U.S. patent number 3,748,955 [Application Number 05/182,106] was granted by the patent office on 1973-07-31 for circuit arrangement for rocket launchers.
This patent grant is currently assigned to Licentia Patent-Verwaltungs-G.m.b.H.. Invention is credited to Willi Gatermann, Heinz Hermes, Hinderk Mudder, Herbert Sedlacek, Rolf Sorgel, Laus-Dietrich Thieme, Uwe Weers.
United States Patent |
3,748,955 |
Gatermann , et al. |
July 31, 1973 |
**Please see images for:
( Certificate of Correction ) ** |
CIRCUIT ARRANGEMENT FOR ROCKET LAUNCHERS
Abstract
A rocket launcher firing control circuit in which a series of
rockets are fired either individually or automatically in sequence
under the control of a mode selector switch control the mode of
operation of a clock pulse generator, a counter counting the
generator pulses and a decoder controlled by the counter output for
firing the detonator caps of a series of rockets in sequence via
thyristors connected in parallel to a power source. The control
electrode of each thyristor is connected to a separate output of
the decoder and the generator is controlled by a digital control
unit so that the operation of the system is not impaired by the
presence of a faulty rocket detonator unit.
Inventors: |
Gatermann; Willi
(Wedel/Holstein, DT), Sorgel; Rolf (Wedel/Holstein,
DT), Mudder; Hinderk (Wedel/Holstein, DT),
Thieme; Laus-Dietrich (Wedel/Holstein, DT), Sedlacek;
Herbert (Hamburg-Rissen, DT), Weers; Uwe
(Elmshorn, DT), Hermes; Heinz (Wedel/Holstein,
DT) |
Assignee: |
Licentia
Patent-Verwaltungs-G.m.b.H. (Frankfurt am Main,
DT)
|
Family
ID: |
5782748 |
Appl.
No.: |
05/182,106 |
Filed: |
September 20, 1971 |
Foreign Application Priority Data
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|
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Sep 18, 1970 [DT] |
|
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P 20 46 098.4 |
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Current U.S.
Class: |
89/1.814;
102/215; 102/217; 361/249 |
Current CPC
Class: |
F41A
19/64 (20130101); F42D 1/055 (20130101); H03K
5/15013 (20130101) |
Current International
Class: |
F42D
1/055 (20060101); F41A 19/64 (20060101); F42D
1/00 (20060101); F41A 19/00 (20060101); H03K
5/15 (20060101); F41f 003/04 () |
Field of
Search: |
;89/1.814 ;102/7.2A,7.2R
;317/80 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Engle; Samuel W.
Claims
We claim:
1. In a device for launching a plurality of rockets each containing
a detonator device arranged in a firing circuit, a circuit for
controlling the firing of the detonator devices, comprising, in
combination: a firing key connected for applying firing energy to
the detonator devices; mode selector switch means connected for
controlling the mode of operation of said circuit and switchable
between a first position in which it causes all previously unfired
detonator devices to be fired in sequence when said key is actuated
and a second position in which it causes one detonator device to be
fired each time said key is actuated, successive actuations of said
key causing successive detonator devices to be actuated; and
control circuit means connected between said key, said mode
selector switch means and the detonator devices for sustaining the
selected mode of operation of said circuit despite malfunctions in
the firing current path of one or more of the detonator devices,
said control circuit means including: a plurality of thyristors
each having one main electrode arranged to be connected to a
respective detonator device; an electronic switch one side of which
is connected to said key and the other side of which is connected
in common to the other main electrodes of all of said thyristors; a
clock pulse generator connected to control the operation of said
electronic switch; a counter and decoder connected between said
generator and the control electrodes of said thyristor; a digital
control unit connected between said selector switch means and said
generator for controlling the operation of said generator; and a
current sensor connected for sensing the current conducted by said
electronic switch and producing an output signal when it senses a
current level corresponding to that drawn by an operative firing
circuit, said sensor being connected to apply its output signal as
an input to said control unit; wherein when said switch means is in
its said first position, said pulse generator produces an output at
a first frequency, composed of pulses whose duration is different
from the interval between pulses, which causes each of said
thyristors to be triggered into conduction in sequence by the
output signals from said decoder, and said control unit is
responsive to the switching of said selector switch into its said
second position for causing said generator to produce an output at
a second frequency higher than said first frequency upon the
actuation of said key and until said sensor produces its output
signal, to then produce an output at said first frequency to fire
an operative detonator device, and to then stop.
2. An arrangement as defined in claim 1 wherein when said selector
switch means is in its said second position, said control circuit
is arranged to maintain the operation of said generator at said
first frequency when the output signal from said sensor is due to a
short-circuited firing circuit and until a detonator device in an
operative firing circuit is fired.
Description
BACKGROUND OF THE INVENTION
The present invention relates to a circuit arrangement for rocket
launchers, particularly for triggering detonator caps in such a
manner as to permit firing rockets either in sequence or
individually.
The firing of a rocket propelling charge is initiated by a
so-called detonator cap which is disposed in the charge. Such
detonator cap contains a heating wire which is enclosed by a
quantity of powder. When the heating wire is heated, the quantity
of powder is ignited so that the outer shell of the detonator cap
explodes and fires the rocket propellant charge.
With a plurality of rockets arranged next to one another to
constitute a rocket battery or batteries it is necessary, for
example, that the rockets be fired either one after the other at
certain time intervals, i.e., in sequence, or that each individual
rocket be fired separately. To meet this requirement, an
electromagnetic circuit arrangement is known which is operated by a
stepping switch mechanism. The entire circuit arrangement is built
into the rocket starting device.
This circuit arrangement has the drawback that the presence of a
short circuit in one of the firing lines leading to one rocket
prevents the firing of the detonator caps which are connected to
the firing lines following the short-circuited line.
Furthermore, it is possible for the mechanical follower in the
stepping switch mechanism to malfunction during an acceleration of
the circuit arrangement. Such an acceleration may occur, for
example, when the rocket launchers are mounted on airborne
bodies.
A soiling of the contacts of the switching mechanism is also very
detrimental to perfect operation.
SUMMARY OF THE INVENTION
It is therefore an object of the present invention to provide a
circuit arrangement which eliminates the above-mentioned
drawbacks.
A further object of the invention is to assure fault-free firing of
a plurality of rockets either in sequence or individually from
launchers disposed on the ground or from those mounted on airborne
bodies.
These and other objects are accomplished according to the present
invention by the provision of means which initiate the functions
"sequential firing" or "individual firing" under the control of an
operational mode selection switch and a firing key and through the
application of a supply voltage, and which assure the automatic
sequence of the firing process even when there is a fault in one or
more of the firing lines.
The supply voltage can be switched, during the sequential firing
operation, from an electronic switch to a plurality of thyristors
in succession, a clock pulse generator controlling the electronic
switch as well as the thyristors, the latter via a counter and a
decoder. The clock pulse generator provides for this purpose a
frequency which has a varying value.
For the "individual firing" operation, the clock pulse generator,
which simultaneously controls a counter and an electronic switch,
is switched by means of a digital control unit to produce a high
clock pulse frequency. This high clock pulse frequency continues
until a current sensor locates a closed firing circuit and
furnishes a signal to the digital control unit. Then the clock
pulse generator switches back to the original frequency, the firing
voltage is applied to the thryistor of the closed firing circuit
and the digital control unit furnishes a stop signal to the clock
pulse generator when the thyristor has fired. The digital control
unit will not furnish a stop signal to the clock pulse generator
when there is a permanent short circuit in one of the firing
lines.
The advantage of the present invention is that no memory elements
are provided in the circuit arrangement. Thus it results that only
the perfect detonator cap which is next in line in the given
sequence is fired, regardless of the presence of a short circuit or
an interruption in the preceding firing line. Even with a short
circuit or an interruption in one firing line, the "series firing"
and "individual firing" operations are performed. The circuit
arrangement can also be built into the rocket launching devices in
place of the previously employed electromagnetic circuit
arrangement.
BRIEF DESCRIPTION OF THE DRAWING
FIG. 1 is a circuit diagram of one preferred embodiment of the
present invention.
FIG. 2 illustrates one embodiment of a applied clock pulse
generator.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
The firing circuit of the illustrated embodiment includes a firing
unit 1 in which a plurality of, e.g., 10, thyristors are connected
together, only three thyristors 2, 3 and 4 being shown. The outputs
of the thyristors 2, 3 and 4 are connected in a standard manner to
heating wires belonging to detonator caps (not shown). The control
inputs of the thyristors are conductively connected to a clock
pulse generator 7 via a decoder 5 and a binary coded decimal
counter 6, the clock pulse generator 7 being fed by the supply
voltage for the system.
Two control inputs of the clock pulse generator 7 are conductively
connected to two outputs of a digital control unit 8. One of the
connecting lines is required for switching the frequency of the
clock pulse sequence and the other line is required to switch off
the clock pulse generator 7.
The digital control unit 8 has a total of three inputs: the first
input is connected to the output of the clock pulse generator 7;
the second input is electrically connected to an operational mode
selector switch 9; and the third input with the signal output of a
current sensor 10.
The supply voltage inputs of the thyristors 2, 3, 4, etc., are
connected, via the operating circuits of current sensor 10 and an
electronic switch 11, to a firing key 12 through which the supply
voltage can be applied to the electronic switch 11 as well as to
the clock pulse generator 7. The control input of the electronic
switch 11 is in electrically conductive connection with the output
of the clock pulse generator 7.
The mode of operation of this circuit arrangement will first be
described for the sequential firing function, in which the
operational mode selection switch 9 has the illustrated position
and the supply voltage is applied, via electronic switch 11 and
current sensor 10, in succession to thyristors 2, 3, and 4 and thus
also to their associated detonator caps.
The automatic firing process of thyristors 2, 3, and 4 is initiated
by the actuation of the firing key 12 and continues as follows:
First clock pulse generator 7 starts running freely and feeds
pulses at its normal clock pulse frequency to the BCD counter 6.
The decoder 5 converts the BCD code to a (.sup.10) code and applies
in succession with each count a control pulse to the control input
of each successive thyristor 2, 3, and 4, etc., each pulse having a
duration of 20 msec. The time between the firing of two adjacent
thyristors is 25 msec, so that in this example with 10 detonators
all of the thyristors will have been pulsed once in a period of 250
msec.
Together with the timing of clock pulse generator 7, the electronic
switch 11 is controlled in parallel with the control pulses and the
supply voltage is applied to the voltage inputs of the thyristors
2, 3, and 4, etc., in synchronism with the control pulses. However,
it will be only the thyristor which receives a control voltage at
its grid and a supply voltage at its voltage input which will be
fired. This AND requirement - presence of the supply voltage and
the grid pulse at the same time - must always be met to fire a
detonator cap.
In order to achieve the required firing sequence period of 25 msec
in operation, the clock pulse generator must be so designed that it
emits a clock pulse train with pulses and pulse intervals of
different durations. For a time period of 20 msec the clock pulse
generator 7 emits a signal representing a binary "1" which closes
the electronic switch 11, i.e., renders it conductive, and
simultaneously serves as a counting pulse for the BCD counter 6. A
firing pulse is derived from the counter output by decoder 5. The
counter 6 is set to produce an output signal representing a logic 0
at each switching on by the firing key 12 so that a continuous
firing sequence from thyristor 2 to thyristor 4 is always
assured.
If it should occur that the detonator cap in one of the rockets
burns into a short circuit so that the launch can not be initiated,
the current to that cap is interrupted after approximately 20 msec
by the circuit arrangement itself, and after the current
interruption there is a pause of 5 msec until the next detonator
cap is fired. The circuit arrangement acts in the same manner when
the input leads to one or more detonator caps have a short circuit
to ground. If, however, a firing line is broken, the effect on the
circuit arrangement will be the same as if the detonator cap had
already been fired.
For the individual firing function, the circuit arrangement is to
fire only a single thyristor and launch only one rocket. For this
purpose, the operational mode selector switch 9 in the rocket
launching device is moved into the position shown in the drawing in
dashed lines to connect one input of control unit 8 to ground. With
this switching arrangement the clock pulse frequency of the clock
pulse generator 7 is switched by means of the digital control unit
8 to a higher value. As for the case of sequential operation,
counter 6 is controlled to effect a count simultaneously with the
closing of electronic switch 11.
If several detonator caps have been fired, the clock pulse
generator 7 continues at the higher clock pulse frequency until the
current sensor 10 detects a closed firing circuit. The current
sensor 10, when it has recognized a closed firing circuit,
furnishes a signal to the digital control unit 8 which switches
clock pulse generator 7 back to the original frequency. If the
current sensor 10 indicates, within a period of 20 msec, a current
interruption in the recognized firing circuit, i.e., the thyristor
associated with this firing circuit is being fired so that there
now is an open firing circuit, the digital control unit 8
additionally furnishes a stop signal to clock pulse generator 7.
The stop signal prevents a further switching to the next-following
firing circuit. The next firing of a thyristor can then take place
only through renewed depression of the firing key 12 so that
counter 6 is set back to zero and the next closed firing circuit is
located in a very short time.
If a short circuit is present in a line in the form of a previously
fired detonator cap, or if there is a line short circuit to ground,
the digital control unit 8 will not furnish a stop signal due to
the presence of a continuous short circuit current. Rather, as in
sequential operation, the current is switched off after 20 msec and
after a further 5 msec it is switched to the next firing circuit.
This process is automatically continued until a properly
functioning firing line has been found and the firing takes place
as planned. A firing circuit which has been interrupted by a
defective firing line can be considered to be an open firing line.
Line a in FIG. 2 serves to transmit a stop signal from the digital
control unit 8 to the clock pulse generator 7. On the other hand,
the signal transmitted by line b to the clock pulse generator 7
causes a change-over of the frequency of the clock pulse generator
7 from "Slow" to "Quick" or vice versa. The signal delivered by the
clock pulse generator 7 through line c serves to control the binary
coded decimal counter 6 of the electronic switch 11 and line b in
the individual as well as in the sequential firing operational
mode.
In the operational mode "Sequential firing" (switch 9 in the
position as shown), there is a L-signal at the inverter located in
the left upper part of the digital control unit 8, whereas a
O-signal is present at the inverter output. A O-signal is then
continuously applied to line a. In this operational mode no stop
signal can influence the clock pulse generator 7. The L-signal
deriving from the operational mode selector switch 9 results in a
continuous O-signal at the output of the upper right And-gate of
the digital control unit 8. Thus the current sensor 10 cannot
effect line b consequently, the signal on line b follows the signal
of line c.
In the operational mode "Individual firing" (switch 9 shown in the
position marked by dotted lines), there is a continuous L-signal at
the left input of the left lower And-gate of the digital control
unit 8 because of the negation by the inverter. Thus the signal on
line a can follow the signal output of the current sensor 10. The
clock pulse generator 7 is not stopped if the current sensor 10
should cause a L-signal. The stopping only takes place if this
signal returns to Zero. As long as the current sensor 10 has no
L-signal, the line b has a O-signal. The clock pulse generator 7
operates with this signal in the highest pulse frequency. When a
L-signal is present, the clock pulse generator 7 operates with the
lowest frequency. The feedback to the clock pulse generator 7
through line c in the operational mode "Individual firing" is
without effect on the signal on line b .
The clock pulse generator 7 shown in FIG. 2 has 3 inputs a, b and c
(as shown in FIG. 1) and the power supply. The control of the input
b has already been described together with the digital control unit
8. In case of a L-signal on line b, the transistor 13 is turned
on.
In order to charge the capacitor 14, in this case it is only the
resistor 15 that can become effective. A slow pulse sequence is
produced at the unijunction transistor. When line b has a O-signal
the resistor 17 acts in parallel to resistor 15 and furnishes the
necessary charging resistance. Thus the frequency of the pulse
sequence of the unijunction transistor 16 is increased. The output
signal of the transistor 16 is fed into a flip-flop 18, the output
signal of which appears on line c. The signal of line c is fed back
by the digital control unit 8 through line b of the clock pulse
generator 7. In the operational mode "Individual firing" the line a
has a L-signal, when a L-signal appears that is released by the
current sensor 10. Since a stop of the clock pulse generator 7 may
only take place after appearance of a O-signal on the line a
following the L-signal, this L-signal must first be converted in
the clock pulse generator 7 by an inverter 19, since the subsequent
flip-flop 20 only operates when the side of the pulse is positive.
The flip-flop 20 can then pass the information at its input D on
the positive pulse side to its output Q. Owing to the coupling
between the clock pulse generator 7 and the current sensor 11, at
this time only a L-signal can appear at the input D of the
flip-flop 20. In case of a L-signal at the output of the flip-flop
20, the transistor 21 is turned on. An additional charging of the
capacitor 16 is avoided.
The components not designated in FIG. 2 only serve to adjust the
operating point and to compensate the temperature of the
components.
In one embodiment of the present invention it is proposed to encase
the circuit arrangement in silicon rubber to form a completely
encapsulated unit. It is in this case advisable to dispose the
outputs so that they are protected against short circuits and the
inputs against changes of polarity. Such a case unit can easily be
installed in rocket launching devices.
It will be understood that the above description of the present
invention is susceptible to various modifications, changes and
adaptations, and the same are intended to be comprehended within
the meaning and range of equivalents of the appended claims.
* * * * *