the petroleum
will remain in liquid form and act as a secondary pressure
transmitting medium.
It will be appreciated, of course, that it is also possible to fill
the space between the transfer element and the workpiece, or the
space between the transfer element and a secondary pressure
transmitting medium which may be located intermediate the workpiece
and the transfer element, with reactable gas mixtures--such as an
acetylene-oxygen mixture--instead of with air and liquid fuels.
Whatever combustible fuels may be selected for inclusion in the
aforementioned space to thereby provide an additional energy input
into the deformation process, it will be appreciated that these
fuels are not explosive in character and are therefore considerable
safer than the use of actual explosives. In addition, whereas the
use of some explosives is governed by laws and statutes in certain
countries so that they cannot be freely utilized in shock
deformation processes and apparatus, the fuels which can be used in
the apparatus according to the present invention are not of
explosive nature and therefore their use is in no way subject to
governmental regulation.
The possibility of using the aforementioned fuels in the
aforementioned manner in the apparatus according to the present
invention makes possible embodiments of the apparatus which utilize
cascade-type energy amplification, that is the summation of
successively produced amounts of shock energy with the combined
total acting upon the workpiece. In such embodiments the actual
shock-energy producing means serves primary or even merely for
triggering the initial energy release of the cascade, with this
initially released energy then triggering another release of energy
which will in turn serve to trigger still a further release of
energy. The number of stages may in this case be quite freely
selected depending upon requirements. Evidently, the initial
shock-energy producing means need under these circumstances produce
considerably less energy than if it alone is responsible for
producing an adequate amount of energy capable of effecting
deformation of the workpiece. Such embodiments are particularly
advantageous because they make it possible to control the direction
of energy flow movement and thus to reduce stresses on highly
stressed parts of the apparatus. For instance, in the apparatus
according to the aforementioned copending application the use of
the energy cascade principle increases the deformation
effectiveness while requiring less than half the working pressures
heretofore necessary. One advantage of this in conjunction with the
apparatus according to the aforementioned copending application is
the fact that it permits a significant reduction in the amplitude
of movement of the movable structural element of the apparatus.
The novel features which are considered as characteristic for the
invention are set forth in particular in the appended claims. The
invention itself, however, both as to its construction and its
method of operation, together with additional objects and
advantages thereof, will be best understood from the following
description of specific embodiments when read in connection with
the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWING
FIG. 1 is a diagrammatic sectional elevation of an apparatus
according to one embodiment of the invention;
FIG. 2 is a view analogous to FIG. 1 but illustrating an apparatus
according to a further embodiment of the invention;
FIG. 3 is another view similar to FIG. 1 but illustrating still a
further embodiment of the invention; and
FIG. 4 is a diagrammatic sectional elevation illustrating yet
another embodiment of the invention.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Discussing firstly the embodiment illustrated in FIG. 1 it will be
seen that reference numeral 5 identifies a vessel or receptacle
which accommodates in its inferior a die 1. In the illustrated
embodiment the die 1 rests on the bottom wall of the receptacle 5
and has an upwardly directed exposed surface which is recessed to
provide a contour desired to be obtained in the finished workpiece.
In the illustrated embodiment a semifinished workpiece or blank 11
is supported on the exposed surface of the die 1 but defines with
the exposed surface a free space or gap 9. The slight spacing
between the exposed surface and the marginal portions of the
workpiece 2 with which the latter rests on the exposed surface is
illustrative only, because there will of course be contact between
them. The spacing has been utilized in FIG. 1 to illustrate that
there is no sealing contact between the marginal portions of the
workpiece 2 and the exposed surface of the die 1, that is that the
space 9 is not sealed.
According to the invention there is provided shock-energy transfer
means which here comprises an annular element 13 peripherally
surrounding the workpiece 2 and projecting upwardly above it, and
an energy transfer element 10 which rests on the other edge of the
annular element 13. Reference numeral 12 identifies suitable seals,
for instance O-rings, which provide for a fluidtight seal between
the annular element 13 and the die on the one hand, and between the
annular element 13 and the transfer element 10 on the other
hand.
Because of the spacing of the element 10 from the outer side of the
workpiece 2, that is the side facing away from the die 1, there
exists between the outer side of the workpiece 2 and the element 10
a space 14. A body of shock-energy transmitting medium, for
instance a liquid such as oil, is identified with reference numeral
6 and accommodated in the receptacle 5 surrounding the die 1, the
annular element 13 and the transfer element 10. Because of the
seals 12 the medium 6 cannot enter into the spaces 9 and 14.
Reference numeral 8 identifies an evacuating conduit which may be
connected to a source of vacuum, for instance a vacuum pump, and
which communicates with the space 9. Because the space 9 is not
sealed, as mentioned before, it in turn communicates with the space
14 so that when evacuation is carried out through the conduit 8,
the spaces 9 and 14 are both evacuated together.
The outer side of the workpiece 2 will be seen to be concave, and
it is filled entirely with a body 11 of secondary pressure
transmitting medium, which may again be a liquid such as oil, but
which need not be the same as the medium 6. The spacing between the
element 10 and the outer side of the workpiece 2 is selected in
accordance with the aforementioned requirement relative to the
desirable acceleration distance, that is the spacing will generally
be on the order of between approximately 2 and 10 cm; the precise
distance can be readily determined empirically or by calculation in
dependence upon the requirements and circumstances of a given
case.
Reference numeral 7 identifies diagrammatically a shock-energy
producing means which may be any of the various types known to
those skilled in the art and thus is not believed to require
detailed discussion. It is simply necessary that the means 7 be
capable of producing a predetermined amount of shock energy. This
is transmitted through the medium 6 to the element 10 which is
thereby deflected towards the workpiece 2 in order to drive the
same into precise conformance with the surface contour of the die
1.
The presence of the body 11 of secondary pressure transmitting
medium not only provides for an even distribution of a pressure
impulse from the element 10 over the entire surface area of the
workpiece 2. In addition its presence protects the surface of the
workpiece 2, that is the surface facing towards the transfer
element 10, against mechanical damage on contact with the transfer
element 10.
It should be emphasized that in the embodiment of FIG. 1, where
both the spaces 9 and 14 are evacuated, the secondary pressure
transmitting medium 11 must have a correspondingly low-vapor
pressure, for instance it must be mineral oil or the like. In
addition the presence of vacuum in the spaces 9 and 14 requires
evidently that the elements 10 and 13 have sufficient mechanical
strength to withstand collapse until and unless the element 10 is
subjected to shock energy released by the means 7.
Coming to the embodiment of FIG. 2 it will be seen that this
differs from that of FIG. 1 essentially in that the space 14 is
fluid-tightly sealed with respect to the space 9. Like reference
numerals identify like elements and it will be seen that here the
marginal zone of the workpiece 2 is sealed with reference to the
die 1 by means of suitable sealing means 15, for instance an
elastomeric sealing element or any other means suitable for the
purpose. Thus, only the space 9 is evacuated through the conduit 8,
it being understood that this evacuation aids in the deformation of
the workpiece 2 into conformance with the surface contour of the
die 1. Because the spaces 9 and 14 are fluid-tightly sealed from
one another it is now possible to increase the quantity of
secondary pressure transmitting medium 11, which in FIG. 2 as in
FIG. 1 is illustrated as a liquid, so that it not only fills the
depression in the outer side of the workpiece 2 but actually has a
level above the marginal portions of the workpiece 2. This
facilitates the transmission of pressure also to these marginal
portions and improves fold retention.
In the embodiment of FIG. 2 the transfer element 10 is of course
not subjected to stresses resulting from the presence of vacuum in
the space 14. It therefore requires less mechanical strength than
in the embodiment of FIG. 1 and may for instance be constructed of
lead or the like. Of course, in FIG. 2 as in FIG. 1 the element 10
must either be replaced with a new one after each deformation
process, that is each time when a workpiece 2 has been deformed in
conformance with the contour of the die 1, or it must be
straightened.
It is advantageous that the elements 10 have relatively great mass
but low-deformation resistance (hence lead) to require as little
energy as possible for deforming them because evidently the energy
necessary for deforming the element 10 is no longer available for
deformation of the workpiece 2.
The vessel in FIG. 2 is the same as in FIG. 1, and while the shock
energy producing means 7 has not been shown in FIG. 2 it will be
appreciated that it will also be required, the same as in FIG.
1.
Coming, to the embodiment illustrated in FIG. 3 it will be seen
that this differs primarily from FIGS. 1 and 2 in that the shock
energy transfer means is reusable, and that moreover it is reusable
without requiring straightening or any other actions. In FIG. 3 the
same reference numerals identify the same elements in the preceding
Figures. Here, however, the transfer element 10 and the annular
element 13 of FIGS. 1 and 2 are replaced with a one-piece unit 16
of inverted substantially cup-shaped configuration. Advantageously
the unit 16 may be composed in part or predominantly of elastomeric
material, such as rubber or synthetic plastic, and can be sealingly
placed over and into engagement with a portion 1a of the die 1. If
necessary or desirable the die 1 may be provided with one or more
circumferential grooves 1b in the portion 1a, and corresponding
circumferential ridges 16a may be provided on the unit 16 and
engage in the associated grooves 1b. Of course, the grooves may be
continuous or discontinuous, and other possibilities for connection
are also possible. If grooves and projections are utilized as in
FIG. 3 they can of course provide an additional seal.
In the illustrated embodiment that portion of the unit 16 which
corresponds to the transfer element 10 of FIGS. 1 and 2 has
embedded therein plate-shaped members 17--which may also have other
configurations, for instance be ball-shaped--which may consist of
lead, Wolfram or another suitable material and which serves to
increase the mass of the unit.
While this has not been specifically illustrated it is possible to
protect the unit 16 against damage in response to contact with the
secondary pressure transmitting medium 11, or against damage by the
elevated temperatures which the air in the space 14 will assume
upon compression, by covering the inner side of the element 16 with
a protective foil of suitable material which may or may not be
self-adhesive and can be replaced from time-to-time whenever
necessary. Plastic or metal foils an be used for this purpose.
It should be understood that it is not necessary for the elements
10 and 13 to be replaced with element 16, but that instead the
element 13 may be utilized as before and may carry an element
corresponding to the element 10 of FIGS. 1 and 2 but consisting in
its entirety of elastomeric material or composed predominantly of
such material with inclusion corresponding to the members 17. In
this case suitable clamping means of well-known construction would
be utilized to clamp the element analogous the element 10 to the
annular element 13. A protective foil may then be held in place
against the inner side of the element which corresponds to but
replaces the element 10 of FIGS. 1 and 2, by being clamped between
the same and the annular element 13.
It will be appreciated that the apparatuses according to the
present invention, for instance those of FIGS. 2 and 3, may be
utilized not only with semifinished partly preformed workpieces,
but also with sheet material workpieces which are as yet
undeformed, and with other configurations.
If it is desired for the particular embodiment to use
energy-cascade amplification, that is if an additional energy input
within the respective space 14 is desired, then it is evidently
necessary to provide additional energy-releasing agents, such as
fuels, in the space 14. In FIGS. 2 and 3 this may be accomplished
for instance by replacing the medium 11 with a combustible fluid,
such as petroleum. The quantity of petroleum may be so selected
that it is larger than the petroleum quantity which can be
combusted with the oxygen available in the space 14 so that, when
as much petroleum is combusted as is possible in view of the
available oxygen, the residual liquid petroleum will continue to
act as a secondary pressure transmitting medium.
FIG. 4 illustrates an embodiment using energy-cascade
amplification. Like reference numerals identify like elements as in
the preceding embodiments. Here, however, a plurality of the
elements 10 of FIGS. 1 and 2 have been utilized and in each of the
chambers defined between successive ones of the elements 10
provision has been made for supplying additional energy by
utilizing chemical energy-liberating agents. The elements 10 may
consist of elastomeric material and are protected at their exposed
surfaces by self-adhesive protecting foils 18. Conical spacing
rings 19, 19a maintain the elements 10 in their desired rest
positions. Screws 26 serve to connect the spacing rings with one
another, and also to connect the lowermost spacing ring 19 with the
flange 1c of the member 1.
The uppermost chamber is filled with a combustible gas mixture 21,
for instance a mixture of acetylene and oxyen, which is supplied
through the conduit 24. The middle chamber contains a chemical
energy carrier 22, for instance a solid fuel Oxydator. In the
lowermost chamber energy is supplied by a cellulose foil 23 which
is suspended as indicated by reference numeral 25 so as to be kept
out of contact with the secondary pressure transmitting medium
11.
When energy is applied to the uppermost element 10 (for instance by
a means analogous to the one identified with reference numeral 7 in
FIG. 1), the movement of the uppermost element 10 towards the
center element 10a compresses the gas mixture 21 in the upper
chamber, an occurrence which is coupled with an adiabatic
temperature increase of the mixture 21. This results in ignition
and subsequent combustion of the mixture 21 whereby the element 10a
is downwardly accelerated into the middle chamber in which the
compression phenomenon is repeated. The temperature increase of the
residual air content of this chamber causes combustion of the solid
fuel 22 and this in turn results in downward acceleration of the
element 10b. The operation in the lowermost chamber corresponds to
what has already been explained with reference to FIGS. 2 and
3.
If desired it is also possible to use a solid fuel in form of a
liquid fuel. Such solid fuel may for instance contain oxygen in
chemically combined form and in known manner it may be on cellulose
basis. In fact, to simplify the problem of providing the proper
quantity of fuel, the solid fuel may be produced in form of a foil
or sheet. In this case particularly it is advantageous to separate
the solid fuel from the secondary pressure transmitting medium
11--which in this case of course has no combustible function--in
order to prevent the medium 11 from inhibiting the combustion of
the solid fuel. This can be accomplished in various different ways,
for instance by interposing a foil of synthetic plastic material
between the medium 11 and the solid fuel which, assuming that it is
employed in the embodiment of FIG. 3, would then of course be
located between the upper surface of the medium 11 and the upper
wall of the unit 16.
It will be understood that each of the elements described above, or
two or more together, may also find a useful application in other
types of applications differing from the types described above.
While the invention has been illustrated and described as embodied
in an apparatus for shock deformation of workpieces, it is not
intended to be limited to the details shown, since various
modifications and structural changes may be made without departing
in any way from the spirit of the present invention.
Without further analysis, the foregoing will so fully reveal the
gist of the present invention that others can by applying current
knowledge readily adapt it for various applications without
omitting features that, from the standpoint of prior art, fairly
constitute essential characteristics of the generic or specific
aspects of this invention and, therefore, such adaptations should
and are intended to be comprehended within the meaning and range of
equivalence of the following claims.
What is claimed as new and desired to be protected by Letters
Patent is set forth in the appended claims.
* * * * *