U.S. patent number 3,613,758 [Application Number 04/788,435] was granted by the patent office on 1971-10-19 for propagation primer.
This patent grant is currently assigned to Dynamit Nobel Aktiengesellschaft. Invention is credited to Hellmut Bendler, Heinz Gawlick, Gunther Marondel, Werner Siegelin.
United States Patent |
3,613,758 |
Gawlick , et al. |
October 19, 1971 |
PROPAGATION PRIMER
Abstract
A propagation primer containing a primer charge having a
composition comprising, by weight, approximately: 40-60 percent of
barium nitrate 10-20 percent of an aluminum-magnesium alloy 5-20
percent of lead dioxide 6-10 percent of zirconium hydride, and 1-5
percent of boron The composition is substantially insensitive to
friction and shock. For propagation over larger distances,
additional specific primer compositions may be employed.
Inventors: |
Gawlick; Heinz (Furth,
DT), Marondel; Gunther (Erlangen, DT),
Bendler; Hellmut (Nuremberg, DT), Siegelin;
Werner (Stein, DT) |
Assignee: |
Dynamit Nobel
Aktiengesellschaft (Troisdorf, DT)
|
Family
ID: |
5684589 |
Appl.
No.: |
04/788,435 |
Filed: |
January 2, 1969 |
Foreign Application Priority Data
|
|
|
|
|
Jan 13, 1968 [DT] |
|
|
P 16 46 350.6 |
|
Current U.S.
Class: |
149/15; 149/28;
149/62; 149/22; 149/43; 149/61; 149/88 |
Current CPC
Class: |
F42C
19/0803 (20130101); F42C 19/0815 (20130101); C06C
5/06 (20130101) |
Current International
Class: |
C06C
5/00 (20060101); C06C 5/06 (20060101); F42C
19/08 (20060101); F42C 19/00 (20060101); C06c
003/10 () |
Field of
Search: |
;149/61,43,22,62,28,15,88 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Quarforth; Carl D.
Assistant Examiner: Lechert, Jr; Stephen J.
Claims
We claim:
1. A propagation primer composition substantially insensitive to
friction and shock comprising, by weight, approximately:
40- 60 percent of barium nitrate
10- 20 percent of an aluminum-magnesium alloy
5- 20 percent of lead dioxide
6- 10 percent of zirconium hydride, and
1- 5 percent of boron.
2. A propagation primer composition substantially insensitive to
friction and shock comprising a first primer charge having a
composition comprising, by weight, approximately:
40-60 percent of barium nitrate
10- 20 percent of an aluminum-magnesium alloy
5- 20 percent of lead dioxide
6- 10 percent of zirconium hydride, and
1- 5 percent of boron
contiguous to a second primer charge having a composition
comprising, by weight, approximately:
40- 60 percent of barium nitrate
13- 25 percent of calcium silicide
10-20 percent of lead dioxide
8- 14 percent of an aluminum-magnesium alloy and, if desired,
1- 6 percent of boron.
3. A propagation primer composition substantially insensitive to
friction and shock comprising a first primer charge having a
composition comprising, by weight, approximately:
40-60 percent of barium nitrate
10- 20 percent of an aluminum-magnesium alloy
5- 20 percent of lead dioxide
6- 10 percent of zirconium hydride, and
1- 5 percent of boron
contiguous to a second primer charge having a composition
comprising, by weight, approximately:
25- 45 percent of lead tricinate
3- 10 percent of nitroguanidine
24- 45 percent of barium nitrate, and
8- 25 percent of calcium silicide.
4. A propagation primer composition substantially insensitive to
friction and shock comprising a first primer charge having a
composition comprising, by weight, approximately:
40- 60 percent of barium nitrate
10- 20 percent of an aluminum-magnesium alloy
5- 20 percent of lead dioxide
6- 10 percent of zirconium hydride, and
1- 5 percent of boron
contiguous to a second primer charge having a composition
comprising, by weight, approximately:
50 percent of barium nitrate
20 percent of calcium silicide
15 percent of lead dioxide
12 percent of an aluminum-magnesium alloy, and
3 percent of boron.
5. A propagation primer composition substantially insensitive to
friction and shock comprising a first primer charge having a
composition comprising, by weight, approximately:
40- 60 percent of barium nitrate
10- 20 percent of an aluminum-magnesium alloy
5- 20 percent of lead dioxide
6- 10 percent of zirconium hydride, and
1- 5 percent of boron
contiguous to a second primer charge having a composition
comprising, by weight, approximately:
30percent of lead tricinate
5 percent of nitroguanidine
45 percent of barium nitrate, and
20 percent of calcium silicide.
6. A propagation primer composition substantially insensitive to
friction and shock comprising, by weight, approximately:
40- 60 percent of barium nitrate
13- 25 percent of calcium silicide
10- 20 percent of lead dioxide
8- 14 percent of an aluminum-magnesium alloy and, if desired,
1- 6 percent of boron.
7. A propagation primer composition substantially insensitive to
friction and shock comprising, by weight, approximately:
25- 45 percent of lead tricinate
3- 10 percent of nitroguanidine
24- 54 percent of barium nitrate, and
8- 25 percent of calcium silicide.
8. A propagation primer composition substantially insensitive to
friction and shock consisting of, by weight, approximately:
50 percent of barium nitrate
20 percent of calcium silicide
15 percent of lead dioxide
12 percent of an aluminum-magnesium alloy, and
3 percent of boron.
9. A propagation primer composition substantially insensitive to
friction and shock consisting of, by weight, approximately:
30 percent of lead tricinate
5 percent of nitroguanidine
45 percent of barium nitrate, and
20 percent of calcium silicide.
10. A propagation primer composition substantially insensitive to
friction and shock consisting of, by weight, approximately:
60 percent of barium nitrate
15 percent of an aluminum-magnesium alloy
12 percent of lead dioxide
10 percent of zirconium hydride, and
3 percent of boron.
Description
BACKGROUND OF THE INVENTION
This invention relates to a propagation primer. More particularly,
it relates to propagation primers which are insensitive to friction
and shock and which contain a primer charge of particular
constituents and/or particular primer compositions.
For use in priming systems, particularly those of the military
type, propagation or transmission primers are known having a primer
composition containing up to about 60 percent by weight and more of
an explosive. These primers, also called flash or flame primers,
serve for the transfer or transmission of an ignition impulse,
optionally with simultaneous boosting, over a more or less long
distance. The operation of such primers involves ignition on one
side, called the igniting side, by a flame arriving at said side
and then the emission by the primer itself of a flame on the other
side, called the firing side, whereby a further ignition is
triggered by means of the latter flame at a certain distance. Thus,
the provision can be made, for example, in the case of aircraft or
missiles, to ignite a propagation primer by means of a conventional
perforating, percussion or electrical primer provided at the head
of the aircraft, the propagation primer then, in turn, emitting a
flame and igniting, for example, through a tube or the like, a
further detonation-triggering primer element disposed at a
detonator, an explosive charge, or the like, provided in the center
or also at the end of the aircraft. Such a provision is made
because the primer element is too far apart from the conventional
primer to be ignited directly thereby.
For certain purposes, it is required that the device provided for
transmitting the ignition flash be most extensively insensitive
against outside influences, i.e., it should not become effective
unintentionally or inadvertently by mechanical effects, such as
impacts, shocks, or the like. In connection with propagation
charges, the propagation primer must thus exhibit a shock and
friction sensitivity which is lower than that of the propagation
charge. Since compact bodies of tetryl
(trinitrophenylmethylnitramine) or penthrite (pentaerythrite
tetranitrate) are usually employed in the art as the propagation
charge, there is hence the requirement for the propagation primers
that the sensitivity to shock and friction be lower than that of
the substances tetryl and penthrite.
One of the objects of the present invention is to provide a
propagation primer having properties and advantages superior to
those of the prior art.
Another object of the present invention is to provide a propagation
primer which is extremely insensitive to friction and shock.
A further object of the invention is to provide primer charges and
primer compositions which can be used advantageously in primers
used for the transmission of an ignition impulse over a more or
less long distance.
A still further object of the invention is to provide advantageous
propagation primers which may be manufactured readily.
These and other objects and advantages of the present invention
will become apparent to those skilled in the art from a
consideration of the following specification and claims.
SUMMARY OF THE INVENTION
In accordance with the present invention, it has been found that
the above advantages and requirements are met by a primer
containing a primer charge consisting essentially of, by weight,
about:
a. 40-60% of barium nitrate, 10-20% of an aluminum-magnesium alloy,
5-20% of lead dioxide, 6-10% of zirconium hydride, and 1-5% of
boron;
and/or a primer charge consisting essentially of, by weight, either
approximately:
b.sub.1. 40-60% of barium nitrate, 13-25% of calcium silicide,
10-20% of lead dioxide, 8-14% of an aluminum-magnesium alloy, as
well as optionally an addition of about 1-6% of boron;
or approximately:
b.sub.2. 25-45% of lead tricinate (lead trinitroresorcinate) 3-10%
of nitroguanidine, 25-45% of barium nitrate, and 8-25% of calcium
silicide.
When accommodated in a metallic part dammed up toward the igniting
side, or in a correspondingly constructed primer case or cup, the
first-mentioned primer charge composition a satisfactorily ignites
propellant charges, as well as pyrotechnical mixtures, over short
distances. If propagation is to be executed over larger distances,
then the first-mentioned primer charge mixture a is suitably
maintained as the initial igniting composition, but as the
propagation charge, there is employed one of the two additionally
mentioned primer charge mixtures b.sub.1 or b.sub.2, depending on
the particular requirements involved. The addition of boron
mentioned in connection with the primer charge composition b.sub.1
is employed for reinforcing the initial ignition. For the
propagation of the ignition over a distance of about 30- 120 cm.,
perhaps through a narrow tube, the utilization of an explosive
cannot be avoided. Thus, in this case, the primer composition
b.sub.2 is suitable. In the latter case, it may well be advisable,
although it is not always necessary, to employ in conjunction with
this primer charge composition also the primer charge composition a
. As for the geometric arrangement of the mixture, the same
requirements and considerations are applicable as in the
utilization of a composition mixture which is free of
explosives.
All primer composition mixtures wherein the individual components
are employed in quantities ranging within the above-stated limits
are substantially less sensitive against shock and friction than
the conventional primer charges, and they are also less sensitive
than tetryl and penthrite. In this connection, the shock
sensitivity thereof is between 0.6 and 1.5 mkp. (meters.sup..
kilopond), depending upon the ratios in which the individual
composition components are employed within the above-mentioned
permissible limits. The friction sensitivity of all the
compositions in accordance with the present invention is above 30
kp. load, as measured in the friction apparatus according to
Rathsburg.
BRIEF DESCRIPTION OF THE DRAWING
The present invention will become more fully understood from the
detailed description given hereinbelow and the accompanying drawing
which is given by way of illustration only and thus is not limiting
of the present invention and wherein,
FIG. 1 shows a primer with an igniting charge and a subsequent
firing element;
FIG. 2 shows a primer having a booster charge interposed; and
FIG. 3 shows a schematic view of an ignition chain or sequence.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Referring now to the drawings, wherein like reference numerals are
used throughout the various figures to designate like parts,
embodiments for propagation primers with the use of a primer charge
in accordance with the present invention are illustrated.
The igniting composition 3 and the firing charge 4 are disposed one
behind the other in the primer case 1, which latter is open on both
ends and is made of, for example, a metal such as brass. The firing
charge is covered by a thick foil or the like. The opening in the
primer case on the igniting side is provided with the funnel-shaped
widened section 2. A flame arriving in the direction of the upper
arrow ignites the igniting charge 3 which, in turn, ignites the
igniting charge 3 which, in turn, ignites the firing charge 4 and
sends, after destroying the cover, an igniting flame in the
direction of the lower arrow.
According to FIG. 2, the booster charge 5 is disposed in the primer
case 1, provided with an annular flange, between the igniting
charge 3 and the firing charge 4. The firing charge is again
covered by a foil or the like, and the opening on the igniting side
is again provided with the funnellike widened section 2. The
propagation primer provided for bridging a distance of, for
example, more than 200 mm., is again ignited by a flame arriving at
the igniting side. The igniting charge 3 then ignites the booster
charge 5, and the latter ignites the firing charge 4, with a
simultaneous reinforcement of the ignition jet being sent out by
the firing charge. The booster charge, shielded by the igniting
charge 3, the firing charge 4 and the case 1 can, in this
embodiment, be provided with an explosive without incurring any
disadvantages.
In the ignition chain of FIG. 3, the primer element 7 is provided
in the igniter (detonator) 6, which primer element can be, for
example, a conventional perforation (pin-actuated) primer or a
percussion primer or, also, a likewise known electrical primer.
After being triggered, this primer element ignites, by means of its
ignition flame sent out in the direction of the arrow, the
propagation primer 9a disposed at the upper end of the tube 8 and
provided with the primer composition of the present invention. The
propagation primer 9a effects the ignition of the identical
propagation primer 9b disposed in the center of the tube. Finally,
the ignition is propagated from the latter primer 9b to the
propagation primer 9c provided at the lower end of the tube, which
primer is likewise identical with the primers 9a and 9b . This
ignition chain can be made as long as desired. In this connection,
the spacing between the propagation primers depends, of course, on
the particular primer charge employed. At the front end of the
ignition chain there is then provided a primer element which, in
turn, ignites an explosive charge or the like.
It has been found that an especially advantageous primer charge
composition a is the following:
60 percent of barium nitrate
15 percent of an aluminum-magnesium alloy
12 percent of lead dioxide
10 percent of zirconium hydride, and
3 percent of boron.
Other preferred compositions include, for example, a propagation
system containing a primer charge b.sub.1 disposed on the firing
side and comprising:
50 percent of barium nitrate
20 percent of calcium silicide
15 percent of lead dioxide
12 percent of an aluminum-magnesium alloy, and
3 percent of boron
or a propagation primer containing a primer charge b.sub.2 having
the following composition:
30 percent of lead tricinate
5 percent of nitroguanidine
45 percent of barium nitrate, and
20 percent of calcium silicide
The invention being thus described, it will be obvious that the
same may be varied in many ways. Such variations are not to be
regarded as a departure from the spirit and scope of the invention,
and all such modifications as would be obvious to one skilled in
the art are intended to be included herein.
* * * * *