U.S. patent number 3,757,696 [Application Number 05/131,206] was granted by the patent office on 1973-09-11 for electronic squib firing sequencer.
This patent grant is currently assigned to The United States of America as represented by the Secretary of the Army. Invention is credited to Joseph T. Derk.
United States Patent |
3,757,696 |
Derk |
September 11, 1973 |
ELECTRONIC SQUIB FIRING SEQUENCER
Abstract
In a projectile carrying a plurality of payloads which are to be
sequentiy ejected, an electronic circuit for selectively firing
ejection charges, which comprises a series of interlocked switches
that are held in one position by the presence of the projectile
backplate. Upon release of the backplate the switches assume a
second position and thereby permit the application of voltage to an
R-C network in which the capacitors charge up to a voltage
sufficient to overcome a zener diode that in turn activates a
silicon controlled rectifier via its conrol electrode. The
rectifier is connected in series with an electrical energy source,
ground interlock switches and a squib so as to fire the same
sequentially after some selected period set by each of the R-C
networks. The ground interlocks being connected so as to
effectively short circuit the squibs prior to release of the
backplate.
Inventors: |
Derk; Joseph T. (Wharton,
NJ) |
Assignee: |
The United States of America as
represented by the Secretary of the Army (Washington,
DC)
|
Family
ID: |
22448396 |
Appl.
No.: |
05/131,206 |
Filed: |
April 5, 1971 |
Current U.S.
Class: |
102/217;
102/393 |
Current CPC
Class: |
F42B
12/62 (20130101) |
Current International
Class: |
F42B
12/62 (20060101); F42B 12/02 (20060101); F42b
022/30 (); F42c 009/00 () |
Field of
Search: |
;102/7.2R,82,7R,28P
;181/.5FS |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Borchelt; Benjamin A.
Assistant Examiner: Doramus; J. V.
Claims
I claim:
1. A missile electronic firing system for sequentially activating a
plurality of squibs for sequential ejections of payloads from the
missile, which missile is provided with a mechanism for releasing
the backplate thereof at some time after launch, said firing system
comprising:
a plurality of squib firing circuits, one for each squib, and each
circuit having included therein,
an asymmetrical electrical conducting means having a control
element whereby when a specific voltage is applied thereto said
conducting means will conduct between its input and output.
a source of electrical energy having a positive and a ground
terminal,
an independently variable time delay means connected to said
control element,
a first bias switch connected intermediate said source and said
delay means and disposed in abutting relation to said backplate and
activated by the release thereof to apply said source to said delay
means,
a pair of terminals, one of said terminals connected to the output
of said conducting means and the other terminal connected to said
ground terminal of said source,
a main source of electrical energy connected across the input of
each of said conducting means and said ground terminal of said
source,
whereby when a squib is connected across each of said pairs of
terminals the squibs will be activated at different times after
said backplate is released which will cause said payloads to be
ejected sequentially.
2. The system according to claim 1 wherein said delay means
includes a series R-C connected resistor and capacitor and a Zener
diode and a second resistor.
3. The system according to claim 2 wherein said conducting means is
a silicon controlled rectifier.
4. The system according to claim 3 wherein said first bias switch
includes a pair of stationary contacts and a movable pole biased to
contact one of said contacts and physically deflectable to contact
the other of said stationary contacts when in abutting relation to
said backplate, said one contact connected to said ground terminal
of said source and said other contact connected to said positive
terminal of said source, said pole connected to said R-C
junction.
5. The system according to claim 4 further including for each
firing circuit a single pole-single throw bias switch in abutting
relation to said backplate for connecting said ground terminal to
said output of said silicon rectifier and removing the same when
said backplate is released.
6. The system according to claim 5 further including another single
pole-single throw bias switch connected intermediate said main
source and the anode input of said silicon rectifier.
7. The system according to claim 6 wherein all of said bias
switches are microswitches.
Description
The invention described herein may be manufactured, used and
licensed by or for the Government for governmental purposes without
the payment to me of any royalty thereon.
BACKGROUND OF THE INVENTION
The present invention relates to system for ejecting a plurality of
payloads from a projectile and more particularly pertains to an
electronic circuit for sequentially initiating the payload release
at selected intervals and incorporates therein malfunction, safety
interlocks.
In the field of sequential payload ejection, it has been the
general practice to employ some pyrotechnic delay composition whose
initiation was dependent of the activation of an explosive used to
blow off the backplate. This method has proved unsatisfactory in
that the ejection times were unpredictable and without proper
function times, plural payloads would be simultaneously ejected
resulting in an action which defeated the primary delivery purpose.
In addition, where the payloads were deployed with parachutes,
fouling thereof occurs in many instances. This problem has been
satisfactorily overcome by the present invention.
SUMMARY OF THE INVENTION
The general purpose of this invention is to provide a sequential
squib firing circuit for payload ejection that has all the
advantages of similarly employed prior art devices and has none of
the above described disadvantages. To attain this, the present
invention provides, for each payload, a unique circuit arrangement
interlocked with the backplate and which includes an R-C network
coupled to overcome a Zener diode and whose charging commences upon
the release of said plate. The diode is connected to turn on a
silicon controlled rectifier which in turn permits the squib to be
fired from an electrical source. Each R-C network includes selected
components to allow independent setting of the time period between
plate release and payload ejection.
An object of the present invention is to provide a simple,
reliable, safe and inexpensive squib firing sequencer circuit for
initiating the ejection of payloads from a projectile at selected
intervals.
Another object is the provision of an electronic circuit for
sequentially firing a plurality of squibs which, circuit is capable
of withstanding setback forces of 30 g's.
Other objects and many of the attendant advantages of this
invention will be readily appreciated as the same becomes better
understood by reference to the following detailed description when
considered in connection with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a perspective view, partially in section, of a missile in
which the subject invention is employed; and,
FIG. 2 is a schematic of an embodiment made in accordance with the
principle of this invention.
DESCRIPTION OF A PREFERRED EMBODIMENT
The missile 10 of FIG. 1 carries at its nose end a pair of dual
thrust rocket motors 11 while the remaining portion of the missile
is provided with a payload chamber 12 that contains the ejection
control system 13 as well as three payloads 14 (two of which are
shown). The rear end of the missile is closed by a backplate 15
that is held in position by four radial release pins 16 whose
central area carries a piston arrangement 17 communicating with a
forward black powder charge 18 through blast tube 19. Each payload
is housed in a launch tube 20 and at the forward end thereof
includes an ejection piston 21 that is activated by an ejection
charge 22 in which is disposed a squib 23, so that when the squib
is activated it will fire the charge and the expanding gases will
displace the piston rearwardly against the nose of the payload,
driving or ejecting the payload after the backplate has been
released. The sequence for removal of the backplate is as follows:
A mechanical time fuze 24 is activated at a prescribed time after
launch, based on the desired range and it initiates an explosive
train in the charge 18 generating a pressure wave which travels
down the blast tube 19 and acts against the backplate piston
arrangement 17 to blow off the backplate. The three small payload
charges 22 are sequential ignited by the subject embodiment of this
invention, namely, the electronic squib firing sequencer or
ejection control system 13 and each one in turn acts on the payload
ejection piston to launch the payloads. These payloads are provided
with attached drogue parachutes 25 which are deployed as soon as
the load clears the missile and serve to limit the impact velocity
of the payload.
Having described the general environment and operation of the main
elements, attention is now directed toward the subject inventive
embodiment which comprises two separate physical structures but a
single electrical system. A plurality of micro switches in a
support 26 are positioned against the backplate so that they will
assume their unbiased switch position when the plate against which
they abut is removed. The remaining portion of the electronics is
disposed forward of the payload with the squibs adjacent the
ejection charges. The seven bias or micro switches 27-33, as shown
in FIG. 2, with their movable arms 34-40 (for the dotted position)
in the biased position as when in abutting relation to the
backplate and for the solid showing with the backplate removed. Two
switches are provided for each squib, with the main power switch 30
having its arm 37 connected through a single-pole single throw 41
switch to a battery 42 and its fixed contact connected to the anode
resistor 43-45 of an asymmetrical conducting means such as silicon
controlled rectifiers (SCR) 46-48. With switch 30 open, no power is
present at the SCR anodes 46-48 so that no current can flow from
the anode to the cathode 52-54 even if the gate electrode 55-57
were accidentally energized. One stationary contact 59-64 of each
control switch is connected to the ground or the negative side of
the source or battery 42 as well as to negative side of batteries
65-67. The other stationary contacts 68-70 of R-C gate switches
27-29 are connected via resistors 71-73 to the high or positive
terminals of batteries 65-67. The movable arms 34-36 of the gate
switch are connected to charging capacitors 74-76 so that when the
arm is released (backplate removed) it effectively places the
battery across the delay means or R-C network (71-74, 72-75, 73-76)
and commences charging of the capacitor. At the same time the
movable arms 38-40 of squib switches 31-33 open from their fixed
contacts and thereby remove ground from the squibs 23, 23a, 23b and
power switch 30 connects the positive terminal of battery 42 to
anode resistors 43-45 and ground via capacitors 77-79. Charging
capacitors 74-76 commence to charge toward the battery voltage at a
rate dependent on their time constants or the values of resistance
and capacitance. When the potential on each capacitor reaches the
breakdown or conduction voltage of the Zener diode 80-82 it then
conducts (discharges capacitor), via discharge divider resistors
83-85, 86-88 providing a voltage at their junction and on the SCR
gates 55-58. This voltage is sufficient to turn the SCR "on" and
conduction takes place between the anode and cathode through the
squib 23 to the battery 42 negative. This passage of current
through the squib fires it almost instantaneously. By properly
adjusting the R-C time constant of each squib circuit, they can be
made to fire sequentially with variable time differentials. The
timing adjustment can most readily be accomplished by setting
variable resistors 71-73 to the selected values.
The system operation can best be summarized as follows: The missile
fuze timer fires a powder charge which blows off the backplate
cover and releases the seven micro switches mounted on the rear of
the missile. The switches are activated as the backplate is blown
clear of the missile. Three of the switches serve to short out the
squibs with the backplate in place while another three are utilized
to activate the R-C time voltages across the capacitors when the
backplate is blown off. The remaining switch maintains an open
circuit for the firing voltage at the SCR anode and closes the
circuit only upon release of the backplate. When one of the
capacitors charges up sufficiently, the Zener diode conducts and
the first SCR conducts from its anode to cathode and fires the
first squib. The time interval is dependent on the R-C time
constant and by appropriately selecting the resistance for each
circuit, the squibs will be fired sequentially.
It should be understood, of course, that the foregoing disclosure
relates only to a preferred embodiment of the invention and that
numerous modifications or alterations may be made therein without
departing from the spirit and the scope of the invention as set
forth in the appended claims.
* * * * *